JP2009174317A - Various energy conservation cycle combined engine - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To prevent great loss occurring by bringing the outputs close to 1/2,139 by high temperature combustion gas having 1/2,139 weight of water or the like through the improvement of the outdated invention at the time when it is sufficient with the generation of rotation output and jet propulsion output in an existing engine. <P>SOLUTION: In an energy conservation cycle combined engine, a mercury heat exchanger serving also as a diameter contracted main combustion chamber divides into high temperature mercury explosion force plus combustion gas mass explosion force through high pressure combustion heat exchange cooling combustion limitlessly. By adding excessively heated steam explosion force in injection promotion, high temperature mercury is subjected to vertically downward additional acceleration of gravity acceleration by vaporization explosion force. Rotation power is brought to 2,139*13.5=29,000 times that of combustion gas. A rotation output is brought closer to 100 times that of the existing technology by driving a full rotor blade mercury turbine so as to be made compact and simple. Supply equipment of heat, electricity and cold heat is taken as generator sets in the world, which is employed for equipment for infusing 300°C or lower heat of by-product in power generation into methane hydrate to vaporize and recover methane and to liquefy it by combustion gas exhaust becoming closer to absolute 0°C, an engine for driving automobile, airplane, marine vessel, space shuttle, rocket or the like in the world. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

  Various energy storage cycle coalescence engines of the present invention drive all blade mercury turbines to the same vacuum as the existing steam turbines, and the intake air is set to 60 to 200 degrees according to the usage amount at a mercury exhaust temperature of around 230 degrees, Cooling heat recovery air temperature is set to 800 to 1200 degrees, etc., and the cooling heat recovery air temperature is cooled to 250 to 300 degrees, etc. once or more, and the cooling heat recovery air temperature is cooled to 300 degrees, etc. by the reduced diameter compression chamber mercury heat exchanger 2Z in the final round. In the process of, the high-pressure combustion heat exchange cooling combustion is possible at any time as long as the fuel injection combustion, and the combustion gas is divided into the high-temperature mercury explosive power of the combustion gas calorie output + the combustion gas mass explosive power of the combustion gas mass output, and the combustion gas In the process of calorie output, for example, mercury explosive force of 600 to 800 degrees saturation pressure or higher + mercury injection pump 6Z injection speed, and acceleration of gravity by adding gravity acceleration vertically downward in vacuum In this process, high-speed mercury 1d with maximum specific gravity and maximum surface tension is generated, and rolling contact rotation output is generated. Will increase the energy revolution with various energy storage cycle coalescing engines, which will be 13.55 * 1700 times that of existing steam turbines = 23,000 times, and will be the best rotational output in theory, such as a small, simple, low-speed, and large rotational output. Regarding technology.

  Used in the same way as an existing steam turbine, the mercury exhaust saturation temperature is set to around 230 degrees Celsius, the mercury is accelerated by the vaporization explosive force of the high-temperature mercury 1d and the mercury injection pump 6Z injection speed, and the exhaust heat is recovered by the intake air. By making the intake air temperature 60 to 200 degrees, it is possible to use a large amount of high-pressure compressed air according to the application, and it is increased to 800 to 1200 degrees by one compression to constitute the theoretical best heat pump, In the process of dividing the mass output into a large amount of high-pressure combustion gas as much as possible, as the compression is performed once or more, the heat that is reduced to about 300 degrees by heating mercury is repeatedly recovered with compression heat to 800-1200 degrees, 300 degrees Combustion gas mass output before and after is set to 24 to 300 MPa or the like, and the whole rotor blade gas turbine gas turbine 8a or the vertical all rotor blade gas turbine 8A is driven to generate the rotational output in the process of generating exhaust gas -273. Allow maximum cold recovery amount close to, reversing the seawater temperature rise of the existing power generation technologies, relating to various energy conservation cycle combined engine technology.

  In the process of increasing the high-temperature mercury 1d temperature by using the reduced-compression chamber mercury heat exchanger 2Z to increase the high-temperature mercury heat exchange cooling without limit, increase the heat-resistant temperature and pressure pressure of the high-temperature high-pressure heat-resistant pressure vessel as much as possible. , Enabling the safe use of 600-1200 degrees, increasing the mercury vaporization explosive power during the expansion process, maximizing the recovery amount of the heat pump 1G and increasing the combustion gas calorie output, increasing the combustion gas mass output Therefore, make the full-blade mercury turbine and full-blade gas turbine the best rotational output theoretically, approach the 100-fold rotational output of the existing steam turbine with the same fuel amount, and use the combustion gas heat amount + combustion gas mass to the limit In order to save and use only heat output using heat recovery, the combustion gas mass is driven by the combustion gas mass explosive force of 300 to less than 24 to 300MPa, etc. As a theoretically best cold energy recovery means, we will develop and provide cold energy utilization means such as various devices utilizing cold energy, and expand and develop the effective energy utilization field, for example, cooling the whole urban area and reversing the heat island Regarding technology.

  It is possible to separate and recover CO2 and sulfur dioxide from nitrogen by melting point difference, approaching to absolute 0 degree, and after recovering cold, the combustion gas is dissolved in water to form combustion gas dissolved water, and the CO2 exhaust is set to zero. Combustion gas dissolved water is increased and used for various applications. In the process of heat exchange cooling, the intake air that has recovered the heat of exhaust gas is compressed and the temperature rises to 800-1200 ° C, etc. , Fuel injection combustion heat exchange cooling heat recovery as appropriate, all-blade mercury turbine with a heat supply per rotation output approaching 1/100 of the existing steam turbine, and mercury is vacuumed vertically downward by high-temperature mercury explosion force Acceleration with gravity acceleration added to make it the best theoretical all-blade mercury turbine drive, with a configuration that heats with the combustion gas of the reduced diameter main combustion chamber and heat exchanger, etc., a partial surplus heat amount of 300 degrees Celsius The following heat The global warming that prevents human extinction by focusing on power generation technology that is recovered and utilized, and by making vehicles, ships and airplanes with CO2 emissions close to 0, and by preventing the rise in seawater temperature ten times as scarce as CO2. Related to prevention technology.

  In the process of generating the propulsion output, there is no surplus heat and the rotational output is small, and the heat is recovered from the mercury exhaust temperature around 230 degrees and used to heat mercury and superheated steam. A very large amount of combustion gas and a large amount of superheated steam, such as 24 to 400 MPa around 400 degrees, can be present in large quantities, most of which are used for recovery of exhaust heat, and a large amount of unused oxygen-containing combustion gas exists. High-pressure combustion gas is supplied to the combined engine injection section 78K, fuel is injected and burned to approach the stoichiometric air-fuel ratio combustion, and the combustion gas is injected. In the combustion process, the superheated steam is heated by the combustor 1Y, high temperature combustion is enabled, the output is increased by high temperature combustion gas injection and high temperature superheated steam injection, and the theoretical best injection propulsion is achieved. The combustion gas and superheated steam are stirred and cooled to the atmosphere to produce combustion gas-dissolved water. The CO2 exhaust is brought close to zero and reduced to zero. The present invention relates to various energy storage cycle coalescing engines for jetting various airplanes, various spacecrafts and various ships.

  Atmospheric pressure mass because the existing engine invention is an improvement over the obsolete invention when it is sufficient to generate rotation output and injection propulsion output, and the engine invention is very difficult and there is no trace of improvement to the theoretically best invention However, it uses 1/2139 high-temperature combustion gas of water, 1/1700 superheated steam, and 1/1517 high-temperature carbon dioxide to generate rotational output and bring the power close to 1/2139 kg weight m / sec of water. As a rotating output, power generators, vehicles, ships and airplanes are driven. At nuclear power plants and thermal power plants around the world, the seawater temperature is increased by the total amount of heat used, that is, 80 to 160 times the amount of steam used. The seawater temperature has been raised by 7 degrees Celsius, for example, phytoplankton required to produce 1 kg of fish in the sea near Japan has been killed, and the sardine population has been reduced to 1/200 by the food chain. 10 ice cubes It melts around the year, and the sea level rises by 5 to 6 meters, and a typhoon with a sea surface temperature of 48 degrees and 300 meters / second is expected. There is an urgent need to invent various kinds of engines.

  For example, the temperature of seawater has risen to increase the danger of methane hydrate decomposition and extinction of mankind, and exhausted all used combustion gases and CO2 to the atmosphere, increasing the risk of global warming and extinction of mankind. 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 The temperature rises 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 1/1700 of water, unit The power of the moving blade area kg weight m / sec is close to 1/1700 of water, the superheated steam velocity is blocked by the stationary blade, the direction of deceleration is changed, and the deadly stupid rotation output is injected into the moving blade. The power plant does not use the mass of combustion gas at all. In addition to the stupid rotational output, various rotational output drive devices such as thermal power plants, vehicles, ships and airplanes exhaust all used combustion gases and CO2 into the atmosphere, resulting in global warming. There are many critically stupid parts that accelerate the process, and there are no inventions around 100 years ago.

  The existing gas turbines and jet aircraft are improved by the obsolete invention when it is sufficient to generate rotational output and injection propulsion output, and the compressed air velocity by the moving blade is blocked by the stationary blade and is repeatedly converted to decelerated air pressure. Compressed air, and generated a rotational output with a high-temperature combustion gas whose atmospheric pressure weight is 1/2139 of water. In addition to the deadly stupid rotation output that blocks the gas velocity with the stationary blade, changes the direction of deceleration and injects it onto the moving blade, and the deadly stupid rotation output that does not use the combustion gas heat at all, the atmospheric pressure weight is Generates jet propulsion output with high-temperature combustion gas of 1/2139 of water, brings the power of kg of injection propulsion output close to 1/2139, and is used in thermal power plants, vehicles, ships and airplanes Large amount of high temperature combustion gas and CO2 And discharged into, a very fatal stupid part to accelerate the global warming many, invention the number there is a background art becomes enormous, such as 100 years.

  Existing gasoline engines and diesel engines improve the obsolete invention when it is sufficient to generate rotational output, and use a volume that does not consider a rational configuration at all. 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 there are background technologies that will increase the number of inventions for 100 years.

He decided to invent the theoretical best engine in 1958 and 1980, and started prototyping at the contract of the Okayama Regional Invention Center in 1963 and continued to make the prototype himself, but it is very difficult to prototype the engine. Therefore, in February 1982, we started requesting cooperation from a large number of large domestic companies, 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 useless invention was found. 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, and US Pat. No. 6,263,664. 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. 2005-247383, 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. there is.

  As explained in the background art, the inventions of existing power generation technologies, vehicles, ships, airplanes, and rockets have many stupid parts, and thermal power plants and nuclear power plants in the existing world Raise seawater surface temperature, raise seawater surface temperature 80 to 160 times the amount of generated steam without limit to 7 degrees Celsius, melt ice in Antarctica etc. around 100 years, and raise sea level 5-6m Increased the risk of typhoon creation, such as 300m / s, and started decomposing when the seawater temperature rises 2 to 3 degrees, increasing the risk of methane hydrate decomposition and extinction of humans. Plankton is drastically reduced, the sardine population is drastically reduced to 1/200, etc. by the food chain, existing updrafts are amplified and downdrafts are increased, unbounded heavy rain, heavy snow, typhoon wind speed, tornado, seasonal wind speed and cold wave And heat waves Has been started, so that the generated mercury exhaust temperature can be repeatedly recovered and reused at 230 degrees Celsius, and all of the partial unnecessary heat can be recovered and used as hot water of 300 degrees Celsius or less, as well as permafrost methane and methane There is a challenge to prevent the extinction of mankind by injecting it into hydrate and evaporating and recovering methane and no rise in seawater temperature.

  In addition to using the combustion gas mass output at all, the existing steam turbine uses the combustion gas calorific power output to generate rotational output with superheated steam whose atmospheric pressure weight is 1/1700 of water. Since kg weight m / sec is close to 1/1700 of water, stationary blades are provided in multiple stages and weighed in multiple stages, the steam speed is reduced, and the output is close to 1/100. The superheated steam explosion speed is converted to mercury explosion speed, and the rotary power generation of the vertical all-blade mercury turbine 8H or all-wheel impeller mercury turbine 8E that completely abolished the stationary blades is generated. 1700 * 13.55 times that of the existing steam turbine = 23,000 times, generating the rotational output of the vertical all-blade gas turbine 8A or all-blade propeller gas turbine 8a with the combustion gas mass output to generate electricity Turn off all combustion gas exhaust It approaches 0 degrees and is recovered as cold hot water or combustion gas dissolved water after use as the largest cold combustion gas utilization, and hot water, cold combustion gas, cold water, or CO2 + sulfur dioxide, which is a by-product of power generation and has a manufacturing cost of approximately 0, is collected. There is a problem that the combustion gas dissolved water that is included is effectively used, etc., and the same fuel amount approaches the 100 times rotation output of the existing steam turbine.

  In areas where water is scarce in the process of recovery and use as hot water, distilled water and salt are produced using hot water of 300 degrees or less and seawater desalination equipment, etc., and sold to customers, usually with hot water pipes and hot water tanks. Supplying water to consumers for use in household and commercial heating equipment, agricultural greenhouse heating, drinking water production equipment, washing / drying machines, dishwashers, various cooking equipment, bathhouses, hot water pools, etc. , Chilled water is supplied to customers through chilled water tanks and chilled water pipes, and is used to manufacture and sell refrigeration equipment, refrigeration equipment, ice making equipment, cooling equipment, etc. Dissolved water is used for the production of cold and hot water, and in the process of fixing combustion gas dissolved water such as CO2 to leftovers or combustible garbage, biomass and energy are extracted to produce fertilizer, and as power generation fuel or fertilizer, etc. Use or low temperature combustion on the sea floor Dissolving water, supplying nitrogen and oxygen, growing algae, etc., and proliferating phytoplankton necessary for the birth of 1 kilogram of fish, such as increasing the production of seaweeds and seafood, etc. there is.

  Existing gas turbines and jet engines have a problem of refusing the compressed air speed by moving the blades with the stationary blades and repeatedly converting them into air pressure, which is a very wasteful low-pressure air compressor, In the process of generating rotational output with high-temperature combustion gas, the combustion gas velocity is blocked by the stationary blade and decelerated, and the direction is changed and repeated injection to the moving blade. As the rotational output of the combustion gas mass output, the atmospheric pressure power kg kg m / s is brought close to 1/2139 of water, and all the high-temperature combustion gas and CO2 used are discharged into the atmosphere, so it is not adopted and burned Gas calorific power output (high-temperature mercury 1d explosion speed * mercury injection pump 6Z) + superheated steam speed converted to a non-superheated steam simplified vertical blade mercury turbine 8H to drive the full blade combustion section 30X Driving Then, the atmospheric pressure work rate of the rotation output is 2139 * 13.55 times that of the existing gas turbine = 29000 times, the theoretical best rotation output is obtained, and superheated steam and combustion gas are injected from the combined engine injection unit 78K. There is a problem of preventing global warming by making CO2 and other combustion gases into dissolved water mixed with steam and reducing CO2 exhaust to zero.

  Existing gasoline engines and diesel engines release the maximum energy near the dead point or near the dead point where rotation output is not generated, and the release energy is less than 1/6 for a perfect machine that generates rotation output 90 degrees after the dead point. It produces a rotational output that is reduced to a low level and exhausts all the high-temperature combustion gas and CO2 used to the atmosphere, making it ideal for non-adoption of engines. However, if it is used exclusively for compression of air or the like, the dead point becomes the maximum advantage, and the piston upper gap is brought close to 0 to recover the heat exhausted by 230 degrees of mercury exhaust as a theoretically best heat pump. For example, 1/30 * 1 / 30 * 1/30 = 1/27000 Volumetric compressed air and so on become possible, so it is used as an 8 types of energy storage compressor 20X for various purposes, and unlimitedly high pressure compression high pressure combustion heat exchange cooling combustion and exhaust It can be divided into, for example, mercury explosive force of 600 to 800 degrees saturation pressure or higher + 300MPa combustion gas explosive force by recovering and using the amount of heat to the maximum, and the mercury velocity is accelerated by high-temperature mercury 1d + mercury injection pump 6Z, and high-temperature combustion gas The output is 2139 * 13.55 times = 29,000 times rotation output, making it easy to use at low speed and making it easy to make small and large output.

  230 degree mercury exhaust heat quantity, intake air recovery compression heat recovery, high pressure compression high pressure combustion heat exchange cooling combustion without limit, exhaust heat quantity is recovered to the limit as theoretical best rotation output + theoretical best heat pump 1G, combustion gas calorific value Divided into output + combustion gas mass output, high-temperature mercury injection pump 6Z explosion speed + high-pressure high-temperature superheated steam explosion speed + high-pressure low-temperature combustion gas explosion speed, high-pressure low-temperature combustion gas explosion speed is used to accelerate the mercury velocity, high temperature The whole blade combustion section 30X including the vertical all blade mercury turbine 8H is driven by the mercury injection pump explosion speed, and the combined engine injection section 78K or the high pressure / high temperature / superheated steam explosion speed + high pressure / low temperature combustion gas explosion speed and fuel are driven. Driving the water jet 78M, various water-injecting ships, various water-injecting combat ships, various air-injecting ships, various air-injecting combat ships, various air Aircraft carriers, various air-injected airplanes, various air-injected combat planes, various spacecrafts, various air-injected flying ships, various air-injected combat-flight ships, various air-injected flying cars, and various vertical rising verticals The most efficient descent airplanes, various vertical ascending vertical descent combat airplanes, various space-returning parent airplanes, various air transport mobile devices, various supersonic airplanes, and everything that can be driven by engines There are challenges.

  Thermal power plants and nuclear power plants in the existing world have raised the seawater temperature 80 to 160 times the amount of steam generated by 7 degrees Celsius, increasing the danger of human extinction, so 8 types of reciprocating engines are dedicated to compression Compressed at high pressure by the energy storage compressor 20X, for example, 1/30 * 1/30 * 1/30 = 1 / 27,000 volume compressed air, etc. The high-temperature mercury explosive force of combustion gas calorie output + combustion gas explosive force of combustion gas mass output is divided into high-pressure high-speed high-temperature mercury 1d by a high-temperature mercury injection pump 6Z that can perform the highest-speed injection. The injection acceleration with acceleration is added, the atmospheric pressure power is increased to 1700 * 13.55 times = 23,000 times that of superheated steam, and all blade impeller mercury turbine 8E or vertical all blade mercury turbine 8H is brought to the limit. Easy Sturdy and high output, the most efficient rotating contact as the rolling contact with mercury with the maximum surface tension, the heat of the mercury exhaust generated by the heat pump is 230 degrees, the heat amount is repeatedly used and the partial unnecessary heat amount is 300 degrees Celsius It recovers and uses heat as below, for example, for recovery of methane, postponing the rise of seawater temperature and ending extinction of humans.

  When mercury with a critical temperature of 1478 degrees and a critical pressure of 1652 atm is injected in the same manner as a steam turbine at 600 to 800 degrees, the exhaust temperature of the steam turbine is 30 to 40 degrees and the exhaust temperature of all turbine mercury turbines is 220 to 240 degrees. The intake air is heated by the best heat pump 1G, and a large amount of high-pressure compressed air and enormous heat recovery are repeatedly used. High-temperature mercury 1d at 600 to 800 degrees is most easily injected at high speed by the mercury injection pump 6Z. In response to the saturation temperature drop in the process of generating the pressure temperature drop and rotating output, a part of the high-temperature mercury 1d is vaporized and expelled to return to the evaporation heat and the high-temperature mercury 1d speed, and the liquid mercury is accelerated most efficiently by increasing the volume. In addition, all blade mercury turbines are driven by rolling contact of mercury with the maximum surface tension. By driving the vertical all-blade gas turbine 8A or all-blade propeller gas turbine 8a with the combustion gas mass explosive force, the combustion gas exhaust temperature can be approached to -273 degrees as much as possible, and power generation with the maximum amount of cold energy can be generated. It is possible to dissolve the combustion gas after cold recovery in water and use it as a combustion gas dissolved water for various purposes, making it a facility for supplying heat, electricity and cold.

  The existing jets are not adopted because they are theoretically difficult to improve. In the case of injection propulsion, high-pressure compression is performed by the energy storage compressor 20X dedicated to the compression of eight types of reciprocating engines, and the main combustion chamber is also used as a reduced diameter main combustion chamber. Endlessly high pressure combustion heat exchange with heat exchanger 1 Cooling combustion for a long time, divided and used for combustion gas calorie output + combustion gas mass output, and most of the vertical turbine blade turbine rotation output is mercury exhaust temperature In the combustor 1Y of the combined engine injection unit 78K, the compressed air is maximized by using it for recovery at around 230 degrees, and most of the compressed air is used for increasing the superheated steam to increase the combustion gas and superheated steam with a large amount of remaining oxygen. Combustor 1 in the process of injecting fuel into 24-300 MPa combustion gas, approaching the theoretical air-fuel ratio combustion, greatly increasing the injection propulsion output, and simultaneously injecting superheated steam at 300-400 degrees 24-400 MPa, etc. The superheated steam reservoir 95c is disposed on the outer periphery of the gas heater to heat the superheated steam to enable high-temperature combustion, and both the superheated steam injection propulsion output and the combustion gas injection propulsion output are increased. The mixture is stirred and cooled to the atmosphere to produce combustion gas-dissolved water, and CO2 and other combustion gas emissions are minimized to prevent global warming.

  The existing gasoline engine and diesel engine cannot be improved to the theoretically best engine, but the reciprocating piston is used exclusively for compression, and the dead center is reversed to the maximum advantage. The storage compressor 20X, the piston top gap is brought close to 0, 1/30 * 1/30 * 1/30 = 1/27000 volume compressed air, etc. are possible, the most efficient generation of mercury driven rotation output The air is efficiently compressed, and most of the exhaust heat is recovered and utilized by the pre-compression compression chamber / heat exchanger 1A by the heat pump 1G, and the high pressure combustion heat exchange cooling combustion is performed without limitation in the reduced diameter compression chamber mercury heat exchanger 2Z. , High temperature mercury explosive power + 40 degrees or more 24 to 300MPa combustion gas explosive power divided and stored, high temperature mercury 1d is accelerated most efficiently by mercury injection pump 6Z, and rolling contact with mercury with maximum surface tension Drive all-wheel impeller mercury turbine 8E or vertical all-blade mercury turbine 8H, and increase the rotational output atmospheric pressure power kg weight m / sec to 2139 * 13.55 times = 29,000 times that of high-temperature combustion gas Therefore, the generators, vehicles, ships, and airplanes are driven most efficiently, and the maximum amount of cold energy is recovered by the combustion gas mass explosive force that drives all rotor blade gas turbines. Etc. to prevent global warming.

  Even the space shuttle of the rocket technology with the least improvement point injects high-temperature carbon dioxide of 1/1517 weight of atmospheric water and brings the reaction rate kg weight m / second to 1/1517 of water. In addition to adding high-pressure high-temperature water injection like a bottle rocket, low-cost liquid fuel and air suction injection combustion is added in the air, and high-pressure high-temperature is added to the outer periphery of the rear combustor 1Y and the combustion chamber 1Z with low-cost output in the air. A water container is provided to enable a significant increase in the reaction caused by the combustion of the combustion chamber 1Z at a significantly high temperature. The injection pressure of the high-pressure high-temperature water 52b is increased and injected in a vacuum or the like. Inhalation and high-pressure injection combustion of the fuel is performed by the fuel injection pump 1D, the low-cost explosive force is increased as much as possible to increase the injection propulsion output, and mercury is injected before the first high-temperature carbon dioxide injection, Early The dynamic work rate approaches 1517 * 13.5 times that of high-temperature carbon dioxide = 20,000 times, and the initial reaction is 5,000 times as long as the 1/4 to 1/40 speed injection. Double injection time increases, mercury recovery is possible, and the simplest and strongest rear combustor 1Y that makes the combustion gas combustion pressure in the combustion chamber 1Z the intake pressure of the fuel injection pump 1D, etc. Will increase.

  In order to accelerate the mercury with the maximum surface gravity and specific gravity by adding various mercury injection pumps 6Z, the high-pressure, high-speed, high-temperature mercury of the various mercury injection pumps is accelerated by adding gravity acceleration in a vacuum vertically below the mercury explosion force. Rolling contact in the process of acceleration generates rotational output with minimum friction loss, and drives the vertical type all-blade mercury turbine and all-blade flywheel mercury turbine most efficiently, theoretically best such as 100 times rotation output with minimum friction loss With the maximum rotation output, the generators, vehicles, ships and airplanes are rotated and driven most efficiently, which is also an excellent military technology.

  Because the combustion gas mass explosive force such as a very large amount of ultra high pressure is used to drive the vertical all-blade gas turbine 8A and the all-blade pusher gas turbine 8a, the most efficient heat, electricity, and cold supply facilities are driven. In other words, it maximizes the amount of cold energy recovered by maximizing the amount of cold energy recovered, cooling the whole city and reversing the heat island.

  Various superheated steam rocket nozzles, various combustion gas rocket nozzles and mercury injection pumps are improved, the maximum friction loss generation part is shortened, and the most efficient superheated steam, various combustion gases, and gravity-maximum mercury are accelerated most efficiently. The vertical type moving blade mercury turbine and the full moving blade propeller mercury turbine are driven well, and the combined engine injection unit 78K is driven by superheated steam or combustion gas, so the combined engine injection unit is driven most efficiently. The best and most powerful propulsion propulsion output and 10x speed in flight in a vacuum, and the most efficient in the military technology by driving and propelling ships, airplanes and spacecrafts most efficiently.

  Improved to various superheated steam rocket nozzles, various combustion gas rocket nozzles and various mercury injection pumps, shortening the maximum friction loss generation part, accelerating various superheated steam, various combustion gases and mercury most efficiently Drive all-blade mercury turbines and all-wheel flywheel mercury turbines to drive water jet 78M, drive water jets most efficiently, and drive ships at 10 times the theoretical best jet propulsion output, etc. There is an effect to.

  8 types of energy storage compressors 20A to 20B to 20C to 20D to 20E to 20F to 20G to 20H by generating high-speed high-temperature mercury with a mercury injection pump to generate the most efficient rotational output and setting the exhaust temperature to around 230 degrees. Therefore, using the energy storage compressor 20X selected according to the application, the air recovered from the exhaust around 230 degrees is compressed one or more times, and heat recovery is repeated one or more times. The amount of heat supplied is recovered and used with hot water of 300 degrees C or less, and methane hydrate is vaporized and recovered with hot water with a manufacturing cost of approximately 0. There is an effect to stop.

  Infinitely high pressure combustion heat exchange cooling combustion, divided into superheated steam explosive power and mercury explosive power + combustion gas explosive power and used, so superheated steam is always held and fired at any time to extinguish fire In addition to being able to operate with high-temperature mercury possessed heat + exhaust heat even when the fuel runs out, a large amount of superheated steam explosive power + combustion gas explosive power can be injected and flying in a vacuum. There is an effect that can be made to airplanes and space return aircraft.

  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. Also, for the very difficult brain invention and to explain the intended place and expectation concretely clearly, the idea is explained with hypothetical figures, but the correct answer is not limited to hypothetical figures as experimental figures. 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 A-type coalesced engine combustion section 29A in FIG. 1 is an explanatory diagram including the plane explanatory views of FIGS. 1 to 4. As shown in FIG. 1, an existing multi-cylinder gasoline engine or diesel engine is used as an energy storage compressor 20A exclusively for compression. For example, 1/30 * 1/30 * 1/30 = 1/27000 volume compressed air is possible by using the multi-cylinder as one or more pre-compression compressors to main pressure compressors. , Infinitely high-pressure combustion heat exchange cooling combustion, divided and stored into mercury explosive force of combustion gas calorie output + combustion gas mass explosive force, and all blade impeller mercury by mercury explosive force + mercury injection pump 6Z injection speed In the process of driving the turbine 8E, the mercury exhaust temperature is set to around 230 degrees using the same vacuum as that of the existing steam turbine, and the exhausted heat amount 5A is heat-exchanged and recovered by the vaporized hot air recovery device 2B. One direction including a check valve 97, in which a large amount or a small amount of air 28a is sucked from the intake valve 28 in accordance with the purpose of use and compressed by the expanded piston 21 of the expanded compression chamber 10a to 800 to 1200 degrees Celsius. With the reduced diameter compression chamber mercury heat exchanger 2Z or the preload compression chamber heat exchanger 1A of the air flow path heat exchanger 9, the heat exchange air is cooled with the high-temperature mercury 1d of the mercury tube at least once and compressed, and is about 300 degrees. Air 28a is cooled and compressed.

  The exhaust heat quantity 5A is recovered and compressed, heat is recovered as 800 to 1200 degrees air 28a temperature, and the operation of the cooling and compression heat recovery is repeated to about 300 degrees thereafter, and the theoretical best heat pump 1G is configured, and the final reduced diameter main combustion Fuel injection combustion is possible at any time during the cooling process in the chamber / heat exchanger 1, high-pressure combustion heat exchange cooling combustion is performed without limitation, and high-temperature mercury 1d + 300 degrees 24-300 MPa combustion gas 49 explosions over 600 to 800 degrees saturation pressure In the process of driving all blade impeller mercury turbine 8E, the high-speed high-temperature mercury 1d injected from the mercury injection pump 6Z is accelerated vertically downward at the mercury explosion speed, and gravity acceleration is added in vacuum. As an acceleration, atmospheric pressure gravity work capacity kg weight m / second was increased to 1700 * 13.55 times = 23,000 times of water vapor, and injected to all-wheel impeller mercury turbine 8E. In the process, 8E8E is synchronized and meshed, and vertically and vertically installed in multiple stages, or 8E is vertically provided with multiple injection walls and vertically and vertically installed in multiple stages. The contact generates the rotational output with the minimum friction loss, and the maximum rotational output of the theoretical best by high temperature mercury 1d with the maximum vaporization explosive force surface tension.

  A vaporized hot air recovery device 2B and an air extractor 51 are provided in the exhaust chamber, and the exhaust heat quantity around the mercury exhaust temperature of 230 degrees is recovered by the intake air 28a of the intake valve 28, and the intake air temperature is set to 60 to 200 degrees or the like. High-temperature mercury 1d compressed at a compression pressure of 800 to 1200 ° C. or higher by the mercury pump 1E to be equal to or higher than the saturation pressure after heating is supplied to the reduced-diameter compression chamber mercury heat exchanger 2Z and heated with compressed air 800 to 1200 ° C. to 600 The high temperature mercury 1d is raised to ˜800 degrees, etc., and is used in the same vacuum as the steam turbine by the air extractor 51, and the vaporization explosive force is maximized by setting the exhaust gas saturation temperature of the high temperature mercury 1d to around 230 degrees. The maximum speed is injected from the mercury injection pump 6Z, expanded in the axial direction by the mercury injection nozzle 6b, and injected into the all-wheel impeller mercury turbine 8E.

  The existing moving turbine turbine 8E is provided at an optimum interval according to the injection mass by appropriately approaching or meshing with each other in a noncontact manner, and synchronized with the water pump / magnetic frictional power transmission device 55, etc. The turbine blades 8c to 8c are projected in the radial direction in parallel with the outer peripheral axis direction of the cylindrical cylinders 8e to 8e. The turbine blade is a mercury turbine 8E with a straight turbine blade with the tip bent into a streamlined shape. By coupling to the horizontal crankshafts 16 to 16, the high-speed mercury 1d boosted to the optimum pressure in the tangential direction + vertically downward direction of all the moving blade propeller mercury turbines 8E to 8E is injected and accelerated, and the combined engine combustion unit 29A is Drive to reduce the amount of supplied heat to the limit, for example, supply the amount of heat supplied to the tap water temperature 52d of 300 degrees Celsius or less, sell it to consumers as a by-product of power generation, and use the tap water temperature 52d close to 300 degrees Celsius Manufacture and sell various types of commercial and household heating equipment, cooking equipment, hot water equipment, dishwashers, washing dryers, and tap water heating / piping buildings that aim to consume 1/10 of the power In this way, the risk of fish extinction and the risk of human extinction due to methane hydrate decomposition are reduced without any increase in seawater temperature.

  Depending on the region, seawater is desalinated with tap water temperature 52d, and manufactured and sold as tap water and salt to eliminate serious water shortage areas. Make heat, electricity and cold supply ship near the center, collect hot water below 300 degrees Celsius, add insulated pipes to existing technology and inject it into methane hydrate, In the process of evaporating and recovering with a conical roof type enclosure and using it as fuel, too much methane is exhausted by a full-blade impeller mercury gas turbine 8G exhaust and multi-cylinder energy storage compressor, which is close to 0 degrees in FIG. With 20X, multi-stage compression heat recovery multi-stage cooling, store in liquid or gas as appropriate, and transport to land with electricity for sale.

  In the process of driving the full-blade flywheel mercury turbine 8E shown in the side view of FIG. 1, high-temperature mercury 1d heated to 600 to 800 ° C. is supplied to the cylindrical mercury reservoir 95D and selectively improved from various existing pumps. The pressure is increased to an optimum pressure such as 300 MPa or more by various mercury injection pumps 6Z, and the mercury injection nozzle 6b expands and expands in the turbine axial direction in the injection process, so that the turbine blade 8c acts evenly. As shown in the figure, the tip is appropriately curved in parallel with the axial direction to generate the most efficient rotational output, and the side plate 8d can be engaged with the tip of both sides of the cylindrical body 8e and the turbine blade 8c so that the high temperature mercury 1d can be engaged. Enclosed in the turbine blades to generate rotational output, meshed with the all-wheel impeller mercury turbine 8E8E and added vertically in multiple stages according to the application, or provided with injection walls It was added to the multi-stage the entire rotor blade flywheel mercury turbine 8E in accordance with the vertical applications Te, and to Zendotsubasa flywheel mercury turbine 8E tailored to the application.

  In the process of driving the all-blade propeller gas turbine 8a of FIG. 1 side view of FIG. 2, a combustion gas 49 of 40 to 300 degrees is supplied to the cylindrical combustion gas reservoir 95a according to the application, and a plurality of combustion gases are supplied. When the control valve 24 is controlled to be opened, the combustion gas 49 is injected from the combustion gas rocket nozzle 6M, and when the amount of cold collected in the injection process is maximized, the combustion gas 49 is cooled at the cooling rate injection pressure at the maximum, When the rotational output is increased with a small amount of cold collected, the combustion output 49 is burned into the combustor 1Y using a combustion gas 49 of 300 degrees or the like, and the rotational output is increased by increasing the temperature and volume of the combustion gas 49. Thus, in the process of injection into the all-wheel impeller gas turbine 8a, the turbine blade is configured to inject from the combustion gas rocket nozzle 6M, expand in the axial direction at the nozzle injection portion 6a, and act equally on the turbine blade 8c. c is shaped to generate the rotational output most efficiently by suitably curving the tip in parallel in the axial direction, and the side plate 8d is fitted to the tip of both sides of the cylindrical body 8e and the turbine blade 8c so that the combustion gas can be engaged. The turbine blades are confined in the turbine blades to generate rotational output, and the all-blade bouncer gas turbine 8a8a is meshed and vertically added in multiple stages according to the application, or an injection wall is provided to provide a full-blade bouncer gas turbine. 8a is vertically expanded in multiple stages according to the application, and the all-rotor impeller gas turbine 8a is adapted to the application.

  In the process of exhaust generation of all rotor blade gas turbine gas turbines 8a to 8a, the exhaust of all rotor blade gas turbines 8a to 8a and the exhaust of mercury turbine gas turbines 8E to 8E are reliably separated, and the exhaust temperature − A rotational output is generated by the combustion gas 49 approaching 273 degrees, and the maximum amount of cold heat collected and the maximum rotational output are set according to the application. The combustion gas 49 of 40 to 300 degrees Celsius and 24 to 300 MPa is close to absolute 0 degrees, and CO2 And SO2 etc. can be separated and recovered as a solid due to a difference in melting point, and the exhaust heat quantity 5A is stored as the heat exchange cold alcohol 1C close to -100 degrees as the heat exchange cold alcohol 1C by the internal and external cold heat recovery devices 103b and 103b. Heat exchange with materials suitable for various types of business, household refrigeration equipment, various refrigeration equipment, various cooling equipment, various cooling equipment, and various Manufacture and sale of ice equipment and various water-cooled heat pipe buildings, etc., for example, cooling the whole city with water at 0 degrees etc. to heat-exchange tap water-cooled heat pipes, reversing the heat island phenomenon, melting combustion gas First, 52g of water is supplied to the seabed, and the algae grows and expands to seafood.

  The combined engine combustion unit 29A in FIG. 3 includes the crankshaft 16 horizontally in order to obtain a theoretically best heat pump 1G by using the vaporized hot air recovery device 2B to collect and use the mercury exhaust temperature around 230 degrees by the intake air 28a. In this way, mercury can be injected and accelerated vertically downward to drive the all-blade flywheel mercury turbine 8E. When the crankshaft 16 is provided vertically, it is connected to a horizontal turbine shaft by a known right angle joint gear or the like. In addition, it accelerates and injects mercury vertically downward to enable a large number of all-wheel impeller mercury turbines 8E to 8E to be driven, and the rotational output of the rolling contact with the addition of gravitational acceleration as the mercury output with the maximum gravitational maximum surface tension. The minimum atmospheric pressure work rate is 2139 * 13.5 times the high-temperature combustion gas = 29,000 times, and all of the moving blade propeller gas turbines 8a to 8a and 8E to 8E can rotate synchronously. A large number of water pump / magnetic friction power transmission devices 55 and the like are provided, and an optimum speed change is performed by the water pump / magnetic friction power transmission devices 55B to 55B, etc., and a large number of crankshafts 16 are rotationally driven to constitute an energy storage compressor 20A. This consists of a full-blade propulsion wheel mercury turbine 8E + all-blade pusher gas turbine 8a that has a large number of expanded pistons 21 and drives the combined engine combustion section 29A.

  Fig. 4 All rotor blade combustor 30A aiming for small size, light weight and large output is adapted to the use of annular mercury reservoir 95D provided at the upper part of the circumference of the uppermost nozzle 6 circumference of all the rotor blades of vertical turbine all turbine blade 8H. From the multiple mercury injection pumps 6Z, the high-speed mercury 1d with the maximum work capability is directed into the vacuum and the acceleration of gravity acceleration of mercury is added, and the atmospheric pressure gravitational work rate kg weight m / sec is 1700 * of steam. 13.55 times = 23,000 times, in the process of generating the rotational output of the vertical all blade mercury turbine 8H, by the mercury injection nozzle 6b by the high temperature mercury 1d with the maximum vaporization explosive force surface tension maximum gravity. Rotational output is generated by rolling contact in the circumferential direction, and the vertical all blade mercury turbine 8H is driven to minimize friction loss, thereby driving the inner blade group 60C and the outer blade group 60D rotating in opposite directions. 1/10 to 1/20, etc. Enables small and simple output and weight reduction, and in the process of exhaust, high-temperature mercury 1d exhaust temperature around 230 degrees is recovered by the vaporized hot air recovery device 2B and the maximum amount of heat is recovered by the intake air 28a. Configured, the reduced diameter main combustion chamber / heat exchanger 1 is used as the reduced diameter compression chamber mercury heat exchanger 2Z, making it a full blade combustion part 30A among 8 types.

  Of all the eight types of all blade combusting units 30X, the whole blade combusting unit 30A is provided in the process of rotating vertically with a vertical crankshaft 16 by a vertical crankshaft mercury turbine 8H. The rotation of the inner rotor blade group 60C and the outer rotor blade group 60D rotating in opposite directions is concentrated on one axis by the water pump / magnetic friction power transmission device 84 and the like, and the water pump / magnetic friction power transmission device 55B is optimal. As the crankshaft 16 of the rotational speed, pre-compression compression or main-pressure compression is performed using an energy storage compressor 20A dedicated to compression as in FIG. 1, for example, 1/30 * 1/30 * 1/30 = 1/7000 volume. Enables compressed air, etc., infinitely high-pressure combustion heat exchange cooling combustion, divided into 600-800 degrees saturation pressure or higher high-temperature mercury 1d + 40-300 degrees Celsius 24-300 MPa combustion gas explosive force, and compressed High temperature mercury 1d explosive force of combustion chamber mercury heat exchanger 2Z and combustion gas 49 mass explosive force. Combustion part using energy storage compressor 20A is all blade combustion part 30A, water repellent action according to application 3G is installed to reduce friction loss with mercury, and high-temperature mercury 1d explosive power is accelerated vertically downward by mercury injection pump 6Z injection pressure.

  The vertical all-blade mercury turbine 8H is provided with an inner shaft device 60A having an inner blade group 60C and an outer shaft device 60B having an outer blade group 60D in a turbine outer box 77a. It is configured to rotate in opposite directions by the heavy reversal magnetic friction power transmission device 84 and the like, and the inner rotor blade group 60C and the outer rotor blade group D are provided with a water repellent action 3G to reduce friction loss, and as fast as possible. The most efficient rotation by large mass mercury velocity, the number of blades of the inner blade group and the outer blade group is set easily and ruggedly optimally according to the respective mass velocity, and from the mercury injection pump 6Z injection explosive force, High-speed mercury 1d is sprayed and accelerated vertically downward, aiming at a small, simple, large output such as 1/10 to 1/20 of all blade impeller mercury turbine 8H and weight reduction, and 10 to 30 stages of all rotor blades. Select and install to always rotate with all rotor blades , Generating a rotational output that makes maximum use of gravitational acceleration up to vacuum, and creating a full blade combustion section 30A that drives the vertical all-blade mercury turbine 8H to produce generators, automobiles, airplanes, and ships. Various rotation outputs such as

  Evaporation hot air recovery device 2B is provided in the exhaust chamber of high-temperature mercury 1d in the exhaust process, and exhaust heat quantity 5A such as mercury exhaust temperature 230 degrees is recovered by intake air 28a, and air 28a at 60 to 200 degrees is intake valve 28 + Energy storage compressor 20A sucks and compresses, 800-1200 degrees, etc., heat recovery and cooling by reduced diameter compression chamber mercury heat exchanger 2Z, and after the second time, cooling air of around 300 degrees, etc., is 800-1200 degrees, etc. The combustion gas 49 is cooled with tap water temperature 52a, the water supply pipe 3 and the superheated steam 50 to a temperature suitable for the application, stored at around 40 to 300 degrees, 24 to 300 MPa, etc. Mercury 1d temperature is set to 230 degrees, etc., and mercury pump 1E is used to send mercury to reduced diameter compression chamber mercury heat exchanger 2Z, heat exchange heat and store at the highest usable temperature such as 600 to 1000 degrees, When the gas extractor 51 is driven to raise the vacuum and is used for injection propulsion, the condensed pump 1F and the water supply pipe 3 feed water to the reduced diameter main combustion chamber / heat exchanger 1 and divide it into superheated steam 50. Use save.

  The heat pump 1G with the best recovery theory is configured with a heat pump 1G with an exhaust heat amount of 5A, such as a mercury exhaust temperature of 230 ° C. The supply heat amount of the same rotational output is set to the minimum target of 1/100, etc. In order to make a surplus, in the process of recovering suction compression heat by the energy storage compressor 20A, heat is recovered from the combustion gas 49 around 300 degrees as air temperature of 300 degrees or less or tap water temperature heat 52d such as 100 degrees, and is a by-product of power generation. In the danger zone of methane hydrate decomposition, it is injected into methane hydrate to recover methane hydrate that requires enormous heat and cannot be profitable with existing technology, aiming for 1/10 power consumption Various types of heating equipment, cooking equipment, hot water equipment, commercial dishwashers, washing dryers, and tap water heating and plumbing buildings , Etc., manufactured and sold as drinking water with the action of pearl barley, brown rice, green tea, barley, pear tea, namban millet, dodomi, habu tea, chicory, evening primrose, loquat leaves, vitamin C, etc. Prevent the rise and reduce the danger of human extinction.

  5 uses a vertical all blade vane turbine 8A instead of the vertical all blade mercury turbine 8H of FIG. 4, and when using a single shaft, Only the blade gas turbine 8A is added to generate combustion gas mass output. In order to maximize the amount of cold heat recovered and the maximum rotational output according to the application, the mass explosive force of the combustion gas 49 mass, such as 24 to 300 MPa around 40 to 300 degrees including the cooling heat recovery, is applied to the vertical rotor blade gas turbine 8A. An inner shaft device 60A having an inner moving blade group 60C provided with a water repellent action 3A and an outer shaft device 60B having an outer moving blade group 60D are provided in the turbine outer box 77a, and a water pump and double reversal are provided. As a configuration that rotates in opposite directions by the magnetic frictional power transmission device 84 or the like, a plurality of combustion gas rocket nozzles 6M provided in the upper part of the nozzle 6 are provided in an annular combustion gas reservoir 95d and the combustion gas 49 explodes. The power is supplied, and the combustion gas 49 explosive force of the combustion gas rocket nozzle 6M is expanded in the circumferential direction by the nozzle injection part 6d. As the all-blade combustion section 30A including the vertical all-blade gas turbine 8A, which enables a small, simple, large output, such as 1/10 to 1/20 of the bucket turbine gas turbine 8a, and weight reduction, various heat and electricity Rotating output of equipment for supplying heat and cooling, various automobiles, various airplanes, various ships, etc.

  In the process of generating the maximum rotation output and the maximum amount of cold recovery, the combustion gas 49 of about 300 degrees is cooled to about 40 degrees by the superheated steam 50 etc. of the water supply pipe 3, and the vertical all blade steam turbine 8B + vertical type In the process of driving the whole blade gas turbine 8A, the combustion output of the vertical combustor blade 8A is maximized by maximizing the combustion amount of the combustor 1Y, and the combustion amount of the combustor 1Y is made zero by maximizing the combustion output Maximizes the recovery of all blade gas turbine 8A cold energy. Combustor 1Y is added to combustion gas rocket nozzle 6M, combustion gas control valve 24 is opened, combustion gas 49 explosive force such as 40 degrees 24 to 300 MPa is supplied to combustor 1Y, and fuel control valve 25b is opened fuel. Injection pump 1D injection Combustion or injection from combustion gas rocket nozzle 6M without combustion, maximizing rotational output of vertical all blade gas turbine 8A or maximizing the amount of cold recovery, and providing gas extractor 51a in gas exhaust chamber 5c Installed and driven, equipped with internal and external cold heat recovery devices 103b and 103b, heat exchange with alcohol 1C-store close to 100 degrees, heat exchange with materials suitable for applications such as tap water cooling heat 52e near 0 degrees Various commercial and household refrigeration equipment, various refrigeration equipment, various air conditioning equipment, various cooling equipment, various ice making equipment, various tap water cooling and heating pipe buildings, etc. Manufactured and sold, and the methane recovery facility stores and sells methane as a recovered liquid and gas as needed. Combustion gas recovered from cold heat is dissolved in water.

  6 is an embodiment of the energy storage compressor 20B. The difference from the whole blade combustion section 30A of FIG. 4 is that the energy storage compressor 20B is used instead of the energy storage compressor 20A. However, the vertical type all-blade mercury turbine 8H etc. are the same. Accordingly, the cylinder head 15 of the energy storage compressor 20A and the one-way flow path reduced-compression-chamber mercury heat exchanger 2Z including the check valve 97 and the one-way air flow path heat exchanger 9 are arranged to the left and right according to the application. The eight-way pendulum arm 40a such as US Pat. No. 6,119,650 increases the reciprocating motion of the piston by the crankshaft 16 twice, etc., and causes the enlarged-diameter piston 21 to reciprocate by the pendulum arm. The energy saving compressor 20B corresponding to the diesel engine is reduced by reducing the kinetic energy reduction loss due to the reciprocating motion of the existing diesel engine, approaching 0, and the water pump, the counter-rotating magnetic friction power transmission device 84, etc. and the water pump The vertical type moving blade mercury turbine 8H and the vertical crankshaft 16 are connected to each other via the magnetic friction power transmission 55B and the like, and the mercury control valve 25d is controlled to be opened. Mercury 1d is supplied to the mercury reservoir 95D, from a mercury reservoir 95D1 of mercury injection pump 6Z of the outer ring, and injected accelerated by adding a gravitational acceleration hot mercury 1d vertically downward.

  It is injected vertically downward from one or more mercury injection pumps 6Z on the circumference to drive the vertical all blade mercury turbine 8H and the all blade combustion part 30B including the energy storage compressor 20B to The crankshaft 16 driven by the type full-blade mercury turbine 8H is rotated, the crankshaft 16 is provided between the fulcrum 81a of the pendulum arm 40a (not shown) and the double-headed enlarged piston 21, and the crankshaft 16 is driven by the pendulum arm 40a. The reciprocating motion is expanded, the side pressure of the biston is reduced most easily, the weight is reduced, the loss of kinetic energy reduction due to the heavy duty reciprocating motion of the diesel engine is reduced, and the number of cylinders is increased to 2 cylinders + 2 cylinders to increase the number of cylinders. The magnetic frictional power transmission 55B or the like can be changed, and the air 28a recovered by the vaporized hot air recovery device 2B is compressed by the suction-expanded compression chamber 10a to be reduced in diameter. Heat exchange heating of high-temperature mercury 1d, etc. in the room mercury heat exchanger 2Z, and then fuel injection and combustion at any time in the process of enabling the compression heat exchange heating multiple times, the most heat supply and compression recovery of exhaust heat With efficient compression of mercury rotation output, the aim is to increase the rotation output of the same fuel quantity by 100 times, etc., and drive the vertical rotor blade mercury turbine 8H.

  7 is an embodiment of the energy storage compressor 20C, and the difference from the whole blade combustion section 30B of FIG. 6 is that the energy storage compressor 20C is used instead of the energy storage compressor 20B. And everything else was the same. Therefore, the energy storage compressor 20C is provided with the energy storage compressor 20B opposite to each other, and the reduced diameter compression chamber mercury heat exchanger 2Z is provided at the center and the left and right.・ The counter reciprocating motion of the piston by the crankshafts 16 and 16 is doubled by 40a and the reciprocating motion of the enlarged pistons 21 and 21 by the pendulum arm so that the side pressure of the piston approaches 0. Therefore, the energy storage compressor 20C corresponding to the large loss of the diesel engine is obtained by using the water pump / magnetic friction power transmission device 55 and the water pump / counter-reversing magnetic friction power transmission device 84 and the like. The vertical all-blade mercury turbine 8H and the vertical crankshafts 16 and 16 are connected, the mercury control valve 25d is controlled to open, and the mercury reservoir 95D is raised. The high-temperature mercury 1d is injected at maximum acceleration from the mercury injection pump 6Z, the high-temperature mercury 1d explosive force is used to accelerate and inject high-temperature mercury vertically downward, and the gravitational maximum mercury is added to the vacuum as an acceleration by adding gravity acceleration. Work capacity kg weight m / sec is 23,000 times that of water vapor.

  Atmospheric pressure work capacity kg weight m / second is set to 23,000 times the steam to drive the vertical all blade mercury turbine 8H, to drive the entire blade combustion section 30C including the energy storage compressor 20C, As the rotation of the crankshaft 16 driven by the vertical all blade mercury turbine 8H, the crankshaft 16 is provided between a fulcrum 81a (not shown) of the pendulum arm 40a and the double-headed enlarged piston 21, and the crankshaft 16 is driven by the pendulum arm 40a. The reciprocating motion of the diesel engine is expanded, the side pressure of the biston is reduced most easily, the weight is reduced, the loss of kinetic energy reduction due to the heavy weight reciprocating motion of the diesel engine is reduced, and the number of cylinders is increased to 4 cylinders + 4 cylinders to increase the number of cylinders. A water pump and magnetic friction power transmission device 55-55 etc. are provided so that the horizontal crankshafts 16-16 can be rotated synchronously by bending 90 degrees, and the vibrations are canceled to the limit by synchronizing the opposing reciprocating motion. The two-head enlarged pistons 21 to 21 are made closer to a large diameter such as 10 m according to the application, and can be changed by a water pump / magnetic frictional power transmission 55B, etc. The air 28a that has recovered the exhaust heat quantity 5A in the vaporized hot air recovery unit 2B is cooled by precompression compression heat recovery cooling or main pressure compression heat recovery cooling in the diameter expansion compression chamber 10a, and fuel is used at any time in the process of compression heat recovery cooling once or more It enables injection combustion, and divides it into high-temperature mercury 1d explosive force + combustion gas 49 mass explosive force, and drives vertical all blade mercury turbine 8H + vertical all blade gas turbine 8A.

    8 is an embodiment of the energy storage compressor 20D. The difference from the whole blade combustion section 30B of FIG. 6 is that the energy storage compressor 20D is used instead of the energy storage compressor 20B. The vertical type all-blade mercury turbine 8H, vertical type all-blade gas turbine 8A, etc. are all the same. Therefore, the cylinder head 15 of the energy storage compressor 20D and the one-way flow path reduced diameter compression chamber mercury heat exchanger 2Z including the check valve 97 and the one-way air flow path heat exchanger 9 are provided on the left and right as described above. The piston rod etc. of the existing gasoline engine is omitted, it is made simple and light, and the double-headed enlarged piston 21 is directly reciprocated by rotating the horizontal crankshaft 16 by bending it vertically or 90 degrees, and the expanded-compression chamber with the simplest structure The energy storage compressor 20D of 10a is used as a multi-cylinder and the piston diameter and the piston stroke are appropriately expanded, and the intake air 28a, in which the heat of exhaust gas 5A is recovered by the vaporized hot air recovery unit 2B, is pre-compressed to compressed. The exhaust heat quantity 5A can be recovered and used by the reduced-diameter compression chamber mercury heat exchanger 2Z, and the piston diameter and piston stroke are appropriately reduced according to the application. It allows you to yield.

  A vertical all-shaft mercury turbine 8H and the vertical crankshaft 16 are connected to each other through a water pump and counter-rotating magnetic friction power transmission device 84 and the like, and a water pump and magnetic friction power transmission device 55B and the like, so that the gear can be shifted, and mercury control is performed. By controlling the opening of the valve 25d, the vertical all-blade mercury turbine 8H is driven in the same manner as in FIG. 6, and the all-blade combustion section 30D including the energy storage compressor 20D is driven. As the rotation of the crankshaft 16 driven by 8H, the double-headed enlarged piston 21 is directly reciprocated to reduce the side pressure of the biston most easily and reduce the weight, reduce the loss of kinetic energy, and increase the number of cylinders to 2 cylinders + 2 cylinders to increase the number of cylinders. The reduced diameter compression chamber mercury heat exchanger 2Z is also provided on both the left and right sides of the final compression stroke so that it can be ignited and burned at any time during the heat exchange cooling process. It is equipped with a reduced diameter main combustion chamber / heat exchanger 1 and pre-pressure compression chamber / heat exchanger 1A for injection propulsion, etc., and recovers 49 calories of combustion gas such as surplus around 300 degrees with superheated steam 50 or tap water. Also, the combustion gas 50 is used for propulsion, and it is also used as the whole blade combustion part 30X that uses tap water as tap water temperature 52d.

  9 is an embodiment of the energy storage compressor 20E. The energy storage compressor 20D is provided opposite to the energy storage compressor 20E to form the energy storage compressor 20E. The counter-reciprocating motion is synchronized to cancel the vibration, and one or more reduced-diameter compression chamber mercury heat exchangers 2Z are provided in the left and right and the center, respectively. It is used as 2Z, and the double-headed enlarged piston 21 diameter is made larger by canceling vibrations, or by the vertical all blade mercury turbine 8H + the vertical all blade gas turbine 8A in FIG. Can be driven in series, bend 90 degrees with a known gear joint to enable horizontal crankshafts 16 and 16, and have a large-diameter compression chamber 10a and 10a opposite to each other with simple structure to the limit. Part 30E Then, pre-compression compression to main pressure compression is performed in the expansion compression chamber 10a, and the high-pressure combustion heat exchange cooling combustion is performed in the contraction compression chamber mercury heat exchanger 2Z as much as possible. + Divide and save the combustion gas to 49 mass explosive force, and drive vertical type moving blade mercury turbine 8H + vertical type moving blade gas turbine 8A.

  Reduced compression chamber mercury heat exchanger 2Z is provided in the left and right and center final compression stages, and the other than the final compression stage is a preload compression chamber / heat exchanger 1A + reduced diameter compression chamber mercury heat exchanger 2Z. The whole blade combustion section 30E is configured to supply and compress the air 28a from which the exhaust heat quantity 5A has been recovered to the expanded diameter compression chamber 10a, and to burn the reduced diameter compression chamber mercury heat exchanger 2Z in the process of supplying and cooling high temperature air. And the reduced diameter compression chamber mercury heat exchanger 2Z is provided in the left and right final compression stages, the central final compression stage is the preload compression chamber / heat exchanger 1A, and the high temperature of the left and right reduced diameter compression chamber mercury heat exchanger 2Z. Supplying cooled air 28a to the air section and causing it to burn with high-temperature air and agitated fuel injection is the full blade combustion section 30F. And the reduced diameter compression chamber mercury heat exchanger 2Z is provided in the central final compression stage, the left and right final compression stages are preloaded compression chamber / heat exchanger 1A, and the high temperature of the central reduced diameter compression chamber mercury heat exchanger 2Z. Supplying cooled air 28a to the air section and causing it to burn with high-temperature air and agitated fuel injection is the full blade combustion section 30G.

  The generation of the air suction / injection output of the various jets of FIG. 10 mainly uses the various all blade combustion parts 30X of FIGS. 4 to 9, and the reduced diameter compression chamber mercury heat exchanger 2Z is used as the reduced diameter main combustion chamber combined heat. The exchanger 1 and the preload compression chamber / heat exchanger 1A are added, and the superheated steam 50 is heat-exchanged in the water supply pipe 3 to cool the combustion gas 49 to the lowest temperature. It is separated from the part 30X and simplified to the limit, and the entire blade combustion part 30X collects the exhaust gas 5A of the high temperature mercury 1d exhaust temperature 230 degrees to the limit, and heats the enormous intake air 28a as compressed 800 to 1200 degrees The recovery cooling is repeated, the high-pressure combustion heat exchange cooling combustion is performed infinitely in the reduced-diameter compression chamber mercury heat exchanger 2Z, the superheated steam 50 approaching 400 MPa and the low-temperature combustion gas 49 approaching 300 MPa are maximized, and all blade combustion Part 30X is a saddle type It is driven by a moving blade mercury turbine and the combined engine injection section 78K is driven by the superheated steam 50 or the low-temperature combustion gas 49, so that the combustion gas 49 pressure can be easily increased by high-temperature high-pressure air or the like depending on the flight speed. Combustion gas 49 that is less and close to compressed air is supplied from the combustion gas control valve 24 to the combustion gas reservoir 95a, fuel 1b is supplied from the fuel control valve 25b, and fuel injection low temperature is injected into the combustor 1Y by the fuel injection pump 1D. The combustion gas 49 is ignited and combusted, and the combustion gas 49 is injected at the maximum speed from the combustion gas injection rocket nozzle 6Y.

  Annularly provided on the outer periphery of the combustor 1Y, the superheated steam 50 in the superheated steam reservoir 95c is heated to enable high-temperature combustion of the combustor 1Y, and the air suction injection propulsion output of the combustion gas 49 is further increased. And the superheated steam rocket nozzle 6L to inject the air suction injection propulsion output into the theoretically best coalescence engine injection section 78K, reduce the friction loss by the water repellent action 3A of the rocket nozzle, streamlined coalescence With the engine injection unit 78K, aiming for a 10-fold reaction reversal of the existing jet aircraft, etc., the magnetic rotating power transmission device 76 provided in the cylindrical rotating unit 77G of the combined engine injection unit outer box 77F, the flying wing 38b and the flying tail 38c, and the known technology, The combined engine injection unit outer box 77F can be rotated 90 to 180 degrees or more according to the application, enabling vertical ascent, vertical descent and reverse injection, building rooftop, moon, stars, etc. As an airfield that can depart and depart, various spacecraft, various space return passenger aircraft, various space return parent planes, various supersonic jets, various supersonic jet fighters and various It generates air suction / injection output from various air suction / injection drive devices such as ultra-high-speed ships and various ultra-high-speed battle ships.

  The generation of air suction / injection output from various jets of the combined engine plane 38A in FIG. 11 is performed by connecting the reduced diameter compression chamber mercury heat exchanger 2Z to the reduced diameter main combustion chamber / heat exchanger 1 and the preload compression chamber / heat exchanger 1A. In addition, the superheated steam 50 is heat-exchanged in the feed water pipe 3 to cool the temperature of the combustion gas 49 to the minimum, and the all-blade combustion section 30X is driven by the vertical all-blade mercury turbine 8H alone. The unit 78K is divided and installed on the left and right sides of the flying wing 38b and the flying tail 38c, and the combined engine combustion unit 29X or the entire moving blade combustion unit 30X is divided and installed in the vertical wings 38d to 38d, etc. 78K is simplified to the limit according to the application, and fuel is injected and burned from a fuel injection pump 1D into a large amount of combustion gas 49 close to compressed air approaching 300 MPa, and a combustor 1Y is configured to form a combustion gas injection rocket nozzle 6Y. injection In the course of combustion, the superheated steam 50 in the superheated steam reservoir 95c provided in an annular shape around the outer periphery of the combustor 1Y is heated to increase the temperature of the superheated steam and to enable high-temperature combustion, thereby increasing the explosive power of each theoretically best. As the propulsion propulsion output is generated, the air and vacuum ahead are sucked and injected, and the propulsion propulsion output with the same fuel amount is increased to 10 times the existing jet.

  When flying in the air, high-speed and high-pressure dynamic pressure air is sucked from the blade leading edge core 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 29X or all blade combustion unit 30X. Inhalation, pre-compression compression and main pressure compression, the high-pressure combustion heat exchange cooling combustion without limit by the reduced-diameter compression chamber mercury heat exchanger 2Z and the reduced-diameter main combustion chamber / heat exchanger 1, the superheated steam 50 explosive force and high temperature Divided and stored as 1d mercury explosive force + 49 mass explosive force of combustion gas, each can be stored in large quantities, and can be used for out-of-fuel or space transportation, reducing the amount of fuel loaded, high-temperature high-pressure water injection at any time To make it a very safe and convenient vehicle, such as instantly extinguishing a fire in the event of a fire, flying in a vacuum at an altitude of 100 km or more without fuel, and instantaneously exceeding the first space velocity of supersonic Mach 23-28 As anywhere on earth Enables return trips, loads various rocket fuels, makes the universe as fast as possible with Mach 48 or more, and is lightweight with carbon fibers, carbon nanotubes, etc. for all parts that become hot at flying speed, such as flight wing 38b and flight tail 38c A high-pressure lightweight container is constructed by connecting the high-pressure to high-pressure water supply pipe 3.

  By using high-temperature mercury 1d pipes in high-pressure lightweight containers made of carbon fiber, water supply 52 in water supply pipes 3 and superheated steam 50, the temperature of the fireballs is recovered according to the flight speed and made into each explosive force. In use, 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 78K 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 ascending, vertical descending, and reverse injection Air and vacuum of various supersonic jets and various supersonic jet fighters aiming at 10 times the speed of existing technologies, various jets and various jet fighters, various space return passenger aircraft, various space return passenger parent planes, etc. As the output generation of various air suction jet drive equipment that sucks and jets, it enables vertical descent and vertical rise anywhere on the rooftop of the building, etc.

  The generation of the output of the air suction injection of FIG. 12 air-injected ship 38B is performed by using the combined engine combustion unit 29X or the all-blade combustion unit 30X selected according to the type A or the like of FIGS. 1 to 3 or 4 to 9. , Separated from the combined engine injection section 78K and appropriately provided in the hull, air 28a is sucked in from the leading edge 38e of the flying wing 38b, etc., and the vaporized hot air recovery device 2B is near 230 degrees of high-temperature mercury 1d. The exhaust heat quantity 5A is recovered by heat exchange, and compressed and raised to 800 to 1200 degrees Celsius at least once, and heat exchange cooling is performed in the reduced diameter main combustion chamber / heat exchanger 1 and reduced diameter compression chamber mercury heat exchanger 2Z. Fuel injection combustion in the process, infinitely high pressure combustion heat exchange cooling combustion, for example, 400 degree Celsius 24-400MPa superheated steam 50 explosive force and high temperature mercury 1d explosive force + 50-200 degree Celsius 24-300MPa combustion gas 49 mass explosion Divided into force, The temperature mercury 1d explosive force drives the vertical full blades mercury turbine 8H or Zendotsubasa flywheel mercury turbine 8E, and drives the injection unit 78K plurality by overheated steam 50 explosive force + the combustion gases 49 mass explosive force.

  In the case of injection propulsion, all of the superheated steam 50 and all of the combustion gas 49 are used to drive a plurality of injection units 78K, and all of the high-temperature mercury 1d drives the combined engine combustion unit 29X or all blade combustion unit 30X, The superheated steam 50 explosive force and the total combustion gas 49 mass explosive force maximize the air suction / injection propulsion output, and optimally include the combined engine injection portion 78K of the tenth embodiment at the front and rear of the hull. Air is sucked and sprayed backwards in the hull bottom enclosure, sprayed behind the front buoyancy plate 9A, in front of the rear levitation plate 9B, and into the parallel vertical plate 9c, and the hull is injected with 50 superheated steam such as 400 MPa. Float with a combustion gas 49 injection pressure such as pressure and 300MPa, and the majority of the bottom of the ship expanded by the parallel vertical plate 9c is the theoretical best hull levitation to minimize friction loss, and air is injected from the air nozzle 9D at the rear of the hull. Speed increase The injection speed naturally increases with, and theoretically the best of air suction injection marine propulsion output.

  In the process of jet propulsion, the rudder 40A of the air nozzle 9D and the rudder 40A of the vertical wing 38d are driven and controlled. The flying wing 38b and the flying tail 38c are integrally or appropriately divided and controlled to be lifted and lowered by existing technology, the maximum speed is made close to the sound speed, the distance from the surface of the water is kept constant, and the flying body 38a and the cabin 10A are controlled. The room 10b, the guest room 10d, the control room 10c, and the cargo room 10e are provided, and the control room 10c is equipped with a general control device 20 to control the whole with existing technology. High-temperature mercury 1d explosive power of 600-800 degrees, etc. + 60-600 degrees Celsius 24-300 MPa combustion gas explosive power is stored, and the amount of fuel loaded can be used effectively when the fuel runs out, As a very safe and convenient way to increase the amount of thermal steam and water loaded in the event of a fire, it is possible to inject immediately, aiming at 20 times the speed of the existing steering vessel by dividing the flying wing 38b and the flying tail 38c integrally or appropriately. Various air suction / injection drive devices such as various passenger ships, various ferry boats, various cargo ships, various aircraft carriers and various battle ships.

  The generation of the water suction / injection propulsion output of the water injection ship 38C in FIG. 13 is selected from 8 + 8 types such as A to H types in FIGS. 1 to 3 and FIGS. The rotor blade combustor 30X is provided separately from the water jet 78M, and the mercury injection pump 6Z is added in the same manner as described above to inject high-temperature mercury 1d vertically downward, and the atmospheric pressure power is set to 2139 * 13. By doubling, the all-blade propeller mercury turbine 8E or the vertical all-blade mercury turbine 8H is driven most efficiently, and the combined engine combustion section 29X or all-blade combustion section 30X is driven to reduce the compression chamber mercury. High-temperature combustion heat exchange cooling combustion without limitation in the heat exchanger 2Z and the reduced diameter main combustion chamber / heat exchanger 1, for example, high-temperature mercury 1d having a superheated steam explosion force of 400 degrees Celsius 24 to 400 MPa and 600 to 800 degrees saturation pressure or higher Explosive power + c The most efficient division and stored in 50 to 200 degrees 24~300MPa combustion gas explosion force, and most efficiently driven coalescence engine combustion section 29X or Zendotsubasa burning part 30X total mercury explosive force.

  The water jet 78M shown in FIG. 14 is optimally driven by the superheated steam 50 explosive force and the combustion gas 49 explosive force to drive the water jet 78M in FIG. The rudder 40A provided in the rear injection unit is driven and controlled to fly and propel the surface of the water at ultra high speed, and the surface wing 38g can be deformed up and down in order to float and transport the same weight as the existing cargo ship. Then, it is moved and deformed to an optimal position shape by a plurality of hydraulic cylinders 48a, optimally deformed to an optimal position according to the speed, and water suction injection propulsion in which a heavy-weight hull is levitated by the water pressure of the surface wing 38g according to the hull speed, A large amount of combustion gas 49 or superheated steam 50 is injected to minimize the friction loss at the bottom of the ship, and the cockpit 10b, the cabin 10d, etc. are provided at the top, and the cargo compartment 10e and the control room 1 are provided in the cabin 10A. c, and overall control with the existing technology by the overall control device 20 to store the superheated steam explosive force and mercury explosive force + combustion gas mass explosive force, which can be used at the time of running out of fuel, As a result of the increase, in the event of a fire, it is possible to inject immediately, making it very safe and convenient. Various types of water suction such as various ships, various ferry boats, various cargo ships, various aircraft carriers and various battle ships aiming at 20 times the speed of existing cargo ships. Use jet drive equipment.

  The water jet 78M shown in FIG. 14 is separated from the whole blade combustion part 30X and simplified to the limit, and the whole blade combustion part 30X collects the high-temperature mercury 1d exhaust temperature 230 degrees exhaust heat quantity 5A to the limit and becomes enormous. The intake air 28a is compressed to 800 to 1200 degrees, and heat recovery and cooling are repeated. The reduced-diameter compression chamber mercury heat exchanger 2Z and the reduced-diameter main combustion chamber / heat exchanger 1 perform unlimited high-pressure combustion heat exchange cooling and combustion, and 400 In the process of driving the water jet 78M with the maximum amount of superheated steam 50 approaching 400 MPa and the combustion gas 49 approaching 300 MPa, the combustion gas 49 with a small amount of fuel combustion and close to compressed air is combusted from the combustion gas control valve 24. The fuel 1b is supplied to the fuel reservoir 95B from the fuel control valve 25b, and the fuel injection low temperature fuel is injected into the combustor 1Y by the fuel injection pump 1D. Ignition and combustion gases 49, and the combustion gas ejection rocket nozzle 6Y than the combustion gases 49 to the maximum speed injection such as 300 MPa, and allows for maximum water suction jet propulsion output.

  In the process of fuel injection ignition combustion, the superheated steam reservoir 95c is annularly provided on the outer periphery of the combustor 1Y to heat the superheated steam 50, enabling the combustor 1Y to perform high-temperature combustion, and generating the water suction injection propulsion output of the combustion gas 49. Further increase, the temperature of the superheated steam 50 is increased and injected from a plurality of superheated steam rocket nozzles 6L to obtain the best water jet 78M in theory, which maximizes the water suction injection propulsion output, and the water repellent action 3A of the rocket nozzle causes friction. The loss is reduced, and a streamlined water jet 78M is used to aim at 20 times the speed of an existing cargo ship. Accelerates suction injection, sucks and injects water most efficiently, and various types of high-speed ships, various high-speed battle ships, various aircraft carriers, various high-speed water transportation equipment To drive the suction injection drive equipment, you have a variety of energy storage cycle combined institutions.

  In the process of generating rotational output, the dead-end defects of the reciprocating engine dead center and turbine blade are completely abolished. In order to make the rate kg weight m / sec close to 1700 * 13.5 times of steam = 23,000 times, the rotation output of the same fuel amount is close to 100 times. There is a possibility that the thermal power plant and nuclear power plant will be completely abolished, CO2 emissions will be reduced to 0, the rise in seawater temperature will be prevented, and the extinction of mankind will be postponed.

  There is a possibility of driving all-wheel impeller mercury turbine 8E or vertical all-blade mercury turbine 8H and making the world's automobiles into electric cars by reducing the electricity bill to 1/10, etc., and reducing CO2 emissions to 0 to slightly In order to reduce pollution, we manufacture and sell various automobiles, various propeller airplanes, various propeller ships, and various types of rotational force driven machinery and equipment to bring CO2 exhaust near 0, and supply heat, electricity, and cold energy when stopped May be used.

  To drive the vertical all-blade mercury turbine to nearly 100 times the rotational output and to increase the propulsion output by 10 times by the combined engine injection unit 77K, the space shuttle returns the space at an altitude of 100 km to around Mach 28 There is a possibility to fly and travel on a day trip anywhere on the planet.

  To drive the vertical all-blade mercury turbine and increase the rotation output to 100 times and increase the propulsion propulsion output to 10 times, etc. As a close flight, there is a possibility to make space travel prime.

  Since the rotation output is increased to 100 times and the injection propulsion output is increased to 10 times, the speed of various ships may approach the speed of sound, and CO2 etc. is agitated into superheated steam by simultaneous injection of superheated steam and combustion gas. Various supersonic jets, various supersonic jet fighters, various ultra-high-speed ships, various ultra-high-speed battle ships, various ultra-high-speed aircraft carriers and various universes to reduce pollution by reducing CO2 emissions by melting. Manufactures and sells return passenger planes, various space passenger planes, various air transport mobile devices, various water transport mobile devices, etc., bringing CO2 and other exhausts close to zero, and heat, electricity, and cold when stopped May be used as a supply facility.

  In order to make heat, electricity, and cold supply equipment close to 100 times the rotational output, the energy storage compressor 20X is used as a multi-cylinder, and almost all the exhaust heat at a high-temperature mercury exhaust temperature of around 230 degrees is recovered, and repeated compression heat recovery. Because of the high-pressure combustion heat exchange cooling combustion without limit, the combustion gas exhaust that approaches absolute 0 degrees becomes enormous, and when all of the combustion gas such as CO2 is dissolved in water with the tap water cooling heat close to 0 degrees Celsius, the combustion gas dissolves When it is supplied to the sea floor, it may grow algae and the like, and fish in the food chain may be proliferated to prevent the extinction of seawater-cooled humans.

  In order to make heat, electricity, and cold supply equipment with a rotational output approaching 100 times, the energy storage compressor 20X is multi-cylinder, recovering almost all the exhaust heat at around 230 degrees Celsius, and repeatedly compressing heat recovery Because of the high-pressure combustion heat exchange cooling combustion without limit, the combustion gas exhaust that approaches absolute 0 degree becomes enormous, so the combustion gas 49 exhaust is first cooled with air and sold for use at cryogenic temperatures. Various cold heat utilization such as direct refrigeration business, ice making business, methane hydrate recovery business, etc., enabling air temperature near -50 degrees to -200 degrees, such as selling to customers with tap water cooling near 0 degrees Celsius There is a possibility of entering the business.

  In order to make heat, electricity, and cold supply equipment close to 100 times the rotational output, the energy storage compressor 20X is used as a multi-cylinder, and almost all the exhaust heat at a high-temperature mercury exhaust temperature of around 230 degrees is recovered, and repeated compression heat recovery. Because of the high-pressure combustion heat exchange cooling combustion without limit, the combustion gas exhaust that approaches absolute 0 degree becomes enormous, and all the heat exchange storage is made with alcohol 1C near -100 degrees, and the heat exchange demand with the material suitable for the application Manufactures and sells various commercial and household refrigeration equipment, various refrigeration equipment, various cooling equipment, various ice making equipment, thermal heating and cooling piping buildings, etc., aiming to consume 1/10 of electricity when sold to the home The whole urban area may be cooled to reverse the heat island phenomenon.

  In order to make heat, electricity, and cold supply equipment with a rotational output approaching 100 times, the energy storage compressor 20X is multi-cylinder, recovering almost all the exhaust heat at around 230 degrees Celsius, and repeatedly compressing heat recovery As much as possible, use high-pressure combustion heat exchange cooling combustion division storage to minimize the supply heat amount, but the supply heat amount is excessive, so the excess heat amount is 300 degrees Celsius or less, etc. Is sold to customers as a by-product of power generation, and uses water temperature heat 52d to aim for power consumption of 1/10, etc., various heating equipment for business use and household use, various cooking equipment, various hot water equipment, There is a possibility of manufacturing and selling various dishwashers, various washing and drying machines, and various seawater desalination equipment.

  In order to make heat, electricity, and cold supply equipment with a rotational output approaching 100 times, the energy storage compressor 20X is multi-cylinder, recovering almost all the exhaust heat at around 230 degrees Celsius, and repeatedly compressing heat recovery As much as possible, use high-pressure combustion heat exchange cooling combustion division storage to reduce the supply heat amount, but the supply heat amount is surplus, so the excess heat amount is less than 300 degrees Celsius, etc., and the tap water temperature directly close to 300 degrees Celsius May be injected into methane hydrate or permafrost methane to enter the methane recovery business.

  By cooling the combustion gas 49 of about 300 degrees with the superheated steam 50 or the like of the feed water pipe 3 and maximizing the combustion amount of the cooling combustor 1Y to about 40 degrees or 0, the vertical all blade gas turbine 8A or There is a possibility of maximizing the rotational output of all blade impeller gas turbine 8a or maximizing the amount of cold energy recovered.

Sectional view of energy storage compressor 20A coalescing engine combustion section 29A (Example 1) Sectional view of rocket nozzle and all-wheel impeller mercury turbine 8E (Example 2) Cross-sectional view of all blade impeller turbine and combined engine combustion section 29A (Example 3) Sectional view of vertical rotor blade mercury turbine 8H and rotor blade combustion section 30A (Example 4) Cross section of vertical all blade mercury turbine 8A and all blade combustion section 30A (Example 5) Cross section of vertical all blade mercury turbine 8H and all blade combustion section 30B (Example 6) Sectional view of vertical all blade mercury turbine 8H and all blade combustion section 30C (Example 7) Cross-sectional view of vertical all blade mercury turbine 8H and all blade combustion section 30D (Embodiment 8) Cross section of vertical all blade mercury turbine 8H and all blade combustion section 30E (Example 9) Sectional drawing which shows union engine injection part 78K (Example 10) Explanatory drawing which shows the union engine airplane 38A (Example 11) Sectional drawing which shows air-injection ship 38B (Example 12) Sectional drawing which shows water-injection ship 38C (Example 13) Sectional view showing water jet 78M (Example 14)

Explanation of symbols

  1: reduced diameter main combustion chamber / heat exchanger, 1A: preload compression chamber / heat exchanger, 1C: alcohol, 1D: fuel injection pump, 1E: mercury injection pump, 1G: heat pump, 1Y: combustor, 1Z: Combustion chamber, 1a: combustion section, 1b: fuel, 1d: high-temperature mercury, 2: reduced diameter main combustion chamber heat exchanger, 2b: vaporized hot water recovery device, 2B: vaporized hot air recovery device, 2Z: reduced diameter compression chamber Mercury heat exchanger, 3: water supply pipe, 3a: water repellent plating, 3A: water repellent action 3G: water repellent action (means for reducing friction loss with mercury) 4a: outer compressor rotor blade group, 4b: inner compressor rotor blade group 5A: Exhaust heat quantity, 5c: Gas exhaust chamber, 6: Nozzle, 6a: Nozzle injection part, 6b: Mercury injection nozzle, 6d: Nozzle injection part, 6A: Superheated steam rocket nozzle, 6B: Superheated steam rocket nozzle, 6C: Combustion gas rocket Nozzle, 6D: Combustion gas rocket nozzle, 6L: Superheated steam rocket nozzle, 6M: Combustion gas rocket nozzle, 6Y: Combustion gas injection rocket nozzle, 6Z: Mercury injection pump (improved from fuel injection pump, gear pump, etc.), 7 : Fuel injection valve, 7C: Fuel injection solenoid valve, 8a: Full blade impeller gas turbine, 8b: Full blade impeller steam turbine, 8c: Turbine blade, 8d: Side plate, 8e: Cylindrical barrel, 8A: Vertical full motion Blade gas turbine, 8B: vertical all-blade steam turbine, 8E: all-blade flywheel mercury turbine (all-blade mercury turbine), 8H: vertical all-blade mercury turbine (all-blade mercury turbine), 9: one Directional air flow heat exchanger (improved for exhaust heat recovery), 9A: Front levitation plate, 9B: Rear levitation plate, 9C: Parallel vertical plate, 9D: Air nozzle, 10 : Cabin, 10a: diameter expansion compression chamber, 10b: cockpit 10c: control room, 10d: cabin, 10e: cargo compartment, 15: cylinder head, 16: crankshaft, 16A: crank, 20A: A type energy storage compressor 20B: B type energy storage compressor, 20C: C type energy storage compressor, 20D: D type energy storage compressor, 20E: E type energy storage compressor, 20F: F type energy storage compressor, 20G: G type Energy storage compressor, 20H: H-type energy storage compressor, 20X: Selected energy storage compressor, 21: Expanded piston, 24: Combustion gas control valve, 25: Superheated steam control valve, 25b: Fuel control valve, 25B : High-temperature water control valve, 28: Intake valve, 28a: Air, 29: Various energy storage cycle coalescing engines (various rockets and various types Engine, steam turbine, gas turbine and energy conservation cycle coalescing engine), 29a: A-type energy conservation cycle coalescence engine (using coalescence engine combustion unit 29A or full blade combustion unit 30A), 29b: B-type energy conservation cycle coalescence Engine (using combined engine combustion section 29B or full blade combustion section 30B), 29c: C-type energy saving cycle combined engine (using combined engine combustion section 29C or full blade combustion section 30C), 29d: D-type energy saving storage combination Engine (using combined engine combustion unit 29D or full blade combustion unit 30D), 29e: E-type energy storage cycle combined engine (using combined engine combustion unit 29E or full blade combustion unit 30E), 29f: F-type energy storage cycle combining Engine (using combined engine combustion section 29F or full blade combustion section 30F), 29g: G-type energy storage cycle Combined engine (using combined engine combustion section 29G or full blade combustion section 30G), 29h: H-type energy saving cycle combined engine (using combined engine combustion section 29H or full blade combustion section 30H), 29A: A-type combined engine combustion 29B: B-type coalescence engine combustion section, 29C: C-type coalescence engine combustion section, 29D: D-type coalescence engine combustion section, 29E: E-type coalescence engine combustion section, 29F: F-type coalescence engine combustion section, 29G: G Type coalescence engine combustion section, 29H: H-type coalescence engine combustion section, 29X: Selected coalescence engine combustion section, 30A: Type A full blade combustion section, 30B: Type B full blade combustion section, 30C: Type C full motion Blade combustor, 30D: D-type all blade combustor, 30E: E-type all blade combustor, 30F: F-type all blade combustor, 30G: G-type all blade combustor, 30H: H-type full motion Wing combustion section, 30X: Selected all blade combustion 37: Double-headed enlarged piston, 38A: Combined engine plane, 38B: Air-injection ship, 38C: Water-injection ship, 38a: Flight trunk, 38b: Flight wing, 38c: Flight tail, 38d: Vertical wing, 38e: Wing Front edge suction port, 38 g: water wing, 39: fixing groove, 40: driving tool, 40A: rudder, 40a: pendulum arm, 48a: hydraulic cylinder, 49: combustion gas, 49a: combustion gas stirring plate, 50: overheating Steam, 51: Air extractor, 51a: Gas extractor, 52: Water supply, 52a: Water, 52b: High-temperature water (high-temperature water with multiple temperatures such as supercritical temperature) 52c: Tap water, 52d: Hot water for tap water, 52e: Tap water cooling heat, 52f: condensed water, 52g: combustion gas dissolved water, 52h: cold water, 55: water pump / magnetic friction power transmission device, 55B: water pump / magnetic Friction power 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, 77K: Combined engine injection part, 77L: Combined engine injection part, 77M: Water jet, 77N: Water jet , 78K: coalescence engine injection unit, 78M: water jet, 81: support shaft, 81a: fulcrum, 84: water pump and counter-rotating magnetic friction power transmission device, 85: counter-rotating magnetic friction power transmission device, 88: publicly known 95: high temperature water reservoir, 95B: fuel reservoir, 95D: mercury reservoir, 95a: combustion gas reservoir, 95b: water reservoir, 95c: Superheated steam reservoir, 95d: Combustion gas reservoir, 96: Stroke, 97: Check valve, 98: Valve seat, 99: Valve body, 103: Cold recovery device,

Claims (11325)

  Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30A) that reduces friction loss, and various energy storage cycle combined engines as various rotary output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various energy storage cycle coalescing engines as various rotary output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30C) that reduces friction loss, and various energy storage cycle coalescing engines as various rotary output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G) .   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30E) that reduces friction loss, and various energy storage cycle coalescing engines as various rotary output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss through water repellent action (3G) .   Mercury pump (1E) Mercury injection pump (6Z) and all blade storage unit (30G) that reduces friction loss by water repellent action (3G) .   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30H) that reduces friction loss by water repellent action (3G) .   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30A) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30B) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30C) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30E) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30F) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30G) that reduces friction loss by the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30H) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and combined with various energy storage cycle engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various energy storage cycle coalescing engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various energy storage cycle coalescing engines as various rotary output drive devices.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion section (30A) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles including a rotating blade combustion section (30B) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various rotational output drive devices. Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30C) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30D) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30E) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30F) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30G) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30H) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including all blade combustion section (30A) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion section (30B) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30C) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30D) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30E) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30F) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30G) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a full blade combustion part (30H) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-energy mercury (1d) all-blade combustion section (30A) that increases the rotational output by the gravity of the various energy storage cycle combined into various rotational output drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and high-energy mercury (1d) all-blade combustion section (30B) that increases the rotational output by the gravity of gravity, combined with various energy output cycle equipment as various rotational output drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and high-energy mercury (1d) all-blade combustion section (30C) that increases the rotational output by the gravity of the various energy storage cycle combined into various rotational output drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and high-energy mercury (1d) all-blade combustion section (30D) that increases the rotational output by the gravity of gravity, and various energy storage cycle combinations as various rotational output drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and high-energy mercury (1d) all-blade combustion section (30E) that increases the rotational output by the gravity of gravity, and various energy storage cycle combinations as various rotational output drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and high-energy mercury (1d) all-blade combustion section (30F) that increases the rotational output by the gravity of gravity, combined with various energy storage cycle units as various rotational output drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and high-energy mercury (1d) all-blade combustion section (30G) that increases the rotational output by the gravity of gravity, combined with various energy storage cycle units as various rotational output drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and high-energy mercury (1d) all-blade combustion part (30H) that increases the rotational output by gravity, and various energy storage cycle coalesced as various rotational output drive devices organ.   Various energy storage cycles with various rotary output drive equipment including a mercury blade (1E) mercury injection pump (6Z) and a full blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d). Combined organization.   Various energy storage cycles with various rotary output drive equipment, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30D) that reduces friction loss by the surface tension of high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d) Combined organization.   Various energy storage cycles with various rotary output drive equipment, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-energy mercury (1d) all-blade combustion section (30G) that reduces friction loss due to surface tension, and various energy storage cycles as various rotary output drive devices Combined organization.   Various energy storage cycles with various rotary output drive equipment including a mercury blade (1E) mercury injection pump (6Z) and a full blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29F) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, combined with various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) for reducing friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) for reducing friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various rotary output drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines as various rotary output drive devices.   Combining various energy storage cycles with a combined engine combustion section (29A) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d). organ.   Combining various energy storage cycles with a combined engine combustion section (29B) that increases rotational output by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Combining various energy conservation cycles with a combined engine combustion section (29C) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Combining various energy storage cycles with a combined engine combustion section (29D) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) organ.   Combining various energy storage cycles with a combined engine combustion section (29E) that increases rotational output by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Combining various energy storage cycles with a combined engine combustion section (29F) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various rotational output drive devices organ.   Combining various energy conservation cycles with a combined engine combustion section (29G) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d). organ.   Combining various energy storage cycles with a combined engine combustion section (29H) that increases rotational output by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) organ.   Combining various energy conservation cycles with a combined engine combustion section (29A) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion section (29B) to reduce friction loss, and various energy storage cycle coalescence as various rotary output drive devices organ.   Combining various energy conservation cycles with a combined engine combustion section (29C) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d). organ.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29D) to reduce friction loss, and various energy conservation cycle coalescence as various rotary output drive devices organ.   Combining various energy conservation cycles with a combined engine combustion section (29E) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d). organ.   Combining various energy storage cycles with a combined engine combustion section (29F) that reduces friction loss by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Combining various energy conservation cycles with a combined engine combustion section (29G) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d). organ.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29H) to reduce friction loss, and various energy conservation cycle coalescence as various rotary output drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various energy storage cycle combined engines as various rotational output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29B) that increases rotational output by the gravity of high-temperature mercury (1d), and various energy storage cycle combined engines as various rotational output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various energy storage cycle combined engines as various rotational output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29D) that increases rotational output by the gravity of high-temperature mercury (1d), and various energy storage cycle combined engines as various rotational output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various energy storage cycle combined engines as various rotational output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29F) that increases rotational output by the gravity of high-temperature mercury (1d), and various energy storage cycle combined engines as various rotational output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various energy storage cycle combined engines as various rotational output drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29H) that increases rotational output by the gravity of high-temperature mercury (1d) and various energy storage cycle combined engines as various rotational output drive devices .   Combining various energy storage cycles with a combined engine combustion section (29A) that reduces friction loss by the surface tension of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various rotational output drive devices organ.   Combining various energy storage cycles with a combined engine combustion section (29B) that reduces friction loss by the surface tension of the mercury pump (1E), mercury injection pump (6Z) and high-temperature mercury (1d), and various rotational output drive devices organ.   Combining various energy storage cycles with various rotational output drive equipment, including a combined engine combustion section (29C) that reduces friction loss by the surface tension of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Combining various energy storage cycles with various rotational output drive equipment, including a combined engine combustion section (29D) that reduces friction loss by the surface tension of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Combining various energy storage cycles with a combined engine combustion section (29E) that reduces friction loss due to the surface tension of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various rotational output drive devices organ.   Combining various energy storage cycles with a combined engine combustion section (29F) that reduces friction loss by the surface tension of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various rotational output drive devices organ.   Combining various energy storage cycles with various rotational output drive equipment, including a combined engine combustion section (29G) that reduces friction loss by the surface tension of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Combining various energy storage cycles with a combined engine combustion section (29H) that reduces friction loss by the surface tension of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various rotational output drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion part (30F) that reduces friction loss by water repellent action (3G) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) for reducing friction loss due to surface tension of mercury, and various rotary output drive devices including various heating equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various heating equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) for reducing friction loss due to surface tension of mercury, and various rotary output driving devices including various heating equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various heating equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) for reducing friction loss due to surface tension of mercury, and various rotary output drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various heating equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) which reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases the rotational output by rolling contact, and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotational output by rolling contact, and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases the rotational output by rolling contact, and various rotational outputs including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by rolling contact, and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30E) that increases rotational output by rolling contact, and various rotational outputs including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases the rotational output by rolling contact, and various rotational outputs including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases the rotational output by rolling contact, and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30H) that increases rotational output by rolling contact, and various rotational outputs including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact part (30A) that reduces friction loss by rolling contact, and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact section (30B) that reduces friction loss by rolling contact, and various rotational outputs including various heating equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30C) that reduces friction loss by rolling contact, and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30D) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30E) to reduce friction loss by rolling contact and various rotary outputs including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30F) to reduce friction loss by rolling contact and various rotary outputs including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30G) that reduces friction loss by rolling contact, and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact section (30H) that reduces friction loss by rolling contact, and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various heating equipments using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various heating equipments using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive including various heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive including various heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various heating equipments using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various types of heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various heating equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various heating equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29A) that reduces friction loss by rolling contact, and various rotational output drives including various heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29B) that reduces friction loss by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29C) that reduces friction loss by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29E) that reduces friction loss by rolling contact, and various rotational output drives including various heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29G) that reduces friction loss by rolling contact, and various rotational output drive including various heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipments using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipments using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by water repellent action (3G), and various rotary output drive equipment including various cooking equipments using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipments using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooking equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipments using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipments using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) for reducing friction loss due to surface tension of mercury, and various rotary output driving devices including various cooking equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) for reducing friction loss due to surface tension of mercury, and various rotary output drive devices including various cooking equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various cooking equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases the rotational output by rolling contact, and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotational output by rolling contact, and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30C) that increases rotational output by rolling contact, and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by rolling contact, and various rotational outputs including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by rolling contact, and various rotational outputs including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases the rotational output by rolling contact, and various rotational outputs including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases the rotational output by rolling contact, and various rotational outputs including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases the rotational output by rolling contact, and various rotational outputs including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion part (30A) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30B) that reduces friction loss by rolling contact, and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30C) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30D) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact part (30E) that reduces friction loss by rolling contact, and various rotational outputs including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30F) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact section (30G) that reduces friction loss by rolling contact, and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all rotor blade combustion section (30H) to reduce friction loss. Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooking equipments using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooking equipment devices using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and rotary blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and rotary blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and rotary blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotational outputs including various cooking equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotating output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by rolling contact of mercury and various rotary output drive devices including various cooking equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooking equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooking equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29C) that reduces friction loss by rolling contact, and various rotational output drives including various cooking equipments using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various rotational output drives including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29E) that reduces friction loss by rolling contact, and various rotational output drives including various cooking equipments using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29F) that reduces friction loss by rolling contact, and various rotational output drives including various cooking equipments using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29H) that reduces friction loss by rolling contact, and various rotary output drive including various cooking equipments using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooking equipment devices using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooking equipments using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooking equipment devices using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooking equipment devices using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooking equipment devices using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooking equipments using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooking equipment devices using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooking equipment devices using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various cooking equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various cooking equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various cooking equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various cooking equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various cooking equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various cooking equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various types of hot water equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water equipment devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various rotary output drive devices including various hot water equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various types of hot water equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion part (30F) that reduces friction loss by water repellent action (3G) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G) and various rotary output drive devices including various hot water equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G) and various rotary output drive devices including various hot water equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various hot water facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various hot water equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various hot water equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water equipment equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various hot water equipment devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact, and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact, and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact, and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact, and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30H) that increases rotational output by rolling contact, and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30A) to reduce friction loss by rolling contact, and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact section (30B) that reduces friction loss by rolling contact and various rotary outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact and various rotary outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30D) to reduce friction loss by rolling contact, and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact and various rotary outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact and various rotary outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact section (30G) that reduces friction loss by rolling contact, and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water equipment. Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water equipment. Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water equipment. Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water equipment using warm heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various types of hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotational outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water facility devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various warm water equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various warm water equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water facility devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water equipment equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various warm water equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water facility devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water facility devices using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss due to mercury surface tension, and various rotary output drive devices including various hot water equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury and various rotary output drive devices including various hot water equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various hot water facility devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water equipment equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water facility equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of mercury and various rotary output drive equipment including various hot water equipment equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various rotational output driving including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various rotational output drive including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29A) that reduces friction loss by rolling contact, and various rotary output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29B) to reduce friction loss by rolling contact, and various rotary output drive including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various rotary output drive including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29D) that reduces friction loss by rolling contact, and various rotary output drive including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various rotational output drives including various types of hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29F) that reduces friction loss by rolling contact, and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29G) that reduces friction loss by rolling contact, and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29H) that reduces friction loss by rolling contact, and various rotary output drive including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water facility devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water facility devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water facility devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water facility devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water equipments A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water facility devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water facility devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water facility devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various hot water equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by water repellent action (3G), and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G) and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by rolling contact with mercury, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact with mercury, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact of mercury and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30A) that increases rotational output by rolling contact, and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotational output by rolling contact, and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30C) that increases rotational output by rolling contact, and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30D) that increases rotational output by rolling contact, and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have all rotor blade combustion section (30E) that increases rotational output by rolling contact, and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30F) that increases rotational output by rolling contact, and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30G) that increases rotational output by rolling contact, and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) which increases rotational output by rolling contact, and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade drive unit (30A) that reduces friction loss by rolling contact, and various rotary output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have all rotor blade combustion section (30B) to reduce friction loss by rolling contact, and various rotary output drive including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30C) that reduces friction loss by rolling contact, and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30D) to reduce friction loss by rolling contact, and various rotary output drive including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30E) that reduces friction loss by rolling contact, and various rotary output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have all rotor blade combustion section (30F) to reduce friction loss by rolling contact, and various rotary output drive including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30G) that reduces friction loss by rolling contact with various rotary output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30H) to reduce friction loss, and various rotary output drive including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30E) that increases the rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various dishwashers that use heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30F) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various dishwashers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29A) that reduces friction loss, and various rotary output drive devices including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29B) that reduces friction loss, and various rotary output drive devices including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29C) that reduces friction loss, and various rotary output drive devices including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29D) that reduces friction loss, and various rotary output drive devices including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29E) that reduces friction loss, and various rotary output drive devices including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29F) that reduces friction loss, and various rotary output drive devices including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29G) that reduces friction loss, and various rotary output drive devices including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29H) that reduces friction loss, and various rotary output drive devices including various dishwashers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various dishwashers using heat Energy conservation cycle coalescence engine.   Various rotary output driving devices including a combined engine combustion section (29A) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and the high temperature mercury (1d), including various dishwashers using heat. A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a combined engine combustion section (29B) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a combined engine combustion section (29C) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a combined engine combustion section (29D) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d), including various dishwashers that use heat A variety of energy conservation cycle coalescence engine.   Various rotary output driving devices including a combined engine combustion section (29E) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a combined engine combustion section (29F) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d), including various dishwashers that use heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29G) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a combined engine combustion section (29H) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d), including various dishwashers that use heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a combined engine combustion section (29A) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29B) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and coalescence engine combustion part (29C) that reduces friction loss A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29D) to reduce friction loss and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29E) that reduces friction loss by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a combined engine combustion section (29F) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with coalesced engine combustion section (29G) that reduces friction loss A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29H) that reduces friction loss, and various rotary output drive devices including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various types of dishwashers using heat, equipped with a combined engine combustion section (29A) that increases the rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various dishwashers using heat, equipped with a combined engine combustion section (29B) that increases rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various dishwashers using heat, equipped with a combined engine combustion section (29C) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including a combined dish combustion unit (29D) that increases the rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various dishwashers using heat Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various dishwashers using heat, equipped with a combined engine combustion section (29E) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including a combined dish combustion unit (29F) that increases the rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and includes various dishwashers using heat. Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various dishwashers using heat, equipped with a combined engine combustion section (29G) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various dishwashers using heat, equipped with a combined engine combustion section (29H) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29A) that reduces friction loss by surface tension, and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drive devices including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drive devices including various dishwashers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G) and various rotary output drive equipment including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) for reducing friction loss due to surface tension of mercury, and various rotary output driving devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) for reducing friction loss due to surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases the rotational output by rolling contact, and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotational output by rolling contact, and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30C) that increases rotational output by rolling contact, and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30D) that increases rotational output by rolling contact, and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by rolling contact, and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact, and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact, and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30H) that increases rotational output by rolling contact, and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion part (30B) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30C) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact section (30D) that reduces friction loss by rolling contact and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30E) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30F) to reduce friction loss and various rotational outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30G) to reduce friction loss by rolling contact and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30H) that reduces friction loss by rolling contact and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30C) that increases the rotational output by gravity, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30D) that increases the rotational output by gravity, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30E) that increases the rotational output by gravity, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) which increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and rotary blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various washing dryers using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G) and various rotary output drive equipment including various washing dryers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various washing dryers using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion part (29G) that increases the rotational output by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29A) that reduces friction loss by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29B) that reduces friction loss by rolling contact, and various rotary output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various rotary output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29D) that reduces friction loss by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29E) that reduces friction loss by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29H) that reduces friction loss by rolling contact, and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) combined engine combustion section (29B) that increases the rotational output by gravity, and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) combined engine combustion section (29F) that increases rotational output by gravity, and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various washing dryers using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including various washing dryers using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G) and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30A) that increases rotational output by rolling contact, and various rotational output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact, and various rotational output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30C) to increase rotational output by rolling contact, and various rotational output drive including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by rolling contact, and various rotational output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have all rotor blade combustion section (30E) that increases rotational output by rolling contact, and various rotational output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact, and various rotational output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion part (30G) which increases rotational output by rolling contact, and various rotational output drive including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30H) that increases rotational output by rolling contact, and various rotational output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30A) that reduces friction loss by rolling contact with various rotating output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30B) to reduce friction loss and various rotary output drive including various hot water piping Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30C) to reduce friction loss, and various rotary output drive including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive part (30D) equipped with all blade combustion part (30D) to reduce friction loss by rolling contact, various rotary output drive including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30E) to reduce friction loss by rolling contact, various rotary output drive including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30F) to reduce friction loss and various rotary output drive including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30G) to reduce friction loss and various rotary output drive including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30H) to reduce friction loss and various rotary output drive including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including various hot water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping buildings Energy conservation cycle coalescence engine.   Various rotary output drive equipment including various hot water pipe buildings with a combined engine combustion section (29A) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various hot water piping buildings equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various hot water pipe buildings with a combined engine combustion section (29D) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various hot water piping buildings with a combined engine combustion section (29E) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various hot water piping buildings with a combined engine combustion section (29F) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various hot water piping buildings equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and combined engine combustion section (29A) to reduce friction loss and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29B) that reduces friction loss and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29C) that reduces friction loss and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29D) to reduce friction loss and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29E) that reduces friction loss and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29F) that reduces friction loss and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29G) to reduce friction loss and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29H) to reduce friction loss and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various hot water piping buildings, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various hot water piping buildings, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) combined engine combustion section (29D) that increases the rotational output by gravity, and various rotary output drive devices including various hot water piping buildings Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various hot water pipe buildings with a combined engine combustion section (29E) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various hot water piping buildings with a combined engine combustion section (29F) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29A) that reduces friction loss by surface tension and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion part (29B) that reduces friction loss by surface tension and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29C) that reduces friction loss due to surface tension and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29D) that reduces friction loss due to surface tension and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29F) that reduces friction loss due to surface tension and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29G) that reduces friction loss by surface tension and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion part (29H) that reduces friction loss by surface tension, and various rotary output drive equipment including various hot water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) for reducing friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) for reducing friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) for reducing friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Various rotational outputs including various cooling equipment using cold heat, equipped with a whole blade combustion part (30A) that increases rotational output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold heat, equipped with a whole blade combustion part (30B) that increases the rotary output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotational outputs including various cooling equipment using cold heat, equipped with all blade combustion part (30C) that increases rotational output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold heat, equipped with a whole blade combustion part (30D) that increases the rotary output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various cooling equipment using cold heat, equipped with a whole blade combustion part (30E) that increases the rotating output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various cooling equipment using cold heat, equipped with all blade combustion part (30F) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various cooling equipment using cold heat, equipped with a whole blade combustion part (30G) that increases the rotating output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold heat, equipped with a whole blade combustion part (30H) that increases the rotary output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all rotor blade combustion section (30A) to reduce friction loss. Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold heat with mercury blade (1E) mercury injection pump (6Z) and all blade combustion part (30B) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30C) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold heat with mercury blade (1E) mercury injection pump (6Z) and all blade combustion part (30D) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various cooling equipment using cold heat with mercury blade (1E) mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various cooling equipment using cold heat with mercury blade (1E) mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade combustion part (30F) that reduces friction loss by rolling contact Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold heat with mercury blade (1E) mercury injection pump (6Z) and all blade combustion part (30G) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30H) to reduce friction loss Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various cooling facility devices using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling facility devices using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Various rotational output drives including a combined engine combustion section (29A) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various cooling facility equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29B) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various cooling facility equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29C) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various cooling facility equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29D) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold heat, equipped with a combined engine combustion section (29E) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold energy, equipped with a combined engine combustion section (29F) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29G) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various cooling facility equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various cooling equipment using cold heat, equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various cooling equipment using cold heat, equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various cooling equipment using cold heat, equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various cooling equipment using cold heat, equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various cooling equipment using cold energy, equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various cooling equipments using cold heat, equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various cooling equipment using cold heat, equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29H) that reduces friction loss by rolling contact, and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotary output drive equipment including various cooling equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output driving equipment including various cooling equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various cooling facility equipment using cold heat, equipped with a combined engine combustion section (29C) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various cooling equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various cooling equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by water repellent action (3G), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by water repellent action (3G), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) to reduce friction loss by water repellent action (3G), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by water repellent action (3G), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various energies as various rotary output drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all blade blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various energy used as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and various energy as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various energies as various rotary output drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various energy as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various energy as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various energies as various rotary output drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30H) that reduces friction loss due to the surface tension of mercury, and various energy used as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30A) that reduces friction loss by rolling contact with mercury, and various energies as various rotary output drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various energies as various rotary output drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various energy as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact with mercury, and various energies as various rotary output drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30E) that reduces friction loss by rolling contact with mercury, and various energy used as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30F) that reduces friction loss by rolling contact with mercury, and various energy used as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various energy as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact with mercury, and various energy as various rotary output drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotational output by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various generators with a full blade combustion part (30E) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various generators with a full blade combustion part (30G) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases rotational output by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all rotor blade combustion section (30A) to reduce friction loss. Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all rotor blade combustion section (30B) to reduce friction loss. Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all rotor blade combustion section (30C) to reduce friction loss Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all rotor blade combustion section (30D) to reduce friction loss and various rotary output drive equipment including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30E) to reduce friction loss Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30F) to reduce friction loss Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30G) to reduce friction loss, and various rotary output drive equipment including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion part (30H) to reduce friction loss Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30B) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30D) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output driving devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30G) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary output drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29A) that reduces friction loss, and various types of rotary output drive equipment including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29B) that reduces friction loss, and various rotary output drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29C) that reduces friction loss, and various rotary output drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29D) that reduces friction loss and various rotary output drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29E) that reduces friction loss, and various rotary output drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29F) that reduces friction loss, and various rotary output drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29G) that reduces friction loss, and various rotary output drive equipment including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29H) that reduces friction loss, and various rotary output drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various energy storage as various rotational output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive devices including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive devices including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive devices including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive devices including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various generators Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various rotational output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29A) for reducing friction loss by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29F) for reducing friction loss by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined engine combustion section (29D) that increases the rotational output by the gravity of gravity, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) combined engine combustion section (29B) for reducing friction loss due to surface tension, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29C) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) combined rotary combustion unit (29F) that reduces friction loss by surface tension, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) combined engine combustion section (29H) that reduces friction loss due to surface tension, and various rotary output drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all-blade combustion section (30B) to reduce friction loss and various rotary output drive equipment including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all-blade combustion section (30C) to reduce friction loss and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all-blade combustion section (30D) that reduces friction loss and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30E) to reduce friction loss and various rotary output drive equipment including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all-blade combustion section (30F) that reduces friction loss and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all rotor blade combustion section (30G) to reduce friction loss, and various rotary output drive equipment including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all-blade combustion section (30H) that reduces friction loss and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various energy storage as various rotary output drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various energy storage as various rotary output drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all rotor blade combustion section (30A) that increases rotational output by rolling contact, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotational output by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases the rotational output by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive section (30D) that increases the rotational output by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) which increases rotational output by rolling contact, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases the rotational output by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases the rotational output by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-rotary blade combustion section (30H) that increases rotational output by rolling contact with various rotating output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all rotor blade combustion section (30A) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30C) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all rotor blade combustion section (30D) to reduce friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive section (30E) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive section (30F) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by the gravity of gravity, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d) and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d) and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29A) that reduces friction loss, and various energy used as various rotary output drive equipment including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29B) that reduces friction loss, and various energy output as various rotary output drive equipment including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various energies as various rotational output drive equipment including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29D) that reduces friction loss, and various energy output as various rotary output drive equipment including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with combined engine combustion section (29E) that reduces friction loss, and various energy used as various rotary output drive equipment including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29F) that reduces friction loss, and various energy used as various rotary output drive equipment including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29G) that reduces friction loss, and various energies for various rotary output drive devices including various motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29H) that reduces friction loss, and various energy as various rotational output drive equipment including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various energy storage cycles as various rotational output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various energy storage cycles as various rotational output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of mercury, and various energy storage cycles as various rotational output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various energy storage cycles as various rotational output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various energy storage cycles as various rotary output drive devices including various electric motors Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29A) that increases rotational output by rolling contact, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact with various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various rotary output drive devices including various electric motors. Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29A) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29B) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29C) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29D) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29E) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29F) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29G) to reduce friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29H) that reduces friction loss by rolling contact, and various rotary output drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) combined engine combustion section (29A) to reduce friction loss by surface tension, and various rotary output drive equipment including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined engine combustion section (29B) that reduces friction loss due to surface tension, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) combined engine combustion section (29C) to reduce friction loss by surface tension, and various rotary output drive equipment including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined engine combustion section (29D) that reduces friction loss due to surface tension and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined engine combustion section (29E) that reduces friction loss due to surface tension, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G) and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss due to mercury surface tension, and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss due to surface tension of mercury and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss due to surface tension of mercury, and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) to reduce friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30A) that increases rotational output by rolling contact, and various rotational output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30B) that increases rotational output by rolling contact, and various rotational output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30C) to increase rotational output by rolling contact, and various rotational output drive including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30D) that increases rotational output by rolling contact, and various rotational output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30E) that increases rotational output by rolling contact, and various rotational output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30F) that increases rotational output by rolling contact, and various rotational output drive including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30G) that increases rotational output by rolling contact, and various rotational output drive including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30H) that increases rotational output by rolling contact, and various rotational output drive including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30A) that reduces friction loss by rolling contact, and various rotational output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30B) that reduces friction loss by rolling contact with various rotating output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30C) to reduce friction loss and various rotary output drive including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30D) that reduces friction loss by rolling contact with various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive part (30E) that reduces friction loss by rolling contact, and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade drive unit (30F) that reduces friction loss by rolling contact, and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30G) that reduces friction loss by rolling contact with various rotating output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30H) to reduce friction loss and various rotary output drive including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30B) that increases the rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) which increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30F) that increases the rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that reduces friction loss by surface tension, and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30C) that reduces friction loss by surface tension, and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drives including various hot water piping greenhouses Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping greenhouses, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping greenhouses, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), various rotary output drive equipment including various hot water piping greenhouses, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, and various rotary output drive devices including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping greenhouses Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various rotary output drive devices including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various rotary output drive devices including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various rotary output drive devices including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various rotary output drive devices including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various rotary output drive devices including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various rotary output drive devices including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and a combined engine combustion section (29G) that increases the rotational output A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and a combined engine combustion section (29H) that increases the rotational output A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29A) to reduce friction loss, and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with coalesced engine combustion section (29B) to reduce friction loss and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion unit (29C) that reduces friction loss, and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29D) to reduce friction loss and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29E) that reduces friction loss, and various rotary output drive devices including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with coalesced engine combustion section (29F) that reduces friction loss and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with coalesced engine combustion section (29G) that reduces friction loss and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with coalesced engine combustion section (29H) that reduces friction loss and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping greenhouses Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29A) that reduces friction loss by surface tension, and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29B) that reduces friction loss by surface tension and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29C) that reduces friction loss by surface tension, and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29D) that reduces friction loss due to surface tension and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various hot water piping greenhouses A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) for reducing friction loss due to surface tension of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by mercury surface tension, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) for reducing friction loss due to mercury surface tension, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by mercury surface tension, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact, and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotational output by rolling contact, and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that increases rotational output by rolling contact, and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by rolling contact and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by rolling contact, and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact, and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) that increases rotational output by rolling contact, and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases the rotational output by rolling contact, and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30A) to reduce friction loss, and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion part (30B) to reduce friction loss and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30C) to reduce friction loss and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30D) to reduce friction loss and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30E) to reduce friction loss and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30F) to reduce friction loss and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30G) to reduce friction loss and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30H) to reduce friction loss and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30E) that increases the rotational output by gravity, and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water storage facilities equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water storage equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water storage facilities equipment Various energy conservation cycle coalescence engine.   Various rotational output drives including various hot water storage equipments, including a combined engine combustion section (29A) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various hot water storage equipments, including a combined engine combustion section (29B) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various hot water storage equipments, including a combined engine combustion section (29C) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various hot water storage facilities equipment, including a combined engine combustion section (29D) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various hot water storage facilities equipment, including a combined engine combustion section (29E) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various hot water storage equipments, including a combined engine combustion section (29F) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various hot water storage facilities equipment, including a combined engine combustion section (29G) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various hot water storage facilities equipment with a combined engine combustion section (29H) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various hot water storage facilities equipment with a combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29B) that reduces friction loss by rolling contact, and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and coalescence engine combustion part (29C) to reduce friction loss and various rotary output drive including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and a combined engine combustion section (29D) that reduces friction loss and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29E) that reduces friction loss by rolling contact, and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various hot water storage equipment with a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and a combined engine combustion section (29G) that reduces friction loss and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and coalescence engine combustion part (29H) to reduce friction loss and various rotary output drive including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water storage facilities A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water storage facilities A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) combined engine combustion section (29C) that increases the rotational output by gravity, and various rotary output drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water storage facilities A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water storage facilities A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational power by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water storage facilities A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water storage facilities A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water storage facilities A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G) and various rotary output drive equipment including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) which reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases the rotational output by rolling contact and various rotational outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30B) that increases rotational output by rolling contact, and various rotational outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that increases rotational output by rolling contact, and various rotational outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by rolling contact, and various rotational outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact, and various rotational outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact, and various rotational outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact, and various rotational outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30H) that increases rotational output by rolling contact, and various rotational outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30A) to reduce friction loss, and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30B) to reduce friction loss and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30C) to reduce friction loss and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact part (30D) that reduces friction loss by rolling contact and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact part (30E) that reduces friction loss by rolling contact, and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30F) to reduce friction loss and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30G) to reduce friction loss, and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion part (30H) to reduce friction loss, and various rotational outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30D) that increases rotational output by the gravity of gravity, and various rotary output drive including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30E) that increases the rotational output by gravity, and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30F) that increases the rotational output by gravity, and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping facilities equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping facilities equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by the surface tension of mercury and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various hot water piping facilities equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping equipment equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping facilities equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping equipment equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29D) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping facilities equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping facilities equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping facilities equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various hot water piping facilities equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot water piping facilities equipment Various energy conservation cycle coalescence engine.   Various rotational output drives including various hot water piping facilities equipment, equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various hot water piping facilities equipment with a combined engine combustion section (29B) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various hot water piping facilities equipment, equipped with a combined engine combustion section (29C) that increases rotation output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various hot water piping facilities equipment, equipped with a combined engine combustion section (29D) that increases rotation output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact, and various rotational output drive including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including various hot water piping facilities equipment, equipped with a combined engine combustion section (29F) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various hot water piping facilities equipment, equipped with a combined engine combustion section (29G) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and coalescence engine combustion part (29A) to reduce friction loss and various rotary output drive including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and a combined engine combustion section (29B) that reduces friction loss. Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and combined engine combustion section (29C) that reduces friction loss, and various rotary output drive including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29D) that reduces friction loss by rolling contact, and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have combined engine combustion section (29E) that reduces friction loss by rolling contact, and various rotary output drive including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29G) that reduces friction loss by rolling contact, and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29H) that reduces friction loss by rolling contact, and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined engine combustion section (29E) that increases the rotational output by gravity, and various rotary output drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined rotary combustion drive unit (29H) that increases the rotational output by gravity, and various rotary output drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by water repellent action (3G) and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various chilled water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various chilled water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by surface tension of mercury, and various rotary output drive equipment including various chilled water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various chilled water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot and cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various chilled water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various hot and cold water piping buildings Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30A) to increase rotational output by rolling contact, and various rotational output drive including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact, and various rotational output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30C) that increases rotational output by rolling contact, and various rotational output drive including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all blade combustion section (30D) that increases rotational output by rolling contact, and various rotational output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by rolling contact, and various rotational output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion part (30F) which increases rotational output by rolling contact, and various rotational output drive including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all rotor blade combustion section (30G) which increases rotational output by rolling contact, and various rotational output drive including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30H) that increases rotational output by rolling contact, and various rotational output drive including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade drive unit (30A) that reduces friction loss by rolling contact, and various rotational output drives including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) and all rotor blade combustion section (30B) to reduce friction loss and various rotary output drive including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all rotor blade combustion section (30C) to reduce friction loss Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all rotor blade combustion section (30D) to reduce friction loss. Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade drive part (30E) that reduces friction loss by rolling contact, and various rotary output drive including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade drive unit (30F) that reduces friction loss by rolling contact, and various rotary output drive including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive part (30G) that reduces friction loss by rolling contact, and various rotary output drive including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor drive unit (30H) that reduces friction loss by rolling contact, and various rotational output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30B) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various cold water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30C) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various cold water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30D) that increases the rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various cold water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30E) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various cold water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices including various cold water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various cold water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various chilled water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various cold water piping buildings Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various chilled water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various chilled water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), various rotary output drive equipment including various cold water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cold water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), various rotary output drive equipment including various cold water piping buildings, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various chilled water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cold water piping buildings Energy conservation cycle coalescence engine.   Various rotary output driving equipment including a combined engine combustion section (29A) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various cold water piping buildings A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various chilled water piping buildings equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various chilled water piping buildings with a combined engine combustion section (29C) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various chilled water piping buildings equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various chilled water piping buildings with a combined engine combustion section (29E) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a combined engine combustion section (29F) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various cold water piping buildings A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various chilled water piping buildings with a combined engine combustion section (29G) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various chilled water piping buildings equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion section (29A) to reduce friction loss and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29B) that reduces friction loss and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29C) that reduces friction loss and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29D) that reduces friction loss and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with coalesced engine combustion section (29E) that reduces friction loss and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29F) that reduces friction loss and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29G) that reduces friction loss and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29H) that reduces friction loss and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various chilled water piping buildings with a combined engine combustion section (29A) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various chilled water piping buildings with a combined engine combustion section (29B) that increases the rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various chilled water piping buildings, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various chilled water piping buildings with a combined engine combustion section (29D) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various chilled water piping buildings equipped with a combined engine combustion section (29E) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various chilled water piping buildings with a combined engine combustion section (29F) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various chilled water piping buildings with a combined engine combustion section (29G) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including various chilled water piping buildings with a combined engine combustion section (29H) that increases the rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29A) that reduces friction loss due to surface tension and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29B) that reduces friction loss by surface tension, and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29C) that reduces friction loss due to surface tension and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29D) that reduces friction loss due to surface tension and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) combined engine combustion section (29E) that reduces friction loss by surface tension, and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion part (29F) that reduces friction loss by surface tension, and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29G) that reduces friction loss by surface tension, and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion part (29H) that reduces friction loss by surface tension, and various rotary output drive equipment including various chilled water piping buildings A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G) and various rotary output drive devices including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G) and various rotary output drive devices including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion part (30A) that increases the rotating output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold energy, equipped with all blade combustion section (30B) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with all blade combustion section (30C) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold energy, equipped with all blade combustion section (30D) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion part (30E) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with all blade combustion part (30F) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion part (30G) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases the rotational output by rolling contact, and various rotational outputs including various cooking facilities and equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with all blade combustion part (30A) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with all blade combustion part (30B) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with all blade combustion section (30C) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with all blade combustion part (30D) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion part (30E) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with all blade combustion part (30F) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with all blade combustion part (30G) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with all blade combustion section (30H) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotary outputs including various refrigeration equipment using cold Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Various rotation output drives including a combined engine combustion section (29A) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29B) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment utilizing cold energy Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29C) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29D) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including a combined engine combustion section (29E) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and the high temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29F) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment utilizing cold energy Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29G) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including a combined engine combustion section (29H) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment utilizing cold energy Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various refrigeration equipment using cold heat, equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various refrigeration equipment using cold energy, equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various refrigeration equipment using cold energy, equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various refrigeration equipment using cold energy, equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various refrigeration equipment using cold heat, equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various refrigeration equipment using cold energy with a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various refrigeration equipment using cold energy, equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various refrigeration equipment using cold energy, equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive equipment including various refrigeration equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various refrigeration equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various refrigeration equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various refrigeration equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various refrigeration equipment using cold energy, equipped with a combined engine combustion section (29E) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various refrigeration equipment using cold energy, equipped with a combined engine combustion section (29F) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a refrigeration equipment that uses cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various refrigeration equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30A) that reduces friction loss and various water storage and injection drive devices combined into various energy storage cycles organ.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30B) which reduces friction loss, and various energy storage cycle combined as various water suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30C) that reduces friction loss, and various energy storage cycle combined as various water suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30D) that reduces friction loss, and various energy storage cycle combined as various water suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30E) that reduces friction loss, and various energy storage cycle combined as various water suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion section (30F) that reduces friction loss and various water storage and injection drive devices combined into various energy storage cycle equipment organ.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G), all-blade combustion part (30G) that reduces friction loss, and various energy storage cycle combined as various water suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30H) that reduces friction loss and various energy storage cycle combined with various water suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30A) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all blade storage unit (30B) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30C) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all-oil blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various energy storage cycle coalescing engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30E) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30F) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all blade storage unit (30H) that reduces friction loss due to mercury surface tension.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various energy storage cycle coalescing engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30B) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various energy storage cycle coalescing engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various energy storage cycle coalescing engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-oil blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30A) that increases rotational output by rolling contact with various water suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) and all-blade combustion part (30B) which increases rotational output by rolling contact, and various energy storage as various water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) and all-blade combustion section (30C) that increases rotational output by rolling contact with various types of water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) and all-blade combustion section (30D) that increases rotational output by rolling contact with various types of water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact with various types of water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that increases rotational output by rolling contact, and various energy storage as various water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30G) that increases rotational output by rolling contact with various types of water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) to increase rotational output by rolling contact, and various energy storage as various water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion part (30A) to reduce friction loss, and various energy storage as various water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high-temperature mercury (1d) with all-blade combustion section (30B) to reduce friction loss, and various types of water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high-temperature mercury (1d) with all-blade combustion section (30C) to reduce friction loss and various energy storage as water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion part (30D) to reduce friction loss and various energy storage as various water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high-temperature mercury (1d) with all-blade combustion section (30E) to reduce friction loss, and various energy storage as various water suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30F) to reduce friction loss, and various energy storage as various water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30G) to reduce friction loss, and various energy storage as various water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high-temperature mercury (1d) with all blade combustion part (30H) to reduce friction loss, and various energy storage as various water suction injection drive equipment Cycle coalescence engine.   Various energy storage cycles including various pumps for water suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30A) that increases the rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion part (30B) that increases the rotational output due to the gravity of high-temperature mercury (1d) to provide various water suction injection drive devices. Combined organization.   Various energy storage cycles including various pumps for water suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various pumps for water suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30D) that increases the rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30E) that increases the rotational output by the gravity of high-temperature mercury (1d) to provide various water suction injection drive devices. Combined organization.   Various energy storage cycles including various pumps for water suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various pumps for water suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various pumps for water suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30H) that increases the rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that reduces friction loss by the surface tension of various types of water suction and injection drive equipment. Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various types of energy storage as water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d), and various energy storage as various water suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various energy storage as various water suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) to reduce friction loss by surface tension of high-temperature mercury (1d) Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various energy storage as various water suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various types of energy storage as water suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various types of energy storage as various water suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion unit (29A) that reduces friction loss by water repellent action (3G) and various energy storage cycle coalescence engines as various water suction / injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various energy storage cycle combined engines that are various water suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion unit (29C) that reduces friction loss by water repellent action (3G), and various energy storage cycle coalescence engines as various water suction / injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various energy storage cycle combined engines as various water suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various energy storage cycle combined engines as various water suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various energy storage cycle combined engines as various water suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion unit (29G) that reduces friction loss by water repellent action (3G), and various energy storage cycle coalescence engines as various water suction / injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various energy storage cycle combined engines as various water suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) for reducing friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) for reducing friction loss due to the surface tension of mercury, and various energy storage cycle combined engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, combined with various energy storage cycle drive engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, combined with various energy storage cycle combined engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various energy storage cycle combined engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines that are various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines that are various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss due to rolling contact of mercury, and various energy storage cycle combined engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various water suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various water suction injection drive devices.   Various energy storage cycles comprising a combined engine combustion section (29A) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices. Combined organization.   Various energy storage cycles comprising a combined engine combustion section (29B) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices. Combined organization.   Various energy storage cycles comprising a combined engine combustion section (29C) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices. Combined organization.   Various energy storage cycles comprising a combined engine combustion section (29D) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29E) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29F) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various water suction injection drive devices. Combined organization.   Various energy storage cycles comprising a combined engine combustion section (29G) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29H) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various water suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29A) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29B) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29C) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29D) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29E) that reduces friction loss by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29F) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29G) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29H) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various water suction injection drive devices Combined organization.   Combined with various energy storage cycle units equipped with a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d) and various water suction injection drive devices organ.   Combined with various energy storage cycle units equipped with mercury pump (1E), mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) and used as various water suction injection drive devices organ.   Combined with various energy storage cycle units equipped with a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d) to form various water suction injection drive devices organ.   Combined with various energy storage cycle units equipped with a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29D) that increases the rotational output due to the gravity of high-temperature mercury (1d) to form various water suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), combined with various energy storage cycle units as various water suction / injection drive devices organ.   Combined with various energy storage cycle units equipped with a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29F) that increases the rotational output by the gravity of high-temperature mercury (1d) to form various water suction injection drive devices organ.   Combined with various energy storage cycle units equipped with a mercury pump (1E), a mercury injection pump (6Z) and a combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d) and used as various water suction injection drive devices organ.   Combined with various energy storage cycle units equipped with a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d) to form various water suction injection drive devices organ.   Various energy storage cycles including a mercury pump (1E) mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss due to the surface tension of high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29B) that reduces friction loss by the surface tension of high-temperature mercury (1d) and various water suction injection drive devices. Combined organization.   Various energy storage cycles including a mercury pump (1E) mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including various pumps for water suction and injection with a combined engine combustion section (29D) that reduces friction loss by the surface tension of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles including various pumps for water suction and injection with a combined engine combustion section (29E) that reduces friction loss by the surface tension of the mercury pump (1E), mercury injection pump (6Z) and high-temperature mercury (1d) Combined organization.   Various energy storage cycles including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29F) that reduces friction loss by the surface tension of high-temperature mercury (1d) and various water suction injection drive devices Combined organization.   Various energy storage cycles including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various water suction injection drive devices. Combined organization.   Various energy storage cycles including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29H) that reduces friction loss by the surface tension of high-temperature mercury (1d) and various water suction injection drive devices. Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30A) to reduce friction loss and various water suction injection drives including various types of heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30B) to reduce friction loss and various water suction injection drives including various types of heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30C) to reduce friction loss and various water suction injection drives including various types of heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30D) to reduce friction loss and various water suction injection drives including various types of heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30E) to reduce friction loss and various water suction injection drive including various heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various water suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all rotor blade combustion section (30G) to reduce friction loss and various water suction injection drives including various heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30H) to reduce friction loss and various water suction injection drives including various heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all moving blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact with mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by rolling contact of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all moving blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all moving blade combustion section (30H) that reduces friction loss by rolling contact with mercury, and various water suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) that increases rotational output by rolling contact, and various water suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30B) that increases rotational output by rolling contact, and various water suction including various types of heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that increases rotational output by rolling contact, and various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30D) that increases rotational output by rolling contact, and various types of water suction including various types of heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) which increases rotational output by rolling contact, and various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30F) that increases rotational output by rolling contact, and various water suction including various types of heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30G) that increases rotational output by rolling contact, and various water suction including various heating facilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30H) that increases rotational output by rolling contact, and various types of water suction including various types of heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) to reduce friction loss by rolling contact, and various water suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30B) to reduce friction loss by rolling contact, and various water suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30C) that reduces friction loss by rolling contact, and various water suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30D) that reduces friction loss by rolling contact, and various water suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) to reduce friction loss by rolling contact, and various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30F) that reduces friction loss by rolling contact, and various water suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) to reduce friction loss by rolling contact, and various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30H) that reduces friction loss by rolling contact, and various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d), and various water suction injections including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various water suction injections including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output due to the gravity of high-temperature mercury (1d), and various water suction injections including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), and various water suction injections including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases the rotational output by the gravity of high-temperature mercury (1d), and various water suction injections including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output due to the gravity of high-temperature mercury (1d), and various water suction injections including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d), and various water suction injections including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output due to the gravity of high-temperature mercury (1d), and various water suction injections including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various water suctions including various types of heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various water suctions including various types of heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various water suctions including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various water suctions including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various water suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that reduces friction loss due to surface tension and various water suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various water suctions including various heating equipments using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that reduces friction loss due to surface tension, and various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29A) that reduces friction loss, and various water suction injection drive devices including various types of heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29B) that reduces friction loss and various water suction injection drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion part (29C) to reduce friction loss and various water suction injection drive equipment including various heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29D) that reduces friction loss and various water suction injection drive devices including various types of heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) combined coal combustion combustion section (29E) to reduce friction loss and various water suction injection drive equipment including various heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) combined coal combustion combustion part (29F) to reduce friction loss and various water suction injection drive equipment including various heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion part (29G) to reduce friction loss and various water suction injection drive equipment including various heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29H) that reduces friction loss and various water suction injection drive devices including various types of heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive devices including various heating facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive devices including various heating facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive devices including various types of heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive devices including various heating facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive devices including various heating facility devices using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29G) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact, and various water suction jets including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact, and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact, and various water suction injection including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and various water suction jets including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various water suction jets including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact, and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that reduces friction loss by rolling contact, and various water suction injection including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact, and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact and various water suction jets including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that reduces friction loss by rolling contact, and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that reduces friction loss by rolling contact, and various water suction injection including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that reduces friction loss by rolling contact, and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output due to the gravity of high-temperature mercury (1d), and various water suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output due to the gravity of high-temperature mercury (1d), and various water suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various water suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d), and various water suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various water suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various water suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various water suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output due to gravity of high-temperature mercury (1d), and various water suction injection drives including various heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various water suction injections including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion part (29B) to reduce friction loss by surface tension, various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various water suction injections including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various water suction injections including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various water suction injections including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various water suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various water suction injections including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various water suction injections including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion part (30A) which reduces friction loss by water repellent action (3G) organ.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion part (30B) that reduces friction loss and various energy storage cycle combined with various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion part (30C) that reduces friction loss by water repellent action (3G) and combined with various energy storage cycle as various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion part (30D) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle as various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and all blade storage unit (30E) that reduces friction loss due to water repellent action (3G), combined with various energy storage cycle units as various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle as various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion section (30G) that reduces friction loss and various energy storage cycle combined into various air suction drive equipment organ.   Mercury pump (1E) Mercury injection pump (6Z) and all blade storage unit (30H) that reduces friction loss due to water repellent action (3G), combined with various energy storage cycle units as various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30A) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30B) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30C) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30G) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and all energy storage cycle coalescing engine with all rotor blade combustion section (30A) to reduce friction loss by rolling contact of mercury and various air suction injection drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30B) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and various energy storage cycle coalescing engines that have all blade combustion parts (30C) that reduce friction loss due to rolling contact of mercury and have various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all energy storage cycle coalescing engine with all blade combustion section (30D) to reduce friction loss by rolling contact of mercury and various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30G) that reduces friction loss by rolling contact of mercury and various energy storage cycle coalescing engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and an all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-blade combustion section (30A) that increases the rotational output by rolling contact with various types of air suction and injection drive equipment. Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-blade combustion section (30B) that increases rotational output by rolling contact with various types of air suction and injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) and all-blade combustion section (30C) that increases rotational output by rolling contact, and various energy storage as various air suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact, and various energy storage as various air suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30E) to increase rotational output by rolling contact, and various energy storage as various air suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-blade combustion section (30F) that increases the rotational output by rolling contact with various kinds of air suction and injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-blade combustion section (30G) that increases rotational output by rolling contact with various air-suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-blade combustion section (30H) that increases the rotational output by rolling contact, and various energy storage as various air suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion part (30A) to reduce friction loss, and various energy storage as various air suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30B) to reduce friction loss and various energy storage as various air suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high-temperature mercury (1d) with all-blade combustion section (30C) to reduce friction loss and various types of air suction injection drive equipment to save energy Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high-temperature mercury (1d) with all-blade combustion section (30D) to reduce friction loss, and various energy storage as various air suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion part (30E) to reduce friction loss, and various energy storage as various air suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30F) to reduce friction loss Various energy storage as various air suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30G) to reduce friction loss, and various energy storage as various air suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high-temperature mercury (1d) with all-blade combustion section (30H) to reduce friction loss, and various energy storage as various air suction injection drive devices Cycle coalescence engine.   Various energy storage cycles including various pumps for air suction / injection with a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30A) that increases the rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various pumps for air suction / injection with a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30B) that increases the rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various pumps for air suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various pumps for air suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various air suction / injection drive devices including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various pumps for air suction / injection with a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30F) that increases the rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various pumps for air suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Various energy storage cycles including various pumps for air suction and injection, including a mercury pump (1E), a mercury injection pump (6Z), and a full blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d). Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that reduces friction loss due to surface tension, and various types of energy storage as air suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that reduces friction loss due to surface tension and various types of air suction and injection drive equipment to save energy Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blades combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various energy storage as various air suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various energy storage as various air suction injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that reduces friction loss due to surface tension, and various types of energy storage as air suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) with all-blade combustion section (30G) that reduces friction loss by surface tension of various types of air suction and injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) with all-blade combustion section (30H) that reduces friction loss due to surface tension, and various types of energy storage as air suction injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various energy storage cycle combined engines as various air suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G) and various energy storage cycle combined engines as various air suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29C) that reduces friction loss by water repellent action (3G), and various energy storage cycle combined engines as various air suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), combined with various energy storage cycle combined engines as various air suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various energy storage cycle combined engines as various air suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion unit (29F) that reduces friction loss by water repellent action (3G), and various energy storage cycle combined engines as various air suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G) and various energy storage cycle combined engines as various air suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) and various energy storage cycle combined engines as various air suction injection drive devices .   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, combined with various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, combined with various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion unit (29E) that reduces friction loss due to the surface tension of mercury and various energy storage cycle combined engines that are various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, combined with various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, combined with various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion unit (29B) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) for reducing friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion unit (29E) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines that are various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion unit (29G) that reduces friction loss by rolling contact of mercury and various energy storage cycle combined engines as various air suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion unit (29H) that reduces friction loss due to rolling contact of mercury, and various energy storage cycle combined engines as various air suction injection drive devices.   Various energy storage cycles including a combined engine combustion section (29A) that increases the rotational output by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29B) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29C) that increases rotational output by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29D) that increases the rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29E) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29F) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29G) that increases the rotational output by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29H) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29A) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29B) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29C) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29D) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a combined engine combustion section (29E) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29F) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29G) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices Combined organization.   Various energy storage cycles including a combined engine combustion section (29H) that reduces friction loss by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive devices Combined organization.   Combining various energy storage cycles with various pumps for air suction / injection with a combined engine combustion section (29A) that increases the rotational output by the gravity of the mercury pump (1E), mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d), and various energy storage cycle coalescence as various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), combined with various energy storage cycle units as various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d), combined with various energy storage cycle units as various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d) and various energy storage cycle coalesced as various air suction injection drive devices organ.   Combining various energy storage cycles with various pumps for air suction / injection with a combined engine combustion section (29F) that increases rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) organ.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output due to gravity of high-temperature mercury (1d), and various energy storage cycle coalescing as various air suction injection drive devices organ.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d), combined with various energy storage cycle units as various air suction injection drive devices organ.   Various energy storage cycles including a combined pump combustion unit (29A) that reduces friction loss by the surface tension of the mercury pump (1E), mercury injection pump (6Z) and high-temperature mercury (1d), and various air suction injection drive devices. Combined organization.   Various energy storage cycles including various pumps for air suction and injection with a combined engine combustion section (29B) that reduces friction loss by the surface tension of the mercury pump (1E), mercury injection pump (6Z), and high-temperature mercury (1d) Combined organization.   Various energy storage cycles including various pumps for air suction and injection with a combined engine combustion section (29C) that reduces friction loss by the surface tension of the mercury pump (1E), mercury injection pump (6Z), and high-temperature mercury (1d) Combined organization.   Various energy storage cycles including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29D) that reduces friction loss by the surface tension of high-temperature mercury (1d) and various air suction injection drive devices. Combined organization.   Various energy storage cycles including various pumps for air suction and injection with a combined engine combustion section (29E) that reduces friction loss by the surface tension of the mercury pump (1E), mercury injection pump (6Z), and high-temperature mercury (1d) Combined organization.   Various energy storage cycles including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29F) that reduces friction loss by the surface tension of high-temperature mercury (1d) and various air suction injection drive devices. Combined organization.   Various energy storage cycles including a mercury pump (1E) mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by the surface tension of high-temperature mercury (1d) and various air suction injection drive devices Combined organization.   Various energy storage cycles that include a combined engine combustion section (29H) that reduces friction loss by the surface tension of the mercury pump (1E), mercury injection pump (6Z), and high-temperature mercury (1d), and various air suction injection drive devices. Combined organization.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various types of heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all blade combustion part (30E) to reduce friction loss, and various air suction injection drives including various types of heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all blade combustion part (30G) to reduce friction loss and various air suction injection drives including various heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all-blade combustion section (30H) that reduces friction loss and various air suction injection drives including various types of heating equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various air suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various air suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various air suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to the surface tension of mercury, and various air suction jet drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various air suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various air suction jet drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) which reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various air suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to rolling contact of mercury, and various air suction injection drive equipment including various heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion unit (30H) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various types of heating equipment using heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by rolling contact of high-temperature mercury (1d), and various air suctions including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30B) that increases rotational output by rolling contact, and various air suction including various types of heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by rolling contact of high-temperature mercury (1d), and various air suctions including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30D) that increases rotational output by rolling contact, and various air suctions including various types of heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30E) that increases the rotational output by rolling contact, and various air suctions including various types of heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30F) that increases rotational output by rolling contact, and various air suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30G) that increases the rotational output by rolling contact, and various air suctions including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30H) that increases rotational output by rolling contact, and various air suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion part (30A) that reduces friction loss by rolling contact, and various air suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30B) that reduces friction loss by rolling contact, and various air suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that reduces friction loss by rolling contact, and various air suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30D) that reduces friction loss by rolling contact, and various air suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that reduces friction loss by rolling contact, and various air suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30F) that reduces friction loss by rolling contact, and various air suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) that reduces friction loss by rolling contact, and various air suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30H) that reduces friction loss by rolling contact, and various air suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injections including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injections including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injections including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various heating equipments using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suctions including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that reduces friction loss due to surface tension, and various air suctions including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suctions including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suctions including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that reduces friction loss due to surface tension, and various air suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction including various heating equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29A) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various heating equipments using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29B) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalesced engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) combined coal combustion combustion part (29D) to reduce friction loss and various air suction injection drive devices including various heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29E) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various types of heating equipment using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion section (29G) to reduce friction loss, and various air suction injection drive equipment including various heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion part (29H) to reduce friction loss and various air suction injection drive devices including various heating equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) for reducing friction loss due to the surface tension of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) for reducing friction loss due to the surface tension of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various heating equipments using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) for reducing friction loss due to the surface tension of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various heating equipment using heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various air suction jets including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact, and various air suction jets including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various air suction jets including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact, and various air suction jets including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction jets including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various air suction jets including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various air suction jets including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various air suction jets including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction jets including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various air suction jets including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various air suction jets including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various air suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction jets including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various air suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various air suction jets including various types of heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various air suction jets including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output due to the gravity of high-temperature mercury (1d), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output due to the gravity of high-temperature mercury (1d), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output due to the gravity of high-temperature mercury (1d), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various types of heating equipment using heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction jets including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction jets including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction jets including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction jets including various heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection including various heating equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction jets including various types of heating equipment using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) for reducing friction loss by water repellent action (3G), various air suction injection drive devices including various generators, and Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) for reducing friction loss by water repellent action (3G), various air suction injection drive devices including various generators, and Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) which reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by mercury surface tension, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various generators Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases the rotational output by rolling contact, and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact with various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact, and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment including all generators with all blade combustion section (30D) increasing rotational output by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) which increases the rotational output by rolling contact, and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact, and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment including all generators with all blade combustion section (30G) that increases rotational output by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction injection drive equipment including all generators with all-blade combustion section (30H) that increases rotational output by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30A) to reduce friction loss and various air suction injection drive equipment including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment including all generators with all blade combustion section (30B) to reduce friction loss by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Various air suction jet drive equipment including all generators with all blade combustion part (30C) to reduce friction loss by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment including all generators with all blade combustion part (30D) to reduce friction loss by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all-blade combustion section (30E) to reduce friction loss A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction injection drive equipment including all generators with all blade combustion part (30F) to reduce friction loss by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment including all generators with all blade combustion part (30G) to reduce friction loss by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment including all generators with all blade combustion part (30H) that reduces friction loss by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that increases rotational output by the gravity of various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction / injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various types of energy used as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various types of energy used as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various energy as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and united engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various energy used as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and united engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various energy as various air suction injection drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various types of energy for various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various energies as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various types of energy used as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion part (29B) that reduces friction loss by rolling contact of mercury, and various energy as various air suction injection drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various energy as various air suction injection drive equipment including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various generators Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that increases rotational output by rolling contact, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29C) that increases rotational output by rolling contact, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29D) that increases rotational output by rolling contact, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29B) that reduces friction loss and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion section (29C) that reduces friction loss and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29D) that reduces friction loss and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29E) that reduces friction loss and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29F) to reduce friction loss and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion section (29G) to reduce friction loss and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion section (29H) that reduces friction loss, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29H) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various generators, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined with combustion engine (29A) that reduces friction loss due to surface tension, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined with combustion engine (29F) that reduces friction loss due to surface tension, and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion injection unit (29H) with a combined engine combustion section (29H) that reduces friction loss and various air suction injection drive devices including various generators Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30E) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30H) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to the surface tension of mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to the surface tension of mercury, and various energy used as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, and various types of energy for various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss due to the surface tension of mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to the surface tension of mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion part (30A) that reduces friction loss by rolling contact with mercury, and various energy as various air suction injection drive equipment including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion part (30C) that reduces friction loss by rolling contact of mercury, and various energy as various air suction injection drive equipment including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion part (30E) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact with mercury, and various energies for various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various energies for various air suction injection drive devices including various electric motors Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact, and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) which increases the rotational output by rolling contact, and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact, and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by rolling contact, and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) which increases the rotational output by rolling contact, and various air suction jet drive devices including various motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases the rotational output by rolling contact, and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion part (30G) that increases the rotational output by rolling contact, and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases the rotational output by rolling contact, and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that reduces friction loss by rolling contact and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that reduces friction loss by rolling contact, and various air suction injection drive devices including various motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all blades combustion section (30C) to reduce friction loss Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30D) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30E) to reduce friction loss and various air suction jet drive equipment including various motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) All-blade combustion part (30F) that reduces friction loss and various air suction jet drive equipment including various motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30G) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that reduces friction loss by rolling contact with various air suction injection drive devices including various motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that increases rotational output by the gravity of various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various electric motors Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury and various energy storage as various air suction injection drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury and various energy storage as various air suction injection drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and various energy storage as various air suction injection drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion part (29C) that reduces friction loss by rolling contact of mercury, and various energy storage as various air suction injection drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and various energy storage as various air suction injection drive equipment including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and various energy storage as various air suction injection drive devices including various electric motors Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29C) that increases rotational output by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that increases the rotational output by rolling contact with various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29G) that increases the rotational output by rolling contact with various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29H) that increases rotational output by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various air suction injection drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various air suction jet drive devices including various motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d), combined with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d), combined with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combination engine combustion section (29A) for reducing friction loss by surface tension of high-temperature mercury (1d), various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29B) for reducing friction loss due to surface tension of high-temperature mercury (1d), various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29C) for reducing friction loss by surface tension of high-temperature mercury (1d), various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29E) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various electric motors Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction injection drive devices including various electric motors equipped with combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion unit (30B) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, and various air suction jet drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various air suction jet drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion unit (30B) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) which reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various air suction jet drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) which reduces friction loss by rolling contact of mercury, and various air suction jet drive equipment including various hot water storage equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30A) that increases rotational output by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30C) that increases rotational output by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by rolling contact and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30F) that increases rotational output by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30G) that increases rotational output by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with various blades equipped with all blade combustion section (30H) that increases rotational output by rolling contact and includes various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) that reduces friction loss by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) to reduce friction loss by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) to reduce friction loss by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30D) that reduces friction loss by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that reduces friction loss by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30F) that reduces friction loss by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) to reduce friction loss by rolling contact, various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30H) that reduces friction loss by rolling contact, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that increases rotational output by gravity, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that increases rotational output by gravity, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that increases rotational output by gravity, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that increases the rotational output by gravity, and various air suction injection including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that increases the rotational output by gravity, and various air suction injection including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that reduces friction loss by surface tension, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that reduces friction loss by surface tension, and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that reduces friction loss due to surface tension and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that reduces friction loss by surface tension and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that reduces friction loss due to surface tension and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that reduces friction loss by surface tension and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction including various hot water storage equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29A) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29B) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water storage facilities A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29E) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29H) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water storage equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29D) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29F) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water storage equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water storage equipment devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water storage equipment devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water storage equipment devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water storage facilities Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water storage equipment devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water storage equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water storage equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water storage equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion jet (29A) with combined engine combustion section (29A) that reduces friction loss due to surface tension. Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with combined engine combustion section (29B) to reduce friction loss due to surface tension, and various air suction injection including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion jet (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion injection unit (29D) with a combined engine combustion section (29D) that reduces friction loss due to surface tension Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and a combination engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction jets including various hot water storage equipment with a combined engine combustion section (29G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction jets including various hot water storage equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all blade combustion part (30A) to reduce friction loss and various air suction injection drive including flying around Mach 28 Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various air suction injection drives including flying around Mach 28 around space Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all blade combustion part (30C) to reduce friction loss and various air suction injection drive including flying around Mach 28 around space Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various air suction injection drives including flying around Mach 28 around space Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive equipment including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various air suction injection drive equipment including flying around Mach 28 around the universe Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive equipment including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive equipment including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including flying around space Mach 28 Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various air suction injection drive equipment including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, and various air suction injection drive equipment including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) which reduces friction loss by rolling contact of mercury, and various air suction injection drive equipment including flying around space Mach 28 Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around Mach 28 around space Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion part (30A) that increases rotational output by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) that increases rotational output by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion part (30C) that increases rotational output by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30D) that increases rotational output by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that increases rotational output by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion part (30F) that increases rotational output by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30G) that increases rotational output by rolling contact, and various air suction including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30H) that increases rotational output by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) that reduces friction loss by rolling contact, and various air suction including flight around Mach 28 Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) that reduces friction loss by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that reduces friction loss by rolling contact, and various air suction including flight around Mach 28 Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30D) that reduces friction loss by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that reduces friction loss by rolling contact, and various air suction including flight around Mach 28 Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30F) that reduces friction loss by rolling contact, and various air suction including flight around Mach 28 Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) that reduces friction loss by rolling contact, and various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, and various air suction including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that increases the rotational output by the gravity of gravity, and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that increases rotational output by the gravity of gravity, and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that increases the rotational output by the gravity of gravity, and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that increases the rotational output by the gravity of gravity, and various air suction jets including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30E) that increases rotational output by the gravity of gravity, and various air suction injection including flight around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that increases the rotational output by the gravity of gravity, and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that increases the rotational output by the gravity of gravity, and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that reduces friction loss by surface tension, and various air suction including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that reduces friction loss by surface tension, and various air suction including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion part (30D) that reduces friction loss by surface tension, and various air suction including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30F) that reduces friction loss by surface tension, various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that reduces friction loss by surface tension, and various air suction including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30H) that reduces friction loss by surface tension, various air suction including flying around Mach 28 around space Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29A) that reduces friction loss by water repellent action (3G), and various air suction / injection drive devices including flying around Mach 28 around space A variety of energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29B) that reduces friction loss, and various air suction injection drive devices including flying around the Mach 28 around the universe A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including flying around the space around Mach 28 A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalesced engine combustion part (29D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including flying around the space around Mach 28 A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29E) that reduces friction loss by water repellent action (3G), and various air suction / injection drive devices including flying around the space around Mach 28 A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including flying around the space around Mach 28 A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29G) that reduces friction loss, and various air suction injection drive equipment including flying around the Mach 28 around the universe A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29H) that reduces friction loss by water repellent action (3G), and various air suction / injection drive equipment including flying around the space around Mach 28 A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including flying around space Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including flying around Mach 28 around the universe Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including flying around space Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) for reducing friction loss due to the surface tension of mercury, and various air suction injection drive devices including flying around space Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including flying around the Mach 28 around the universe Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including flying around Mach 28 around the universe Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including flying around the Mach 28 around the universe Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) for reducing friction loss due to the surface tension of mercury, and various air suction injection drive devices including flying around Mach 28 around the universe Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around the space around Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around the space around Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around the space around Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around the space around Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various air suction injection drive equipment including flying around Mach 28 around the universe Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around the space around Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around the space around Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including flying around the space around Mach 28 Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various air suction injection including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various air suction injection including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various air suction injection including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various air suction injection including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various air suction injection including flying around Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various air suction injection including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various air suction injection including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various air suction injection including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction jets including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various air suction injection including flying around Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various air suction jets including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various air suction injection including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction jets including flying around Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various air suction jets including flying around Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various air suction injection including flying around Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various air suction injection including flying around Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases the rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drives including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injections including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that reduces friction loss by surface tension, and various air suction injection including flying around the Mach 28 Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection including flying around Mach 28 around the universe Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all blade combustion part (30E) to reduce friction loss and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by water repellent action (3G), and various air suction injection drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all blade combustion part (30H) to reduce friction loss and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, and various air suction injection drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, and various air suction injection drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) which reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30A) that increases rotational output by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30B) that increases rotational output by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30C) that increases rotational output by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30D) that increases rotational output by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that increases rotational output by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30F) that increases rotational output by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30G) that increases rotational output by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion section (30H) that increases rotational output by rolling contact with various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) that reduces friction loss by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) that reduces friction loss by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that reduces friction loss by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction including various refrigeration equipment using cold air with all blade combustion part (30D) reducing friction loss by rolling contact Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that reduces friction loss by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30F) that reduces friction loss by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) that reduces friction loss by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion part (30H) that reduces friction loss by rolling contact, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that increases rotational output by gravity, and various air suction injection including various refrigeration equipment using cold Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that increases rotational output by gravity, and various air suction injection including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that reduces friction loss due to surface tension, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that reduces friction loss due to surface tension, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that reduces friction loss by surface tension, and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29A) that reduces friction loss and various air suction injection drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29B) that reduces friction loss and various air suction injection drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29C) that reduces friction loss and various air suction injection drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29E) that reduces friction loss and various air suction injection drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion section (29G) to reduce friction loss and various air suction injection drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29H) that reduces friction loss and various air suction injection drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29A) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29C) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various refrigeration equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, and Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, and Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion jet (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion jet (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss due to surface tension, and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with combined engine combustion section (29D) that reduces friction loss due to surface tension, and various air suction injection including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and a combination engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with combined engine combustion section (29G) that reduces friction loss due to surface tension, and various air suction injection including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction jets including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G) and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various air suction jet drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various air suction injection drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, and various air suction injection drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various air suction injection drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various air suction injection drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, and various air suction jet drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to the surface tension of mercury, and various air suction jet drive equipment including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) that increases rotational output by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact with various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases the rotational output by rolling contact and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion part (30D) that increases the rotational output by rolling contact and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30G) that increases rotational output by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30H) that increases rotational output by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) to reduce friction loss by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30B) that reduces friction loss by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) to reduce friction loss by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30D) to reduce friction loss by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that reduces friction loss by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30F) that reduces friction loss by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) that reduces friction loss by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30H) that reduces friction loss by rolling contact, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) and various air suction injection including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that increases rotational output by gravity, and various air suction injection including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that increases rotational output due to gravity, and various air suction injection including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that increases the rotational output by gravity, and various air suction injection including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that increases rotational output by gravity, and various air suction injection including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that increases rotational output by gravity, and various air suction injection including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that reduces friction loss due to surface tension and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that reduces friction loss by surface tension, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30E) that reduces friction loss by surface tension and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that reduces friction loss by surface tension, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that reduces friction loss by surface tension, and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that reduces friction loss by surface tension and various air suction including various hot water piping equipment Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion part (29A) to reduce friction loss and various air suction injection drive equipment including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion part (29B) to reduce friction loss and various air suction injection drive equipment including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29E) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29G) that reduces friction loss by water repellent action (3G) and various air suction injection drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29H) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various hot water piping equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) for reducing friction loss due to mercury surface tension, and various air suction injection drive devices including various hot water piping equipment devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, and various air suction injection drive devices including various hot water piping equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) for reducing friction loss due to mercury surface tension, and various air suction injection drive devices including various hot water piping equipment devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various hot water piping equipment devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various hot water piping equipment devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drives including various hot water piping equipment Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion combustion section (29A) that reduces friction loss due to surface tension, and various air suction injection including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion jet (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion jet (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion jet (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction jets including various hot water piping equipment Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) for reducing friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) for reducing friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) for reducing friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) for reducing friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) for reducing friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to the surface tension of mercury Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various vertical ascent and descent Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various types of air suction injection drive equipment including various vertical ascent and descent Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various vertical ascending and descending Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various vertical ascent and descent Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various vertical ascent and descent Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various vertical ascent and descent Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various vertical ascent and descent Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various air suction injection drive equipment including various vertical ascent and descent Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various types of air suction injection drive equipment including various vertical ascent and descent Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion part (30B) which increases rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact, and various air suction jet drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) which increases the rotational output by rolling contact, and various air suction jet drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases the rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases the rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment with all-blade combustion part (30A) that reduces friction loss by rolling contact and includes various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that reduces friction loss by rolling contact, and various air suction injection drive devices including various vertical ascent and descent A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment that includes all blade combustion part (30C) that reduces friction loss by rolling contact and includes various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30D) that reduces friction loss by rolling contact, and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30E) that reduces friction loss by rolling contact, and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment that has all-blade combustion section (30F) that reduces friction loss by rolling contact and includes various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment with all-blade combustion part (30G) that reduces friction loss by rolling contact and includes various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment with all vertical blade descent equipped with all blade combustion part (30H) to reduce friction loss by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rises and drops Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices that include various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various energies for various air suction injection drive devices including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29D) that reduces friction loss due to the surface tension of mercury, and various energy as various air suction injection drive equipment including various vertical ascending and descending Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined energy combustion unit (29E) that reduces friction loss due to the surface tension of mercury Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined energy combustion unit (29F) that reduces friction loss due to the surface tension of mercury Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various energies as various air suction injection drive devices including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive equipment including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss by rolling contact with mercury, and various energies for various air suction injection drive devices including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss due to rolling contact of mercury, and various energies as various air suction injection drive equipment including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive devices including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact with mercury, and various energies for various air suction injection drive devices including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive equipment including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various energy as various air suction injection drive equipment including various vertical ascent and descent Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various air suction jet drive equipment including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that increases rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction jet drive equipment including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various air suction jet drive equipment including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion part (29B) to reduce friction loss and various air suction jet drive equipment including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29F) that reduces friction loss and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) Rolling contact of high-temperature mercury (1d) with coalesced engine combustion section (29H) that reduces friction loss, and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29B) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that increases the rotational output due to the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29G) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical ascent and descent Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various vertical rise and fall Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion part (30A) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion part (30E) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G) and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss due to mercury surface tension, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss due to mercury surface tension, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact with mercury, and various air suction injection drive devices including various supersonic flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact with various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact, and various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion part (30C) which increases rotational output by rolling contact and various air suction jet drive equipment including various supersonic flight A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) which increases rotational output by rolling contact, and various air suction jet drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact, and various air suction jet drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30F) that increases rotational output by rolling contact with various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact and various air suction jet drive devices including various supersonic flights A variety of energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and various air suction jet drive equipment including all-blade combustion section (30H) that increases rotational output by rolling contact and includes various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that reduces friction loss by rolling contact, and various air suction jet drive devices including various supersonic flights A variety of energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact, and various air suction jet drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion part (30C) that reduces friction loss by rolling contact and various air suction jet drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact, and various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30E) that reduces friction loss by rolling contact and various air suction jet drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that reduces friction loss by rolling contact, and various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) various air suction jet drive equipment including all-supersonic flight with all blade combustion part (30G) to reduce friction loss by rolling contact A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30H) that reduces friction loss by rolling contact and various air suction jet drive devices including various supersonic flights A variety of energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that increases rotational output by the gravity of gravity, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that increases rotational output by gravity, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that increases rotational output by the gravity of gravity, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that increases rotational output by gravity, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that increases rotational output by gravity, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion unit (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion unit (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various air suction jet drive equipment including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion unit (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction jet drive devices including various supersonic flights A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion unit (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction jet drive equipment including various supersonic flights A variety of energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G) and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G) and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion part (29D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G) and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G) and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various energies used as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various energies as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various energies for various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various energies used as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various energies used as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various energies used as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various energies for various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various energies as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29A) that reduces friction loss by rolling contact with mercury, and various energies for various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact with mercury, and various energies for various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various energy as air suction injection drive equipment including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion part (29H) that reduces friction loss by rolling contact of mercury, and various energies as various air suction injection drive devices including various supersonic flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that increases rotational output by rolling contact, and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that increases rotational output by rolling contact, and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29F) that increases rotational output by rolling contact, and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29G) that increases rotational output by rolling contact, and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29H) that increases rotational output by rolling contact, and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29A) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29C) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that increases the rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction jet drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29G) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various supersonic flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion injection unit (29A) with a combined engine combustion section (29A) that reduces friction loss, including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined combustion unit (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined with combustion engine (29C) that reduces friction loss due to surface tension, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion part (29D) that reduces friction loss by surface tension, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion unit (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction jet drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion combustion unit (29F) that reduces friction loss due to surface tension, and various air suction injection drive devices including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion combustion part (29G) that reduces friction loss due to surface tension, and various air suction jet drive equipment including various supersonic flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction jet drive equipment including supersonic flight with coalescence engine combustion part (29H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30G) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various energies for various air suction and injection drive devices including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various energies as various air suction jet drive equipment including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various energy used as various air suction injection drive devices including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various energies as various air suction injection drive devices including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, and various energies for various air suction jet drive equipment including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to the surface tension of mercury, and various energies for various air suction jet drive equipment including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to the surface tension of mercury, and various energies as various air suction injection drive devices including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to the surface tension of mercury, and various energies for various air suction jet drive equipment including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive devices including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive devices including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various energy used as various air suction injection drive equipment including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact with mercury, and various energies for various air suction jet drive equipment including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive devices including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact with mercury, and various energies for various air suction injection drive devices including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive equipment including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion part (30H) that reduces friction loss by rolling contact with mercury, and various energies as various air suction injection drive equipment including various space flights Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30D) that increases rotational output by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30F) that increases rotational output by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion part (30G) that increases the rotational output by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases rotational output by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30B) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30C) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D) and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30E) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30F) to reduce friction loss and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion unit (30G) that reduces friction loss by rolling contact and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact, and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) which increases rotational output by gravity of high temperature mercury (1d), and various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) which increases rotational output by the gravity of high temperature mercury (1d), and various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction jet drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive equipment including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various air suction injection drive devices including various space flights Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G) and various air suction injection drive devices including various space flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion part (29B) to reduce friction loss and various air suction injection drive devices including various space flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various space flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29D) that reduces friction loss and various air suction injection drive devices including various space flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G) and various air suction injection drive devices including various space flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various air suction injection drive devices including various space flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29G) that reduces friction loss and various air suction injection drive devices including various space flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29H) that reduces friction loss and various air suction injection drive devices including various space flights Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury and various energy storage as various air suction injection drive devices including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various energy storage as various air suction injection drive devices including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various energy storage as various air suction injection drive equipment including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury and various energy storage as various air suction injection drive devices including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various energy storage as various air suction injection drive devices including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various energy storage as various air suction injection drive devices including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various energy storage as various air suction injection drive equipment including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various energy storage as various air suction injection drive devices including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and various energy storage as various air suction injection drive equipment including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and various energy storage as various air suction injection drive equipment including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and various energy storage as various air suction injection drive equipment including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various energy storage as various air suction injection drive equipment including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various energy storage as various air suction injection drive equipment including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various energy storage as various air suction injection drive equipment including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various energy storage as various air suction injection drive devices including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various energy storage as various air suction injection drive equipment including various space flights Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29A) that increases the rotational output by rolling contact with various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29B) that increases the rotational output by rolling contact with various air suction injection drive devices including various space flights Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29C) that increases the rotational output by rolling contact with various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29D) that increases rotational output by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29H) that increases the rotational output by rolling contact with various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various air suction jet drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction / injection drive equipment including various space flights equipped with combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction / injection drive equipment including various space flights equipped with combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction jet drive equipment including various space flights equipped with coalescence engine combustion section (29C) that reduces friction loss by surface tension of high temperature mercury (1d), Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined air combustion combustion part (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various air suction injection drive devices including various space flights, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction / injection drive devices including various space flights equipped with combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction / injection drive equipment including various space flights equipped with a combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction jet drive equipment including various space flights equipped with coalescence engine combustion section (29G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and various air suction / injection drive equipment including various space flights equipped with coalescence engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat, Various energy conservation cycle coalescence engine.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion part (30A) that increases the rotating output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion part (30B) that increases the rotary output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact, and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion section (30D) that increases the rotary output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion section (30E) that increases the rotary output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion part (30F) that increases the rotary output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with a whole blade combustion part (30G) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases rotational output by rolling contact, and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with all blade combustion section (30B) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various refrigeration equipment using cold heat, equipped with all blade combustion section (30C) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotational outputs including various refrigeration equipment using cold heat, equipped with all blade combustion part (30D) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) and all rotor blade combustion section (30E) to reduce friction loss. Various energy storage cycle coalescing engines as driving equipment.   Various rotational outputs including various refrigeration equipment using cold heat with mercury blade (1E) mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold and heat, equipped with all-blade combustion section (30G) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various refrigeration equipment using cold heat, equipped with all blade combustion part (30H) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury and various rotary output drive devices including various refrigeration equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various refrigeration equipment using cold heat Various energy conservation cycle coalescence engine.   Various rotational output drives including a combined engine combustion section (29A) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including a combined engine combustion section (29B) that increases rotation output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including a combined engine combustion section (29C) that increases rotation output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including a combined engine combustion section (29D) that increases rotation output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including a combined engine combustion section (29E) that increases rotation output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including a combined engine combustion section (29F) that increases rotation output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including a combined engine combustion section (29G) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including a combined engine combustion section (29H) that increases rotation output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various refrigerating equipment using cold energy with a combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various refrigeration equipment using cold energy, equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various refrigeration equipment using cold heat, equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various refrigeration equipment using cold energy with a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various refrigeration equipment using cold energy with a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various refrigeration equipment using cold energy with a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various refrigeration equipment using cold energy, equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various refrigeration equipment using cold energy with a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive devices including a merging engine combustion section (29A) that increases the rotational output by the gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and includes various refrigeration equipment using cold heat. A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive devices including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various refrigeration equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various refrigeration equipment using cold heat A variety of energy conservation cycle coalescence engine.   Various rotation output drive equipment including various refrigerating equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29F) that increases the rotation output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various refrigeration equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various cooling equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury, and various rotational output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact with mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) which reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold heat, Various energy conservation cycle coalescence engine.   Various rotary outputs including various cooling equipment using cold air with mercury blade (1E) mercury injection pump (6Z) and all blade combustion part (30A) which increases rotary output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade combustion part (30B) that increases the rotary output by rolling contact Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with mercury pump (1E) mercury injection pump (6Z) and all blade combustion section (30C) which increases rotary output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with mercury pump (1E) mercury injection pump (6Z) and all blade combustion part (30D) which increases rotary output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with mercury pump (1E) mercury injection pump (6Z) and all blade combustion part (30E) which increases rotary output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with mercury pump (1E) mercury injection pump (6Z) and all blade combustion part (30F) which increases rotary output by rolling contact with high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade combustion part (30G) that increases the rotary output by rolling contact Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with mercury pump (1E) mercury injection pump (6Z) and all blade combustion part (30H) which increases rotary output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various cooling equipment using cold air with mercury blade (1E) mercury injection pump (6Z) and all blade combustion part (30A) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with a mercury blade (1E) mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with a mercury blade (1E) mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various cooling equipment using cold air with mercury blade (1E) mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade combustion section (30D) that reduces friction loss by rolling contact Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various cooling equipment using cold air with mercury blade (1E) mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade combustion part (30E) that reduces friction loss by rolling contact Various energy storage cycle coalescing engines as driving equipment.   Various rotary outputs including various cooling equipment using cold air with a mercury blade (1E) mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotational outputs including various cooling equipment using cold air with a mercury blade (1E) mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotational outputs including various cooling equipment using cold air with a mercury blade (1E) mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30F) that increases the rotational output by gravity, and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotational outputs including various cooling equipment using cold Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various cooling equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooling equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various cooling equipment using cold energy Various energy conservation cycle coalescence engine.   Various rotation output drives including various cooling equipment using cold heat, equipped with a combined engine combustion section (29A) that increases rotation output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including various cooling equipment using cold air equipped with a combined engine combustion section (29B) that increases rotation output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various cooling equipment using cold energy, equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold air with a combined engine combustion section (29D) that increases rotation output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold air with a combined engine combustion section (29E) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including various cooling equipment using cold air with a combined engine combustion section (29F) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold air with a combined engine combustion section (29G) that increases rotation output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold air equipped with a combined engine combustion section (29H) that increases rotation output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various cooling equipment using cold air with a combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including various cooling equipment using cold air with a combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various cooling equipment using cold air with a combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold air with a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold air with a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold air with a combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold air with a combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various cooling equipment using cold air with a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output driving equipment including various cooling equipment using cold air, equipped with a combined engine combustion section (29A) that increases the rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various cooling equipment using cold air, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various cooling equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various cooling equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various cooling equipment using cold air, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29E) that increases the rotational output by gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various cooling equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various cooling equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various cooling equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various ice making equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various ice making equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various ice making equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various rotary output drive devices including various ice making equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G) and various rotary output drive devices including various ice making equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various ice making equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by water repellent action (3G), and various rotary output drive equipment including various ice making equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various ice making equipment using cold heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat, Various energy conservation cycle coalescence engine.   Various rotation outputs including various ice making equipment using cold heat, equipped with a whole blade combustion part (30A) that increases rotation output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with a whole blade combustion part (30B) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotational outputs including various ice making equipment using cold heat, equipped with all blade combustion part (30C) that increases rotational output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with a whole blade combustion part (30D) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with all blade combustion part (30E) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with a whole blade combustion part (30F) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with a whole blade combustion part (30G) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with a whole blade combustion part (30H) that increases rotating output by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with all blade combustion part (30A) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice-making equipment using cold heat, equipped with all-blade combustion section (30B) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with all blade combustion part (30C) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice-making equipment using cold heat, equipped with all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with all blade combustion part (30E) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice making equipment using cold heat, equipped with all blade combustion part (30F) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice-making equipment using cold heat, equipped with all-blade combustion section (30G) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Various rotating outputs including various ice-making equipment using cold heat, equipped with all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30B) that increases the rotational output by gravity, and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drives including various ice making equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive including various ice making equipment using cold heat Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various ice-making equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various ice making equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various ice making equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational outputs including various ice making equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational outputs including various ice making equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various ice making equipment using cold Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various ice making equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational outputs including various ice making equipment using cold energy Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various ice making equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various ice making equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various ice making equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various ice making equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various ice making equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various ice making equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various ice making equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various ice making equipment using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various ice making equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss due to mercury surface tension, and various rotary output drive devices including various ice making equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various ice making equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various ice making equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various ice making equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various ice making equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various ice making equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various ice making equipment using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various ice making equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various ice making equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various ice making equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various ice making equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various ice making equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various ice making equipment using cold heat Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various ice making equipment using cold heat Various energy conservation cycle coalescence engine.   Various rotational output drives including various ice-making equipment using cold energy, equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including various ice-making equipment using cold energy, equipped with a combined engine combustion section (29B) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various ice-making equipment using cold energy, equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various ice-making equipment using cold energy, equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various ice-making equipment using cold energy, equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various ice-making equipment using cold energy, equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drives including various ice-making equipment using cold energy, equipped with a combined engine combustion section (29G) that increases the rotation output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotational output drives including various ice-making equipment using cold energy, equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various types of ice making equipment using cold heat, equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various types of ice making equipment using cold heat with a combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various ice-making equipment using cold heat with a combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drive including various ice-making equipment using cold heat, equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Various rotary output drives including various types of ice making equipment using cold heat, equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29G) that reduces friction loss by rolling contact, and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Various rotation output drive including various ice-making equipment using cold energy with a combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various ice making equipment using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including various ice making equipment using cold heat, equipped with a combined engine combustion section (29B) that increases rotational output by gravity of mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Various rotary output driving equipment including various types of ice making equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational output drive devices including various ice making equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various ice making equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various rotational output drive devices including various ice making equipment using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive devices including various ice making equipment using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output driving equipment including various types of ice making equipment using cold energy, including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29H) that increases the rotational output by the gravity of high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotational output drives including various ice-making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various ice-making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotational output drives including various ice making equipment using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30A) to reduce friction loss and water jet (78M) as various water suction injection drive equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) provided with all blade combustion part (30B) to reduce friction loss, and water jet (78M) as various water suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30C) to reduce friction loss, water jet (78M) various water suction injection drive equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30D) to reduce friction loss and water jet (78M) as various water suction injection drive equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30E) to reduce friction loss and water jet (78M) as various water suction injection drive equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30F) to reduce friction loss, water jet (78M) various water suction injection drive equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) provide all-blade combustion section (30G) to reduce friction loss, making water jet (78M) various water suction and injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30H) to reduce friction loss, water jet (78M) various water suction injection drive equipment Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water suction and injection drive devices Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to surface tension of mercury, water jet (78M), various types of water suction and injection drive devices Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to the surface tension of mercury, water jet (78M) and various types of water suction and injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water suction and injection drive devices Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water suction and injection drive devices Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water suction and injection drive devices Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss due to the surface tension of mercury, water jet (78M) and various types of water suction and injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water suction and injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury, water jet (78M) various energy used as water suction injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to rolling contact of mercury, water jet (78M), various energy for water suction injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, water jet (78M), various energy for water suction injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury, water jet (78M), various energy for water suction injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, water jet (78M), various energy for water suction injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, water jet (78M), various energy as water suction injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, water jet (78M), various energy for various water suction injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact with mercury, water jet (78M), various types of energy for water suction injection drive equipment Conservation cycle coalescence organization.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion part (30A) which increases rotational output by rolling contact, water jet (78M) various water suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30B) that increases rotational output by rolling contact with water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-blade combustion section (30C) that increases rotational output by rolling contact with water jet (78M) various water suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30D) that increases rotational output by rolling contact with water jet (78M), various water suction and injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact with water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-blade combustion section (30F) that increases rotational output by rolling contact with water jet (78M), various water suction and injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) that increases rotational output by rolling contact, water jet (78M) various water suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-blade combustion section (30H) that increases rotational output by rolling contact with water jet (78M) various water suction and injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30A), water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30C), water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, water jet (78M) various water suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30G), water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30H), water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases the rotational output by the gravity of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M), various water suction / injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M), various water suction and injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases the rotational output by the gravity of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M), various water suction and injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M), various water suction and injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M), various water suction and injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), water jet (78M), various water suction and injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29A) that reduces friction loss, water jet (78M) various water suction injection drive equipment Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29B) to reduce friction loss, water jet (78M) various water suction injection drive equipment Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29C) to reduce friction loss, water jet (78M) various water suction injection drive equipment Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29D) to reduce friction loss, water jet (78M) various water suction injection drive equipment Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29E) that reduces friction loss, water jet (78M), various water suction and injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29F) to reduce friction loss, water jet (78M) various water suction injection drive equipment Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29G) to reduce friction loss, water jet (78M) various water suction injection drive equipment Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29H) that reduces friction loss, water jet (78M) various water suction injection drive equipment Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water suction and injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water storage and injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, water jet (78M) various water suction and injection drive devices and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water suction and injection drive devices Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water suction and injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water storage and injection drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by the surface tension of mercury, water jet (78M) various water suction injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, water jet (78M), various types of water storage and drive equipment Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion part (29A) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion part (29B) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29C) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion part (29D) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) to reduce friction loss by rolling contact of mercury, water jet (78M) various water suction injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction injection drive equipment and various energy storage Cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact with water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact with water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact with water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact with water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases the rotational output by rolling contact, water jet (78M) various water suction injection drive equipment, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact with water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and water jet (78M) various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, water jet (78M) various water suction injection drive equipment, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and water jet (78M) various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and water jet (78M) various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and water jet (78M) various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29D) that reduces friction loss by rolling contact, water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and water jet (78M) various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and water jet (78M) various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that reduces friction loss by rolling contact, water jet (78M) various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and water jet (78M) various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various water suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) and water jet (78M) various water suction / injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and water jet (78M) various water suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and water jet (78M) various water suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) and water jet (78M) various water suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) and water jet (78M) various water suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output due to gravity of high-temperature mercury (1d) and water jet (78M) various water suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) and water jet (78M) various water suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), water jet (78M), various water suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), water jet (78M), various water suction and injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30A) to reduce friction loss, including water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30B) to reduce friction loss, including water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion part (30C) to reduce friction loss, including water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30D) to reduce friction loss, including water heater (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30E) to reduce friction loss and water heater (78M) including various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30F) to reduce friction loss, including water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all rotor blade combustion section (30G) to reduce friction loss, including water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30H) to reduce friction loss, including water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to the surface tension of mercury, water jet (78M), various water including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, water jet (78M) and various waters including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to the surface tension of mercury, water jet (78M), various water including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, water jet (78M) and various types of water including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, water jet (78M) and various waters including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, water jet (78M) and various waters including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, water jet (78M) and various waters including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, water jet (78M) and various waters including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, water jet (78M) and various water including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, water jet (78M) and various water including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, water jet (78M) and various water including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact with mercury, water jet (78M) and various waters including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by rolling contact with mercury, water jet (78M) and various water including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all water blade combustion section (30F) that reduces friction loss by rolling contact with mercury, water jet (78M) and various waters including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact of mercury, water jet (78M) and various waters including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to rolling contact of mercury, water jet (78M) and various waters including various heating equipment using heat Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) that increases rotational output due to rolling contact with water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30B) that increases rotational output by rolling contact with water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that increases rotational output due to rolling contact with water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30D) that increases rotational output by rolling contact with water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30E) that increases rotational output by rolling contact with water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that increases rotational output by rolling contact with water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30G) that increases rotational output by rolling contact with water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30H) that increases rotational output by rolling contact with water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion part (30A) to reduce friction loss, water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30B) to reduce friction loss, water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30C) to reduce friction loss, water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30D) to reduce friction loss and water jet (78M) heating equipments Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30E) to reduce friction loss and various heating equipment using water jet (78M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion part (30F) to reduce friction loss, water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30G) to reduce friction loss, water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30H) to reduce friction loss, water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30C) which increases rotational output by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by the gravity of gravity, water jet (78M) heating equipment that uses heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30E) that increases rotational output by the gravity of high-temperature mercury (1d), water heater (78M) and various heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), water heater (78M), various heating equipment that uses heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases the rotational output due to the gravity of high temperature water (78M) Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), water heater (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29A) that reduces friction loss, water jet (78M) and various types of heating equipment using heat Various energy storage cycle coalescing engine as water suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water jet (78M) coalescence engine combustion section (29B) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as water suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29C) that reduces friction loss, water jet (78M) and various types of heating equipment using heat Various energy storage cycle coalescing engine as water suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29D) that reduces friction loss, water jet (78M) and various types of heating equipment using heat Various energy storage cycle coalescing engine as water suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29E) that reduces friction loss, water jet (78M) and various types of heating equipment using heat Various energy storage cycle coalescing engine as water suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29F) to reduce friction loss, water jet (78M) various types of heating equipment using heat Various energy storage cycle coalescing engine as water suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29G) that reduces friction loss, water jet (78M) and various types of heating equipment using heat Various energy storage cycle coalescing engine as water suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29H) that reduces friction loss, water jet (78M) and various types of heating equipment using heat Various energy storage cycle coalescing engine as water suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, water jet (78M) Various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact with mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) to reduce friction loss by rolling contact of mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact with mercury, water jet (78M) various water suction including various heating equipment using heat Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output due to rolling contact with water jet (78M) and various heating equipment using hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact with water jet (78M) and various heating equipment using hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact with water jet (78M) and various heating equipment using hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact with water jet (78M) and various heating equipment using water heat (78M) Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact with water jet (78M) and various heating equipment using hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact with water jet (78M) and various heating equipment using water heat (78M) Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact with water jet (78M) and various heating equipment that uses hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact with water jet (78M) and various heating equipment that uses hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact with water jet (78M) and various types of heating equipment using heat. Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact with water jet (78M) and various heating equipment using hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a coalesced engine combustion section (29C) that reduces friction loss by rolling contact with water jet (78M) and various heating equipment that uses hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact with water jet (78M) and various heating equipment that uses hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact with water jet (78M) and various heating equipment that uses hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact with water jet (78M) and various types of heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact with water jet (78M) and various heating equipment that uses hot water Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact with water jet (78M) and various types of heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), including various heating equipment using water jet (78M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), including water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output due to gravity of high-temperature mercury (1d), including various heating equipment using water jet (78M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalesced engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), including water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalesced engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), including various heating equipment using water jet (78M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output due to gravity of high-temperature mercury (1d), including various heating equipment using water jet (78M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), including various heating equipment using water jet (78M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output due to gravity of high-temperature mercury (1d), including water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M), various heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d) and water heater (78M) heating equipment using water heating Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), water jet (78M) various heating equipment using heat Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30D) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion part (30G) to reduce friction loss, combined engine injection part (78K) various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) as various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) as various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) as various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by mercury surface tension, combined engine injection section (78K) various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) as various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) as various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) as various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) as various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K), various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K), various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K), various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K), various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have all-blade combustion section (30A) that increases rotational output by rolling contact, and united engine injection section (78K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with an all-blade combustion section (30B) that increases the rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with all blade combustion section (30C) that increases rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a full blade combustion section (30D) that increases the rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have all-blade combustion section (30E) that increases rotational output by rolling contact, and united engine injection section (78K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with an all-blade combustion section (30F) that increases the rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30G) that increases rotational output by rolling contact, combined engine injection section (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with an all-blade combustion section (30H) that increases the rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30A), combined engine injection part (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, combined engine injection part (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, combined engine injection part (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) for reducing friction loss by water repellent action (3G), combined engine injection section (78K) various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K), various types of air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K), various types of air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) various air suction injection drive equipment Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K), various types of air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K), various types of air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K), various types of air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction injection drive devices Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29G) that increases the rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29H) that increases rotational output by rolling contact, and combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29A) that reduces friction loss by rolling contact, combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29B) that reduces friction loss by rolling contact, combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29D) that reduces friction loss by rolling contact, combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29F) that reduces friction loss by rolling contact, combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), various air suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), various air suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), various air suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), various air suction injection drive devices Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G) and united engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G) and united engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30A) that increases the rotational output by rolling contact and includes combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30B) that increases rotational output by rolling contact, and combined engine injection section (78K) includes various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30C) that increases rotational output by rolling contact and includes combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30D) that increases rotational output by rolling contact, combined engine injection section (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30E) that increases rotational output by rolling contact, and combined engine injection section (78K) includes various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30F) that increases the rotational output by rolling contact and includes combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30G) that increases rotational output by rolling contact, and includes combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have all-blade combustion section (30H) that increases the rotational output by rolling contact, and includes combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade combustion part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30B) that reduces friction loss by rolling contact, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade combustion part (30D) that reduces friction loss by rolling contact, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30G) to reduce friction loss by rolling contact, combined engine injection section (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30A) that reduces friction loss due to surface tension, combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion section (30B) that reduces friction loss due to surface tension, combined engine injection section (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion section (30C) that reduces friction loss due to surface tension, combined engine injection section (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30D) that reduces friction loss due to surface tension, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30E) that reduces friction loss due to surface tension, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30F) that reduces friction loss due to surface tension, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion section (30G) that reduces friction loss due to surface tension, combined engine injection section (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30H) that reduces friction loss due to surface tension, combined engine injection part (78K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) have combined engine combustion section (29A) to reduce friction loss, combined engine injection section (78K) Various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) have combined engine combustion section (29B) to reduce friction loss, combined engine injection section (78K) Various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) have combined engine combustion section (29C) to reduce friction loss, combined engine injection section (78K) Various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) have combined engine combustion section (29D) to reduce friction loss, combined engine injection section (78K) Various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) have combined engine combustion section (29E) to reduce friction loss, combined engine injection section (78K) Various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury and combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various combat capabilities Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and a combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and combined engine injection section (78K) various types including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, combined engine injection section (78K) various types including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and combined engine injection section (78K), including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and a combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and combined engine injection section (78K) various types including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and combined engine injection section (78K) various types including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by rolling contact of high-temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and a combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact between high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29D) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and a combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and a combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and a combined engine injection section (78K) with various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29A) that increases rotational output by gravity of high-temperature mercury (1d) and Combined Engine Injection Unit (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output due to the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29D) that increases rotational output by the gravity of high-temperature mercury (1d), Combined Engine Injection Unit (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29E) that increases rotational output by gravity of high-temperature mercury (1d), Combined Engine Injection Unit (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29F) that increases rotational output by gravity of high-temperature mercury (1d) and Combined Engine Injection Unit (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all blade combustion part (30A) to reduce friction loss, combined engine injection part (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30B) to reduce friction loss, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30C) to reduce friction loss, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30D) to reduce friction loss, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30E) to reduce friction loss, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion part (30F) to reduce friction loss, combined engine injection part (78K) Various types including various air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30G) to reduce friction loss, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various types including various air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various air combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30A) that increases the rotational output by rolling contact, combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with all blade combustion section (30B) that increases the rotation output by rolling contact, combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30C) that increases rotational output by rolling contact, combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30D) that increases the rotational output by rolling contact, combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30E) that increases rotational output by rolling contact, combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30F) that increases the rotational output by rolling contact, and the combined engine injection section (78K) has various air combat capabilities. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30G) that increases rotational output by rolling contact, and combined engine injection section (78K) has various air combat capabilities. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) that increases the rotation output by rolling contact, combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30A), combined engine injection part (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30B) that reduces friction loss by rolling contact, combined engine injection part (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling all-blade combustion section (30C) that reduces friction loss by rolling contact, combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade combustion part (30G) that reduces friction loss by rolling contact, combined engine injection part (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) to reduce friction loss by rolling contact, combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30D) that increases the rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30G) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) including various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion section (30A) that reduces friction loss due to surface tension, combined engine injection section (78K) with various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) that reduces friction loss by surface tension, combined engine injection part (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that reduces friction loss by surface tension, combined engine injection part (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30D) that reduces friction loss by surface tension, combined engine injection part (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) equipped with all-blade combustion section (30E) that reduces friction loss by surface tension, combined engine injection section (78K) with various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by mercury surface tension, combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury and combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various air combat capabilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29G) that increases the rotational output by rolling contact, and includes a combined engine injection section (78K) with various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29A) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29B) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29C) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29D) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29E) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29F) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29G) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29H) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including various air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including various air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including various air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including various air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including various air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including various air combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with combined engine combustion section (29A) that reduces friction loss due to surface tension, combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with combined engine combustion section (29C) that reduces friction loss due to surface tension, combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29D) that reduces friction loss due to surface tension, and combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with combined engine combustion section (29E) that reduces friction loss due to surface tension, combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with combined engine combustion section (29F) that reduces friction loss due to surface tension, combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) combined coal combustion combustion part (29G) that reduces friction loss due to surface tension, combined engine injection part (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with combined engine combustion section (29H) that reduces friction loss due to surface tension, combined engine injection section (78K) includes various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) and various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cockpits Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all-blade combustion section (30A) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30B) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30C) that increases rotational output by rolling contact and includes combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30G) that increases rotational output by rolling contact and includes combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact and includes combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30B) to reduce friction loss by rolling contact, combined engine injection part (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30D) that reduces friction loss by rolling contact, combined engine injection part (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30E) to reduce friction loss by rolling contact, combined engine injection part (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30F) to reduce friction loss by rolling contact, combined engine injection part (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30H) to reduce friction loss by rolling contact, combined engine injection part (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases the rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by gravity, and various types including combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and combined engine injection section (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion part (30D) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection part (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), including combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30G) to reduce friction loss due to surface tension, combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cockpits Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact, and various types including combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact, and various types including combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion part (29A) that reduces friction loss by rolling contact, combined engine injection part (78K) Various types including cockpit Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion unit (29E) that reduces friction loss by rolling contact, and various types including a combined engine injection unit (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by rolling contact of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases the rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various air including various cockpits Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), various air including various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) which reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), various air including various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), various air including various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) and various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) and various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) and various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss due to surface tension of mercury, combined engine injection section (78K) various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) and various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) and various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) and various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) and various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various control chambers Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all-blade combustion section (30A) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30B) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30C) that increases rotational output by rolling contact and includes combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with all-blade combustion section (30E) that increases the rotational output by rolling contact, and includes combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with rolling blade combustion part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30G) that increases rotational output by rolling contact and includes combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact and includes combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30A) that reduces friction loss by rolling contact and includes combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade combustion part (30B) to reduce friction loss by rolling contact, combined engine injection part (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30D) to reduce friction loss by rolling contact, combined engine injection part (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact section (30E) that reduces friction loss by rolling contact, combined engine injection section (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30G) that reduces friction loss by rolling contact, combined engine injection part (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), including combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that reduces friction loss due to surface tension, combined engine injection section (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), including combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and combined engine injection section (78K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), including combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d), including combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various control chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various control chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various control chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various control chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various control chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various control chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various control chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various control chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drives including various control chambers Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by rolling contact of high-temperature mercury (1d), combined engine injection section (78K), including various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of high-temperature mercury (1d), combined engine injection section (78K), including various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various types including a combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air including combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d), and various air including coalescence engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air including coalescence engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air including combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various air including various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), and various air including coalescence engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air including combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) and various engine air including coalescence engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30A) to reduce friction loss and combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all blade combustion part (30E) to reduce friction loss, combined engine injection part (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30G) to reduce friction loss and combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30H) to reduce friction loss and combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various space travel Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30A) to increase rotational output by rolling contact, and combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30B) to increase rotational output by rolling contact, combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30C) that increases rotational output due to rolling contact with combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30D) to increase rotational output by rolling contact, combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30E) to increase rotational output by rolling contact, combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30F) that increases rotational output by rolling contact, and combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30G) to increase rotational output by rolling contact, and combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact with combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30A), combined engine injection part (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30C) to reduce friction loss, combined engine injection section (78K) including various space travel Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high-temperature mercury (1d) with all-blade combustion part (30D) to reduce friction loss, combined engine injection part (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30F), combined engine injection part (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30G) that reduces friction loss by rolling contact, combined engine injection part (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various types including various space trips Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various types including various space trips Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including various space trips Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various types including various space trips Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various types including various space trips Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that increases the rotational output by the gravity of gravity, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various types including various space trips Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion section (30B) that reduces friction loss by surface tension, combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30C) that reduces friction loss due to surface tension, combined engine injection part (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30D) that reduces friction loss by surface tension, combined engine injection part (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion section (30E) that reduces friction loss by surface tension, combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various space travel Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) equipped with all-blade combustion section (30H) that reduces friction loss by surface tension, combined engine injection section (78K) including various space trips Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various space trips Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various space travel Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various space travel Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various space travel Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various space trips Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various space trips Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various space trips Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various space travel Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various space trips Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various space trips Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various space trips Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drives including various space trips Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various space trips Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various space trips Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various space travel Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and combined engine injection section (78K) various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29B) that increases the rotational output by rolling contact, and combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact, and combined engine injection section (78K) Various types including various space trips Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29A) that reduces friction loss by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29B) that reduces friction loss by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29D) that reduces friction loss by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact between high-temperature mercury (1d) and combined engine injection section (78K) Various types including space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29F) that reduces friction loss by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various types including space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various space trips Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various space trips Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various space trips Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output due to the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air including various space travel Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) and combined engine injection section (78K) Various types including various space trips Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various types including space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) and combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various types including various space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) to reduce friction loss by water repellent action (3G) and combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30H) to reduce friction loss and combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection drives including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive including various cabins Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drive including various guest rooms Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30A) that increases rotational output by rolling contact and various types including united engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotational output by rolling contact, and various engine including combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30C) that increases rotational output by rolling contact, and various types including united engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact and various types including combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact and various types including combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that increases rotational output by rolling contact, various types including united engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30G) that increases rotational output by rolling contact and various types including united engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact and various types including united engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30A) to reduce friction loss, combined engine injection section (78K), including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30B) to reduce friction loss, combined engine injection section (78K), including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30C) to reduce friction loss by rolling contact, various types including united engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30D) that reduces friction loss by rolling contact and various engine including combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30E) to reduce friction loss by rolling contact and various types including combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that reduces friction loss by rolling contact and various engine including combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30G) to reduce friction loss by rolling contact, various types including united engine injection section (78K) various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30H) to reduce friction loss, combined engine injection section (78K) Various types including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) whose rotational output is increased by the gravity of gravity, combined engine injection section (78K) various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that reduces friction loss by surface tension, combined engine injection section (78K), including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that reduces friction loss by surface tension, combined engine injection section (78K) Various types including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that reduces friction loss due to surface tension, combined engine injection section (78K), including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that reduces friction loss by surface tension, combined engine injection section (78K), including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that reduces friction loss by surface tension, combined engine injection section (78K), including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that reduces friction loss due to surface tension, combined engine injection section (78K), including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that reduces friction loss by surface tension, combined engine injection section (78K), including various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection drive devices including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drive devices including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drive equipment including various guest rooms A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29A) that increases rotational output by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29B) that increases rotational output by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by rolling contact of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various air including combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various air including combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases the rotation output by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotation output by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29A) that reduces friction loss by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29B) to reduce friction loss by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29C) that reduces friction loss by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29D) that reduces friction loss by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29E) that reduces friction loss by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29F) to reduce friction loss by rolling contact, combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29G) that reduces friction loss by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have combined engine combustion section (29H) that reduces friction loss by rolling contact, and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29C) that increases rotational output due to the gravity of high-temperature mercury (1d) and Combined Engine Injection Unit (78K) Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) and combined engine injection section (78K) Various air suction including various guest rooms Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29A) that reduces friction loss by surface tension, combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29B) that reduces friction loss by surface tension, combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) Various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction injection including various cargo compartments Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30A) to increase rotational output by rolling contact, and combined engine injection section (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30B) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all-blade combustion section (30C) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30D) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that increases rotational output by rolling contact, and includes combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30G) that increases rotational output by rolling contact and includes combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact and includes combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade combustion part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30B) to reduce friction loss by rolling contact, combined engine injection section (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade combustion part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30D) to reduce friction loss by rolling contact, combined engine injection part (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade combustion part (30E) that reduces friction loss by rolling contact, combined engine injection part (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade combustion part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) and various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30A) to reduce friction loss due to surface tension, combined engine injection section (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that reduces friction loss due to surface tension, combined engine injection section (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that reduces friction loss due to surface tension, combined engine injection section (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30D) that reduces friction loss due to surface tension, combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) with all-blade combustion section (30E) to reduce friction loss due to surface tension, and combined engine injection section (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30F) that reduces friction loss due to surface tension, combined engine injection section (78K), including various cargo chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) to reduce friction loss due to surface tension, combined engine injection section (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cargo chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cargo chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cargo chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cargo compartments Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cargo compartments Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cargo compartments Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cargo compartments Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air suction including various cargo chambers Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection drives including various cargo compartments Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact, and various types including a combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and various types including a combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various types including a combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact between high-temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and various types including combined engine injection section (78K) various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29B) that increases rotational output due to the gravity of high-temperature mercury (1d), Combined Engine Injection Unit (78K) Various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29D) that increases rotational output by the gravity of high-temperature mercury (1d), and Combined Engine Injection Unit (78K) Various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29E) that increases rotational output due to the gravity of high-temperature mercury (1d), Combined Engine Injection Unit (78K) Various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29F) that increases rotational output by the gravity of high-temperature mercury (1d), and Combined Engine Injection Unit (78K) Various Air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), various air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury Pump (1E) Mercury Injection Pump (6Z) and Combined Engine Combustion Unit (29H) that increases rotational output due to the gravity of high-temperature mercury (1d), Combined Engine Injection Unit (78K) Various Air including various cargo compartments Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K), including various cargo compartments Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30E) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion part (30H) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by the surface tension of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K), various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by the surface tension of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss due to the surface tension of mercury, combined engine injection section (78K), various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K), various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by the surface tension of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30A) that increases the rotational output by rolling contact, and the combined engine injection part (78K) has various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30B) that increases the rotational output by rolling contact, and the combined engine injection part (78K) has various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30C) that increases the rotational output by rolling contact, and the combined engine injection section (78K) has various vertical ascent and descent. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30D) that increases the rotational output by rolling contact, and the combined engine injection part (78K) has various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30E) that increases the rotational output by rolling contact, and the combined engine injection section (78K) has various vertical rises and drops Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that increases the rotational output by rolling contact, combined engine injection section (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30G) that increases the rotational output by rolling contact, and the combined engine injection part (78K) has various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30H) that increases rotational output by rolling contact with the combined engine injection part (78K). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30C), combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion part (30D) that reduces friction loss by rolling contact, combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, combined engine injection part (78K) various vertical ascent and descent Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30A) that reduces friction loss due to surface tension, combined engine injection section (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30C) that reduces friction loss due to surface tension, combined engine injection section (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30D) that reduces friction loss due to surface tension, combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with full blade combustion part (30E) that reduces friction loss due to surface tension, combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30F) that reduces friction loss by surface tension, combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with full blade combustion part (30G) to reduce friction loss by surface tension, combined engine injection part (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury and combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury and combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact, and combined engine injection section (78K) includes various vertical rises and drops Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29C) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29D) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29E) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29F) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29G) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29H) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), including various vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30A) to reduce friction loss, combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various vertical ascent and descent anywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various vertical ascent and descent anywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) various vertical rising and falling everywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various vertical rising and falling everywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various vertical ascent and descent includes airfield anywhere Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various vertical ascent and descent includes airfield anywhere Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various vertical ascent and descent includes airfield anywhere Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various vertical ascent and descent includes airfield anywhere Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various vertical ascent and descent includes airfield anywhere Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various vertical ascent and descent includes airfield anywhere Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by the surface tension of mercury, combined engine injection section (78K) Various vertical ascent and descent, including airfield anywhere Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various vertical ascent and descent includes airfield anywhere Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical ascent and descent anywhere including airfield Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical ascent and descent anywhere including airfield Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various vertical ascent and descent anywhere including airfield Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical ascent and descent anywhere including airfield Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical ascent and descent anywhere including airfield Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical ascent and descent anywhere including airfield Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical ascent and descent anywhere including airfield Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical ascent and descent anywhere including airfield Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion part (30A) that increases rotational output by rolling contact, combined engine injection part (78K) various vertical rising and falling But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30B) to increase rotational output by rolling contact, combined engine injection section (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that increases rotational output by rolling contact, combined engine injection part (78K) various vertical rising and falling But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output due to rolling contact with combined engine injection section (78K) But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact, combined engine injection section (78K) But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30F) that increases rotational output by rolling contact, combined engine injection section (78K) various vertical rising and falling But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30G) to increase the rotational output by rolling contact, combined engine injection section (78K) various vertical rising and falling But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact, combined engine injection section (78K) But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30A) to reduce friction loss by rolling contact, combined engine injection section (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30B) to reduce friction loss by rolling contact, combined engine injection section (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all-blade combustion section (30C) to reduce friction loss But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K) But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion part (30E) to reduce friction loss by rolling contact, combined engine injection part (78K) various vertical rising and falling But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) with all blade combustion part (30F) to reduce friction loss, combined engine injection part (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30G), combined engine injection part (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact of high temperature mercury (1d) with all blade combustion part (30H) to reduce friction loss, combined engine injection part (78K) But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall everywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), various vertical rise and fall everywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), various vertical rises and falls anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases the rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K), various vertical rise and fall everywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall everywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling everywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion part (30C) to reduce friction loss by surface tension, combined engine injection part (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that reduces friction loss by surface tension, combined engine injection section (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion part (30H) that reduces friction loss by surface tension, combined engine injection part (78K) But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various vertical ascent and descent wherever you go Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) have combined engine combustion section (29B) to reduce friction loss, combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29C) that reduces friction loss, combined engine injection section (78K) various vertical rising and falling anywhere in the airfield Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) have combined engine combustion section (29D) to reduce friction loss, combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) have combined engine combustion section (29E) to reduce friction loss, combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various vertical ascent and descent wherever you go Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) have combined engine combustion section (29H) to reduce friction loss, combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various vertical ascent and descent anywhere including airfield Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various vertical lifts and various places including airfields Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various vertical lifts and various places including airfields Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical ascents and various places including airfields Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical lifts and various places including airfields Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical ascent and various places including airfield Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical lifts and various places including airfields Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various vertical lifts and various places including airfields Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, combined engine injection section (78K) various vertical rise and fall anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29B) that reduces friction loss by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29D) that reduces friction loss by rolling contact, and combined engine injection section (78K) various vertical ascent and descent anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) various vertical rise and fall anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling everywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling everywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical ascent and descent everywhere Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling everywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling everywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling everywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling everywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling everywhere airfield Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29F) that reduces friction loss by surface tension, combined engine injection section (78K) various vertical rise and fall anywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rise and fall Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various vertical rising and falling everywhere Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) all-blade combustion section (30C) that reduces friction loss, combined engine injection section (78K), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30G) to reduce friction loss, combined engine injection section (78K), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K), various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K), various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) which reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30A) that increases the rotational output by rolling contact with the combined engine injection section (78K) and various satellite installations. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30B) that increases the rotational output by rolling contact with the combined engine injection section (78K) and various satellite installations. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with an all-blade combustion section (30C) that increases the rotational output by rolling contact with the combined engine injection section (78K) and various satellite installations. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30D) that increases the rotational output by rolling contact with the combined engine injection section (78K) and various satellite installations. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30E) that increases the rotational output by rolling contact with the combined engine injection section (78K) and various satellite installations. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion part (30F) that increases rotational output by rolling contact, and combined engine injection part (78K) various satellite installations Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with an all-blade combustion section (30G) that increases the rotational output by rolling contact with the combined engine injection section (78K) and various satellite installations. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30H) that increases the rotational output by rolling contact with the combined engine injection section (78K) and various satellite installations. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30A), combined engine injection part (78K) various satellite installations Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K) various artificial satellite installation Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K) various artificial satellite installation Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K) various artificial satellite installation Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K), various satellite installations Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K) various artificial satellite installation Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K) various artificial satellite installation Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K) various artificial satellite installation Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion section (30C) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion part (30G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection part (78K) including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion part (30H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection part (78K) including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30A) that reduces friction loss due to surface tension, combined engine injection section (78K) and various satellite installations Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30B) that reduces friction loss by surface tension, combined engine injection section (78K) various artificial satellite installation Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30C) that reduces friction loss due to surface tension, combined engine injection section (78K) and various satellite installations Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30D) that reduces friction loss due to surface tension, combined engine injection section (78K) and various satellite installations Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30E) that reduces friction loss by surface tension, combined engine injection section (78K) various artificial satellite installations Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30F) that reduces friction loss by surface tension, combined engine injection section (78K) various artificial satellite installation Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30G) that reduces friction loss due to surface tension, combined engine injection section (78K) and various satellite installations Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30H) that reduces friction loss by surface tension, combined engine injection section (78K) various artificial satellite installation Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by mercury surface tension, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact, and includes a combined engine injection section (78K) with various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact, and includes a combined engine injection section (78K) with various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and a combined engine injection section (78K) includes various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and a combined engine injection section (78K) includes various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and a combined engine injection section (78K) includes various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact, and the combined engine injection section (78K) includes various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and a combined engine injection section (78K) includes various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact, and includes a combined engine injection section (78K) with various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact, and a combined engine injection section (78K) includes various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and a combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and a combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and a combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and a combined engine injection section (78K) includes various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and a combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and a combined engine injection section (78K) includes various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and a combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29A) that reduces friction loss due to surface tension, and coalescence engine injection section (78K) including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with combined engine combustion section (29B) that reduces friction loss by surface tension, combined engine injection section (78K) including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high temperature mercury (1d), combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that reduces friction loss due to surface tension, combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to surface tension of high temperature mercury (1d), combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with combined engine combustion section (29G) that reduces friction loss by surface tension, combined engine injection section (78K) including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with combined engine combustion section (29H) that reduces friction loss due to surface tension, combined engine injection section (78K) including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including lunar landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including lunar landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including lunar landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including lunar landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including lunar landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion part (30F) to reduce friction loss, combined engine injection part (78K), including lunar landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including lunar landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K), including lunar landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction including moon landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction including moon landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including moon landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction including lunar landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction including moon landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction including lunar landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction including moon landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K), various air suction including lunar landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including lunar landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including lunar landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) various air suction including lunar landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction including lunar landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) various air suction including lunar landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including moon landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) various air suction including moon landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including moon landing start Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30A) that increases rotational output due to rolling contact, combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30B) that increases rotational output by rolling contact, combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30C) that increases rotational output by rolling contact, and united engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30D) that increases rotational output due to rolling contact, combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30E) that increases rotational output by rolling contact, and united engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30F) that increases rotational output by rolling contact, combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30G) that increases rotational output by rolling contact, and united engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30H) that increases rotational output by rolling contact, and united engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling rotor contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) that reduces friction loss by rolling contact, combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30C) that reduces friction loss by rolling contact, and united engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30E) that reduces friction loss by rolling contact, and united engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30F) to reduce friction loss by rolling contact, combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30H) that reduces friction loss by rolling contact, and united engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output due to gravity of high-temperature mercury (1d), including combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output due to gravity of high-temperature mercury (1d), including combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), including combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), including combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), including combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output due to gravity of high-temperature mercury (1d), including combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30G) that increases rotational output due to gravity of high-temperature mercury (1d), including combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), including combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion section (30A) that reduces friction loss due to surface tension, combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) that reduces friction loss by surface tension, combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) to reduce friction loss by surface tension, combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion section (30D) that reduces friction loss due to surface tension, combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) moon landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30F) that reduces friction loss due to surface tension, combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) moon landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all blade combustion part (30H) that reduces friction loss by surface tension, combined engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including moon landing start Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including moon landing start Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including moon landing start Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including moon landing start Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including moon landing start Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including moon landing start Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including moon landing start Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) various air including moon landing start Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Moon landing with mercury pump (1E) mercury injection pump (6Z) and coalescence engine injection part (78K) coalescence engine injection part (78K) coalescence engine combustion part (29G) to reduce friction loss by surface tension of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices including start.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by mercury surface tension, combined engine injection section (78K) various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including lunar landing start Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact, and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact, and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact, and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and includes a combined engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) and various types including moon landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various types of landing on the moon Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) and various types including moon landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) including various types of landing on the moon Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) and various types including moon landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) and various types including moon landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) and various types including moon landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K), including lunar landing start Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion part (29A) that reduces friction loss by surface tension of high-temperature mercury (1d), including coalescence engine injection part (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) to reduce friction loss by surface tension of high-temperature mercury (1d), including coalescence engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), including coalescence engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), including coalescence engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) to reduce friction loss due to surface tension, including coalescence engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d), including coalescence engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion part (29G) to reduce friction loss by surface tension, and coalescence engine injection part (78K) including lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d), including coalescence engine injection section (78K) lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30D) to reduce friction loss, combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30G) to reduce friction loss, combined engine injection section (78K) various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30H) to reduce friction loss and combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact with mercury, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30A) that increases the rotational output by rolling contact, and combines engine injection part (78K) for various supersonic flights. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) that increases rotational output by rolling contact, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30C) that increases the rotational output by rolling contact with the combined engine injection section (78K) for various supersonic flights. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30D) that increases the rotational output by rolling contact with the combined engine injection section (78K) for various supersonic flights. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that increases rotational output by rolling contact, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30F) that increases the rotational output by rolling contact with the combined engine injection section (78K) for various supersonic flights. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30G) that increases the rotational output by rolling contact with the combined engine injection part (78K) for various supersonic flights. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30H) that increases the rotational output by rolling contact with the combined engine injection section (78K) for various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30A) that reduces friction loss by rolling contact, combined engine injection section (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30B) that reduces friction loss by rolling contact, and combined engine injection section (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30C), combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a full blade combustion part (30D) that reduces friction loss by rolling contact, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with an all-blade combustion section (30F) that reduces friction loss by rolling contact, and combined engine injection section (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30G), combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30D) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full blade combustion section (30G) that increases rotational output due to gravity of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) that reduces friction loss by surface tension, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-pressure mercury (1d) with all-blade combustion section (30C) to reduce friction loss by surface tension, combined engine injection section (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30D) that reduces friction loss by surface tension, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that reduces friction loss by surface tension, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30F) that reduces friction loss due to surface tension, combined engine injection section (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) that reduces friction loss by surface tension, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30H) that reduces friction loss due to surface tension, combined engine injection part (78K) various supersonic flight Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G) and combined engine injection section (78K) Various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) to reduce friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury and combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury and combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by mercury surface tension, combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and combined engine injection section (78K) Various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases the rotational output by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29A) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact between high-temperature mercury (1d) and coalescence engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have a combined engine combustion section (29D) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact between high-temperature mercury (1d) and coalescence engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29H) that reduces friction loss by rolling contact, and combined engine injection section (78K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K), including various supersonic flights Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to surface tension of high temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) to reduce friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), combined engine injection section (78K) including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G) and various rotational outputs including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G) and various rotational outputs including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotational outputs including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G) and various rotational outputs including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various rotational outputs including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotational outputs including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G) and various rotational outputs including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various rotational outputs including various methane hydrate decomposition and recovery facilities using heat Various energy storage cycle coalescing engines as driving equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities utilizing heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities utilizing heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities utilizing heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various rotary output drive devices including various methane hydrate decomposition and recovery facilities using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities utilizing heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities utilizing heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities utilizing heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various methane hydrate decomposition and recovery facilities using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane hydrate decomposition and recovery facilities using heat A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various thermal methane hydrate decomposition and recovery facilities A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases the rotational output by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29B) that reduces friction loss by rolling contact, including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact, including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact, and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that reduces friction loss by rolling contact, including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29G) that reduces friction loss by rolling contact, including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29H) that reduces friction loss by rolling contact, including various types of methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotations including various methane hydrate decomposition and recovery facilities utilizing thermal energy Various energy storage cycle coalescence engine as output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotations including various methane hydrate decomposition and recovery facilities utilizing thermal energy Various energy storage cycle coalescence engine as output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotations including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescence engine as output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotations including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescence engine as output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotations including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescence engine as output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output due to gravity of high-temperature mercury (1d), and various rotations including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescence engine as output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotations including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescence engine as output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotations including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescence engine as output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various types including thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various types including thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various types including methane hydrate decomposition and recovery facilities utilizing thermal energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various types including methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss due to mercury surface tension, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to mercury surface tension, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact, and various rotational output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30B) that increases rotational output by rolling contact, and various rotational output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30C) that increases rotational output by rolling contact, and various rotational output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30D) that increases rotational output by rolling contact, and various rotational output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30E) that increases rotational output by rolling contact, and various rotational output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have all rotor blade combustion section (30F) that increases the rotational output by rolling contact, and various rotational output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) that increases rotational output by rolling contact, and various rotational output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30H) that increases rotational output by rolling contact, and various rotational output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30A) that reduces friction loss by rolling contact, and various rotary output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have all blade combustion section (30B) that reduces friction loss by rolling contact, and various rotational output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have all blade combustion part (30C) to reduce friction loss by rolling contact, and various rotational output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) have all-blade combustion section (30D) that reduces friction loss by rolling contact, and various rotational output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30E) that reduces friction loss by rolling contact, and various rotational output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that reduces friction loss by rolling contact, and various rotary output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) have all rotor blade combustion section (30G) that reduces friction loss by rolling contact, and various rotary output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) that reduces friction loss by rolling contact, and various rotational output drive including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30A) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30E) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all-rotary blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotational output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that increases the rotational output by the gravity of high-temperature mercury (1d), and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d), and various rotary output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drives including methane recovery cooling using cold energy Various energy storage cycle coalescing engines as equipment.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), various rotary output drive equipment including various methane recovery cooling using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various methane recovery cooling using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various methane recovery cooling using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), various rotary output drive equipment including various methane recovery cooling using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotary output drive equipment including various methane recovery cooling using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various rotary output drive devices including various methane recovery cooling using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), various rotary output drive equipment including various methane recovery cooling using cold energy, Various energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury. Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury. Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury. Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and a combined engine combustion section (29H) that reduces friction loss by rolling contact with mercury, and various rotary output drive equipment including various methane recovery cooling using cold energy Energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29A) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29B) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29C) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29D) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29E) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29F) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29G) that increases rotational output by rolling contact of a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment including a combined engine combustion section (29H) that increases the rotational output by rolling contact of the mercury pump (1E) mercury injection pump (6Z) and the high-temperature mercury (1d), including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive equipment that includes a combined engine combustion section (29A) that reduces friction loss by rolling contact between a mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29B) to reduce friction loss and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29C) that reduces friction loss by rolling contact, and various rotary output drive devices including methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29D) that reduces friction loss by rolling contact, and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact, and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion unit (29F) that reduces friction loss, and various rotary output drive devices including methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high-temperature mercury (1d) Combined engine combustion part (29G) that reduces friction loss, and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Rolling contact between high temperature mercury (1d) Combined engine combustion part (29H) that reduces friction loss, and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various rotary output drive devices including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d), including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Various rotary output drive equipment that includes a combined engine combustion section (29B) that increases the rotational output by the gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and includes various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including a merging engine combustion section (29C) that increases the rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and includes various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Various rotary output drive equipment that includes a combined engine combustion section (29D) that increases the rotational output by the gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and includes various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Various rotary output drive devices including a mercury pump (1E), a mercury injection pump (6Z), and a combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d), including various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including a merging engine combustion section (29F) that increases the rotational output by gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d), and includes various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including a merging engine combustion section (29G) that increases the rotational output by the gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and includes various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Various rotary output drive equipment including a merging engine combustion section (29H) that increases the rotational output by the gravity of the mercury pump (1E) mercury injection pump (6Z) and high-temperature mercury (1d) and includes various methane recovery cooling using cold energy Various energy conservation cycle coalescing engines.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29A) that reduces friction loss by surface tension, and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of high-temperature mercury (1d) and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) Combined engine combustion section (29C) that reduces friction loss by surface tension, and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drive equipment including methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with combined engine combustion section (29F) that reduces friction loss due to surface tension, and various rotary output drive equipment including methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to surface tension of high-temperature mercury (1d), and various rotary output drive equipment including various methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Mercury pump (1E) Mercury injection pump (6Z) and high-temperature mercury (1d) combined engine combustion section (29H) that reduces friction loss due to surface tension, and various rotary output drive equipment including methane recovery cooling using cold energy A variety of energy conservation cycle coalescence engine.   Various energy storage cycle coalescing engines that inject high temperature mercury (1d) from a vertical all blade mercury turbine (8H) all blade combustion section (30A) mercury injection pump (6Z).   Various energy storage cycle coalescing engines that inject high temperature mercury (1d) from a vertical all blade mercury turbine (8H) all blade combustion section (30B) mercury injection pump (6Z).   Various energy storage cycle coalescing engines that inject high temperature mercury (1d) from a vertical all blade mercury turbine (8H) all blade combustion section (30C) mercury injection pump (6Z).   Various energy storage cycle coalescing engines that inject high temperature mercury (1d) from a vertical all blade mercury turbine (8H) all blade combustion section (30D) mercury injection pump (6Z).   Various energy storage cycle coalescing engines that inject high temperature mercury (1d) from a vertical all blade mercury turbine (8H) all blade combustion section (30E) mercury injection pump (6Z).   Various energy storage cycle coalescing engines that inject high temperature mercury (1d) from a vertical all blade mercury turbine (8H) all blade combustion section (30F) mercury injection pump (6Z).   Various energy storage cycle coalescing engines that inject high temperature mercury (1d) from a vertical all blade mercury turbine (8H) all blade combustion section (30G) mercury injection pump (6Z).   Various energy storage cycle coalescing engines that inject high temperature mercury (1d) from a vertical all blade mercury turbine (8H) all blade combustion section (30H) mercury injection pump (6Z).   All energy blade cycle engine mercury turbine (8E) coalescence engine (29A) various energy storage cycle coalescence engine that injects high temperature mercury (1d) from mercury injection pump (6Z).   Various energy storage cycle coalescing engines that inject high-temperature mercury (1d) from a combustion blade (29B) mercury injection pump (6Z).   All energy blade cycle engine mercury turbine (8E) coalescence engine (29C) various energy storage cycle coalescence engine that injects high temperature mercury (1d) from mercury injection pump (6Z).   Various energy storage cycle coalescence engine that injects high-temperature mercury (1d) from a combustion blade (29D) mercury injection pump (6Z).   All energy blade cycle engine mercury turbine (8E) coalescence engine (29E) various energy storage cycle coalescence engine that injects high temperature mercury (1d) from mercury injection pump (6Z).   Various energy storage cycle coalescence engine that injects high-temperature mercury (1d) from a combustion blade (29F) mercury injection pump (6Z).   Various energy storage cycle coalescence engine that injects high-temperature mercury (1d) from a combustion blade (29G) mercury injection pump (6Z).   Various energy storage cycle coalescence engine that injects high-temperature mercury (1d) from a combustion blade (29H) mercury injection pump (6Z).   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is provided in an annular shape on the upper part of the nozzle (6) on the circumference of the vertical all blade gas turbine (8A) all blade combusting section (30A).   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is annularly provided on the upper part of the nozzle (6) on the circumference of the vertical all blade gas turbine (8A) all blade combusting section (30B).   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is provided in an annular shape on the top of the nozzle (6) on the circumference of the vertical all blade gas turbine (8A) all blade combustion section (30C).   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference of the vertical blade dynamic turbine (8A), full blade combustion section (30D) circumference.   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference of the vertical all blade gas turbine (8A) all blade combusting section (30E) circumference.   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference of the vertical all blade gas turbine (8A) all blade combustion section (30F) circumference.   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is provided in an annular shape on the upper part of the nozzle (6) on the circumference of the vertical all blade gas turbine (8A) all blade combusting section (30G).   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is annularly provided on the upper part of the nozzle (6) on the circumference of the vertical all blade gas turbine (8A) all blade combustion section (30H).   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29D) of the all-rotor impeller gas turbine (8a).   Various energy storage cycle coalescing engines in which a combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion section (29X) of the all-rotor impeller gas turbine (8a).   Combined with various energy conservation cycles to expand high-temperature mercury (1d) in the circumferential direction by the injection mercury injection nozzle (6b) from the vertical all blade mercury turbine (8H) all blade combustion part (30A) mercury injection pump (6Z) organ.   Combined with various energy conservation cycles to expand high-temperature mercury (1d) in a circumferential direction by a jet mercury injection nozzle (6b) from a vertical all blade mercury turbine (8H) full blade combustion section (30B) mercury injection pump (6Z) organ.   Combined with various energy storage cycles to expand high-temperature mercury (1d) in the circumferential direction by the injection mercury injection nozzle (6b) from the vertical all blade mercury turbine (8H) all blade combustion part (30C) mercury injection pump (6Z) organ.   Combined with various energy conservation cycles to expand high-temperature mercury (1d) in the circumferential direction from the vertical type moving blade mercury turbine (8H) all blade combustion section (30D) mercury injection pump (6Z) with the injection mercury injection nozzle (6b) organ.   Combined with various energy conservation cycles to expand high-temperature mercury (1d) in a circumferential direction by a mercury injection nozzle (6b) from a vertical-type all blade mercury turbine (8H) all blade combustion part (30E) mercury injection pump (6Z) organ.   Combined with various energy storage cycles to expand the high-temperature mercury (1d) in the circumferential direction by the injection mercury injection nozzle (6b) from the vertical type all-blade mercury turbine (8H) all blade combustion part (30F) mercury injection pump (6Z) organ.   Combined with various energy conservation cycles to expand the high-temperature mercury (1d) in the circumferential direction with the injection mercury injection nozzle (6b) from the vertical blade dynamic turbine (8H) all blade combustion part (30G) mercury injection pump (6Z) organ.   Combined with various energy conservation cycles to expand high-temperature mercury (1d) in a circumferential direction by a mercury injection nozzle (6b) from a vertical all blade mercury turbine (8H) all blade combustion part (30H) mercury injection pump (6Z) organ.   Various energy storage cycle coalescing engine that expands the high-temperature mercury (1d) in the axial direction by an injection mercury injection nozzle (6b) from a combustion blade (29A) mercury injection pump (6Z).   Various energy storage cycle coalescing engine that expands the high-temperature mercury (1d) in the axial direction by the injection mercury injection nozzle (6b) from the combustion blade (29B) mercury injection pump (6Z).   Various energy conservation cycle coalescing engine that expands the high-temperature mercury (1d) in the axial direction by the injection mercury injection nozzle (6b) from the combustion blade (29C) mercury injection pump (6Z).   Various energy storage cycle coalescing engine that expands the high-temperature mercury (1d) in the axial direction by the injection mercury injection nozzle (6b) from the combustion blade (29D) mercury injection pump (6Z).   Various energy storage cycle coalescing engine that expands the high-temperature mercury (1d) in the axial direction by an injection mercury injection nozzle (6b) from a combustion blade (29E) mercury injection pump (6Z).   Various energy conservation cycle coalescing engine that expands the high-temperature mercury (1d) in the axial direction by the injection mercury injection nozzle (6b) from the combustion blade (29F) mercury injection pump (6Z).   Various energy storage cycle coalescing engine that expands the high-temperature mercury (1d) in the axial direction by the injection mercury injection nozzle (6b) from the combustion blade (29G) mercury injection pump (6Z).   Various energy storage cycle coalescing engine that expands the high-temperature mercury (1d) in the axial direction by the injection mercury injection nozzle (6b) from the combustion blade (29H) mercury injection pump (6Z).   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) Various energy conservation cycle coalescing organizations in contact with.   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) Various energy conservation cycle coalescing organizations in contact with.   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Various energy conservation cycle coalescing organizations in contact with.   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Various energy conservation cycle coalescing organizations in contact with.   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) Various energy conservation cycle coalescing organizations in contact with.   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) Various energy conservation cycle coalescing organizations in contact with.   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Various energy conservation cycle coalescing organizations in contact with.   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Various energy conservation cycle coalescing organizations in contact with.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange Various energy conservation cycle coalescing engines in communication with the vessel (2Z).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29X), and the reduced diameter compression chamber mercury heat exchange. Various energy conservation cycle coalescing engines in communication with the vessel (2Z).   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30A) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy conservation cycle coalescence engine that injects into mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) Full moving blade combustion section (30B) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy conservation cycle coalescence engine that injects into mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30C) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy conservation cycle coalescence engine that injects into mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30D) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy conservation cycle coalescence engine that injects into mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30E) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy conservation cycle coalescence engine that injects into mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) Full moving blade combustion section (30F) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy conservation cycle coalescence engine that injects into mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30G) High temperature mercury (1d) is injected from mercury injection pump (6Z), and expanded in the circumferential direction by mercury injection nozzle (6b). Various energy conservation cycle coalescence engine that injects into mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30H) High temperature mercury (1d) is injected from a mercury injection pump (6Z), and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy conservation cycle coalescence engine that injects into mercury turbine (8H).   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29A) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy conservation cycle coalescing engines to be injected into.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29B) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy conservation cycle coalescing engines to be injected into.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29C) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy conservation cycle coalescing engines to be injected into.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29D) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy conservation cycle coalescing engines to be injected into.   All blade impeller mercury turbine (8E) Combined engine combustion section (29E) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy conservation cycle coalescing engines to be injected into.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29F) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy conservation cycle coalescing engines to be injected into.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29G) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and is expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy conservation cycle coalescing engines to be injected into.   All blade impeller mercury turbine (8E) Combined engine combustion part (29H) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy conservation cycle coalescing engines to be injected into.   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that supply the combustion gas 49 to the combustion gas reservoir (95a).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange Various energy storage cycle coalescing engines for supplying the combustion gas 49 to the combustion gas reservoir (95a).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29X), and the reduced diameter compression chamber mercury heat exchange. Various energy storage cycle coalescing engines for supplying the combustion gas 49 to the combustion gas reservoir (95a).   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30A) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection into a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) Full moving blade combustion section (30B) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection into a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30C) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection into a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30D) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection into a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30E) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection into a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) Full moving blade combustion section (30F) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection into a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30G) High temperature mercury (1d) is injected from mercury injection pump (6Z), and expanded in the circumferential direction by mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection into a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30H) High temperature mercury (1d) is injected from a mercury injection pump (6Z), and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection into a mercury turbine (8H).   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29A) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29B) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29C) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection.   All blade impeller mercury turbine (8E) Combined engine combustion section (29D) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection.   All blade impeller mercury turbine (8E) Combined engine combustion section (29E) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29F) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29G) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and is expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection.   All blade impeller mercury turbine (8E) Combined engine combustion part (29H) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output by high-pressure high-temperature injection.   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) And various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange. Various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29X), and the reduced diameter compression chamber mercury heat exchange. Various energy storage cycle coalescing engines that operate the combustion gas control valve (24) to supply the combustion gas 49 to the combustion gas reservoir (95a).   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30A) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure, high-temperature, vacuum-direction injection, and vaporization explosive force in a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) Full moving blade combustion section (30B) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure, high-temperature, vacuum-direction injection, and vaporization explosive force in a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30C) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure, high-temperature, vacuum-direction injection, and vaporization explosive force in a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30D) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure, high-temperature, vacuum-direction injection, and vaporization explosive force in a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30E) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure, high-temperature, vacuum-direction injection, and vaporization explosive force in a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) Full moving blade combustion section (30F) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure, high-temperature, vacuum-direction injection, and vaporization explosive force in a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30G) High temperature mercury (1d) is injected from mercury injection pump (6Z), and expanded in the circumferential direction by mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure, high-temperature, vacuum-direction injection, and vaporization explosive force in a mercury turbine (8H).   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30H) High temperature mercury (1d) is injected from a mercury injection pump (6Z), and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase rotational output by high-pressure, high-temperature, vacuum-direction injection, and vaporization explosive force in a mercury turbine (8H).   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29A) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output with high-pressure, high-temperature, vacuum-direction injection and vaporization explosive force.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29B) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output with high-pressure, high-temperature, vacuum-direction injection and vaporization explosive force.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29C) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output with high-pressure, high-temperature, vacuum-direction injection and vaporization explosive force.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29D) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output with high-pressure, high-temperature, vacuum-direction injection and vaporization explosive force.   All blade impeller mercury turbine (8E) Combined engine combustion section (29E) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output with high-pressure, high-temperature, vacuum-direction injection and vaporization explosive force.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29F) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output with high-pressure, high-temperature, vacuum-direction injection and vaporization explosive force.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29G) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and is expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output with high-pressure, high-temperature, vacuum-direction injection and vaporization explosive force.   All blade impeller mercury turbine (8E) Combined engine combustion part (29H) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and expanded in the axial direction by the mercury injection nozzle (6b). ) Various energy storage cycle coalescing engines that increase rotational output with high-pressure, high-temperature, vacuum-direction injection and vaporization explosive force.   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting open combustion gas 49.   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting open combustion gas 49.   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting open combustion gas 49.   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting open combustion gas 49.   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting open combustion gas 49.   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting open combustion gas 49.   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting open combustion gas 49.   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting open combustion gas 49.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of all-blade propeller gas turbine (8a) coalescence engine combustion section (29A), and reduced diameter compression chamber mercury heat exchange. The engine (2Z) and the communication combustion gas 49 are supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting the open combustion gas 49.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange. The engine (2Z) and the communication combustion gas 49 are supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) Various energy storage cycle coalescence engines for injecting the open combustion gas 49.   All blade impeller gas turbine (8H) All blade combustor (30A) High-temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). The engine (8H) is a high-pressure, high-temperature, vacuum direction injection. The engine is combined with various energy conservation cycles to increase the rotational output by the vaporization explosive force and to bring the exhaust saturation temperature to around 230 degrees.   All blade impeller gas turbine (8H) All blade combustor (30B) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the circumferential direction by the mercury injection nozzle (6b). The engine (8H) is a high-pressure, high-temperature, vacuum direction injection. The engine is combined with various energy conservation cycles to increase the rotational output by the vaporization explosive force and to bring the exhaust saturation temperature to around 230 degrees.   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30C) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase the rotational output by high-pressure high-temperature vacuum direction injection vaporization explosive force to the mercury turbine (8H) and make the exhaust saturation temperature around 230 degrees.   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30D) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase the rotational output by high-pressure high-temperature vacuum direction injection vaporization explosive force to the mercury turbine (8H) and make the exhaust saturation temperature around 230 degrees.   Vertical type moving blade mercury turbine (8H) All moving blade combustion part (30E) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase the rotational output by high-pressure high-temperature vacuum direction injection vaporization explosive force to the mercury turbine (8H) and make the exhaust saturation temperature around 230 degrees.   Vertical type moving blade mercury turbine (8H) Full moving blade combustion section (30F) High temperature mercury (1d) is injected from a mercury injection pump (6Z) and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase the rotational output by high-pressure high-temperature vacuum direction injection vaporization explosive force to the mercury turbine (8H) and make the exhaust saturation temperature around 230 degrees.   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30G) High temperature mercury (1d) is injected from mercury injection pump (6Z), and expanded in the circumferential direction by mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase the rotational output by high-pressure high-temperature vacuum direction injection vaporization explosive force to the mercury turbine (8H) and make the exhaust saturation temperature around 230 degrees.   Vertical type moving blade mercury turbine (8H) All moving blade combustion section (30H) High temperature mercury (1d) is injected from a mercury injection pump (6Z), and expanded in the circumferential direction by a mercury injection nozzle (6b). Various energy storage cycle coalescing engines that increase the rotational output by high-pressure high-temperature vacuum direction injection vaporization explosive force to the mercury turbine (8H) and make the exhaust saturation temperature around 230 degrees.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29A) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and expanded in the axial direction by the mercury injection nozzle (6b). ) High-pressure high-temperature vacuum direction injection Vaporization explosive force Increases the rotational output and combines various energy storage cycle engines with exhaust saturation temperature around 230 degrees.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29B) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) High-pressure high-temperature vacuum direction injection Vaporization explosive force Increases the rotational output and combines various energy storage cycle engines with exhaust saturation temperature around 230 degrees.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29C) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) High-pressure high-temperature vacuum direction injection Vaporization explosive force Increases the rotational output and combines various energy storage cycle engines with exhaust saturation temperature around 230 degrees.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29D) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) High-pressure high-temperature vacuum direction injection Vaporization explosive force Increases the rotational output and combines various energy storage cycle engines with exhaust saturation temperature around 230 degrees.   All blade impeller mercury turbine (8E) Combined engine combustion section (29E) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) High-pressure high-temperature vacuum direction injection Vaporization explosive force Increases the rotational output and combines various energy storage cycle engines with exhaust saturation temperature around 230 degrees.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29F) High-temperature mercury (1d) is injected from the mercury injection pump (6Z) and expanded in the axial direction by the mercury injection nozzle (6b). ) High-pressure high-temperature vacuum direction injection Vaporization explosive force Increases the rotational output and combines various energy storage cycle engines with exhaust saturation temperature around 230 degrees.   All-wheel impeller mercury turbine (8E) Combined engine combustion section (29G) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and is expanded in the axial direction by the mercury injection nozzle (6b). ) High-pressure high-temperature vacuum direction injection Vaporization explosive force Increases the rotational output and combines various energy storage cycle engines with exhaust saturation temperature around 230 degrees.   All blade impeller mercury turbine (8E) Combined engine combustion part (29H) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and expanded in the axial direction by the mercury injection nozzle (6b). ) High-pressure high-temperature vacuum direction injection Vaporization explosive force Increases the rotational output and combines various energy storage cycle engines with exhaust saturation temperature around 230 degrees.   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle combined engines that inject high pressure low temperature combustion gas 49.   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle combined engines that inject high pressure low temperature combustion gas 49.   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle combined engines that inject high pressure low temperature combustion gas 49.   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle combined engines that inject high pressure low temperature combustion gas 49.   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle combined engines that inject high pressure low temperature combustion gas 49.   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle combined engines that inject high pressure low temperature combustion gas 49.   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle combined engines that inject high pressure low temperature combustion gas 49.   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle combined engines that inject high pressure low temperature combustion gas 49.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange. The engine (2Z) and the communication combustion gas 49 are supplied to the combustion gas reservoir (95a).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29X), and the reduced diameter compression chamber mercury heat exchange. The engine (2Z) and the communication combustion gas 49 are supplied to the combustion gas reservoir (95a).   Vertical all-blade mercury turbine (8H) All-blade combustion section (30A) High-temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all-blade turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air collector (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion part (30B) High temperature mercury (1d) is injected from mercury injection pump (6Z), vertical all blade mercury turbine (8H) rotational output increases exhaust saturation temperature Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air collector (2B) at around 230 degrees.   High-temperature mercury (1d) is injected from vertical all blade mercury turbine (8H) all blade combustion section (30C) mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air collector (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion section (30D) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air collector (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion part (30E) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air collector (2B) at around 230 degrees.   High-temperature mercury (1d) is injected from vertical all blade mercury turbine (8H) all blade combustion section (30F) mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output increases exhaust saturation temperature Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air collector (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion section (30G) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotation output is increased. Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air collector (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion section (30H) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output increases exhaust saturation temperature Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air collector (2B) at around 230 degrees.   All-wheel impeller mercury turbine (8E) coalescence engine combustion section (29A) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) increases rotational output, and exhaust saturation temperature is around 230 degrees Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) coalescence engine combustion part (29B) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) rotational output is increased exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) united engine combustion section (29C) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) rotational output is increased exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) coalescence engine combustion part (29D) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and all-rotor impeller mercury turbine (8E) rotation output is increased. Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air recovery unit (2B).   All blade impeller mercury turbine (8E) coalescence engine combustion section (29E) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and all blade impeller mercury turbine (8E) rotational output increases exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) coalescence engine combustion section (29F) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) increases the rotational output exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) united engine combustion section (29G) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) rotational output is increased, exhaust saturation temperature is 230 degrees Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air recovery unit (2B) before and after.   All-wheel impeller mercury turbine (8E) united engine combustion section (29H) High-temperature mercury (1d) is injected from mercury injection pump (6Z), and all-rotor impeller mercury turbine (8E) rotational output increases exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that recover exhaust heat from the vaporized hot air recovery unit (2B).   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange Combining engine (2Z) and supplying combustion gas 49 to combustion gas reservoir (95a) Combustion gas control valve (24) Opening high-pressure and low-temperature combustion gas 49 is generated by rotating various energy storage cycles.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29X), and the reduced diameter compression chamber mercury heat exchange. Combining engine (2Z) and supplying combustion gas 49 to combustion gas reservoir (95a) Combustion gas control valve (24) Opening high-pressure and low-temperature combustion gas 49 is generated by rotating various energy storage cycles.   Vertical all-blade mercury turbine (8H) All-blade combustion section (30A) High-temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all-blade turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that recover the exhaust heat amount by the intake air (28a) of the vaporized hot air recovery device (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion part (30B) High temperature mercury (1d) is injected from mercury injection pump (6Z), vertical all blade mercury turbine (8H) rotational output increases exhaust saturation temperature Various energy storage cycle coalescing engines that recover the exhaust heat amount by the intake air (28a) of the vaporized hot air recovery device (2B) at around 230 degrees.   High-temperature mercury (1d) is injected from vertical all blade mercury turbine (8H) all blade combustion section (30C) mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that recover the exhaust heat amount by the intake air (28a) of the vaporized hot air recovery device (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion section (30D) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that recover the exhaust heat amount by the intake air (28a) of the vaporized hot air recovery device (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion part (30E) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that recover the exhaust heat amount by the intake air (28a) of the vaporized hot air recovery device (2B) at around 230 degrees.   High-temperature mercury (1d) is injected from vertical all blade mercury turbine (8H) all blade combustion section (30F) mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output increases exhaust saturation temperature Various energy storage cycle coalescing engines that recover the exhaust heat amount by the intake air (28a) of the vaporized hot air recovery device (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion section (30G) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotation output is increased. Various energy storage cycle coalescing engines that recover the exhaust heat amount by the intake air (28a) of the vaporized hot air recovery device (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion section (30H) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output increases exhaust saturation temperature Various energy storage cycle coalescing engines that recover the exhaust heat amount by the intake air (28a) of the vaporized hot air recovery device (2B) at around 230 degrees.   All-wheel impeller mercury turbine (8E) coalescence engine combustion section (29A) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) increases rotational output, and exhaust saturation temperature is around 230 degrees Various energy storage cycle combined engines that recover the amount of exhaust heat by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) coalescence engine combustion part (29B) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) rotational output is increased exhaust saturation temperature around 230 degrees Various energy storage cycle combined engines that recover the amount of exhaust heat by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) united engine combustion section (29C) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) rotational output is increased exhaust saturation temperature around 230 degrees Various energy storage cycle combined engines that recover the amount of exhaust heat by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) coalescence engine combustion part (29D) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and all-rotor impeller mercury turbine (8E) rotation output is increased. Various energy storage cycle combined engines that recover the amount of exhaust heat by the intake air (28a) of the vaporized hot air recovery unit (2B).   All blade impeller mercury turbine (8E) coalescence engine combustion section (29E) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and all blade impeller mercury turbine (8E) rotational output increases exhaust saturation temperature around 230 degrees Various energy storage cycle combined engines that recover the amount of exhaust heat by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) coalescence engine combustion section (29F) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) increases the rotational output exhaust saturation temperature around 230 degrees Various energy storage cycle combined engines that recover the amount of exhaust heat by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) united engine combustion section (29G) High-temperature mercury (1d) is injected from mercury injection pump (6Z), and all-rotor impeller mercury turbine (8E) rotational output is increased. Various energy storage cycle combined engines that recover the amount of exhaust heat by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) united engine combustion section (29H) High-temperature mercury (1d) is injected from mercury injection pump (6Z), and all-rotor impeller mercury turbine (8E) rotational output increases exhaust saturation temperature around 230 degrees Various energy storage cycle combined engines that recover the amount of exhaust heat by the intake air (28a) of the vaporized hot air recovery unit (2B).   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 is supplied to the combustion gas reservoir (95a). Combustion gas control valve (24) is opened.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange Combustion gas 49 is supplied to the combustion gas reservoir (95a) with the combustor (2Z). Combustion gas control valve (24) is opened.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29X), and the reduced diameter compression chamber mercury heat exchange Combustion gas 49 is supplied to the combustion gas reservoir (95a) with the combustor (2Z). Combustion gas control valve (24) is opened.   Vertical all-blade mercury turbine (8H) All-blade combustion section (30A) High-temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all-blade turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that compress the exhaust heat quantity by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion part (30B) High temperature mercury (1d) is injected from mercury injection pump (6Z), vertical all blade mercury turbine (8H) rotational output increases exhaust saturation temperature Various energy storage cycle coalescing engines that compress the exhaust heat quantity by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) at around 230 degrees.   High-temperature mercury (1d) is injected from vertical all blade mercury turbine (8H) all blade combustion section (30C) mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that compress the exhaust heat quantity by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion section (30D) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that compress the exhaust heat quantity by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion part (30E) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output is increased. Various energy storage cycle coalescing engines that compress the exhaust heat quantity by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) at around 230 degrees.   High-temperature mercury (1d) is injected from vertical all blade mercury turbine (8H) all blade combustion section (30F) mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output increases exhaust saturation temperature Various energy storage cycle coalescing engines that compress the exhaust heat quantity by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion section (30G) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotation output is increased. Various energy storage cycle coalescing engines that compress the exhaust heat quantity by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) at around 230 degrees.   Vertical all blade mercury turbine (8H) All blade combustion section (30H) High temperature mercury (1d) is injected from mercury injection pump (6Z), and vertical all blade mercury turbine (8H) rotational output increases exhaust saturation temperature Various energy storage cycle coalescing engines that compress the exhaust heat quantity by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) at around 230 degrees.   All-wheel impeller mercury turbine (8E) coalescence engine combustion section (29A) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) increases rotational output, and exhaust saturation temperature is around 230 degrees Various energy storage cycle coalescing engines that compress the exhaust heat quantity with the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) coalescence engine combustion part (29B) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) rotational output is increased exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress the exhaust heat quantity with the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) united engine combustion section (29C) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) rotational output is increased exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress the exhaust heat quantity with the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) coalescence engine combustion part (29D) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and all-rotor impeller mercury turbine (8E) rotation output is increased. Various energy storage cycle coalescing engines that compress the exhaust heat quantity with the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B).   All blade impeller mercury turbine (8E) coalescence engine combustion section (29E) High-temperature mercury (1d) is injected from the mercury injection pump (6Z), and all blade impeller mercury turbine (8E) rotational output increases exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress the exhaust heat quantity with the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) coalescence engine combustion section (29F) High-temperature mercury (1d) is injected from mercury injection pump (6Z), all-rotor impeller mercury turbine (8E) increases the rotational output exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress the exhaust heat quantity with the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) united engine combustion section (29G) High-temperature mercury (1d) is injected from mercury injection pump (6Z), and all-rotor impeller mercury turbine (8E) rotational output is increased. Various energy storage cycle coalescing engines that compress the exhaust heat quantity with the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B).   All-wheel impeller mercury turbine (8E) united engine combustion section (29H) High-temperature mercury (1d) is injected from mercury injection pump (6Z), and all-rotor impeller mercury turbine (8E) rotational output increases exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress the exhaust heat quantity with the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B).   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescing engines that supply open combustion gas 49 to combustor (1Y).   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescing engines that supply open combustion gas 49 to combustor (1Y).   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescing engines that supply open combustion gas 49 to combustor (1Y).   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescing engines that supply open combustion gas 49 to combustor (1Y).   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescing engines that supply open combustion gas 49 to combustor (1Y).   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescing engines that supply open combustion gas 49 to combustor (1Y).   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescing engines that supply open combustion gas 49 to combustor (1Y).   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescing engines that supply open combustion gas 49 to combustor (1Y).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange. Combustion gas 49 connected to the combustor (2Z) and supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines supplying the open combustion gas 49 to the combustor (1Y).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29X), and the reduced diameter compression chamber mercury heat exchange. Combustion gas 49 connected to the combustor (2Z) and supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle coalescence engines supplying the open combustion gas 49 to the combustor (1Y).   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the vertical blade mercury turbine (8H) full blade combustion part (30A). Various energy storage cycle coalescing engines that are compressed by the heat and recovered by the heat exchanger (2Z) with reduced diameter compression chamber.   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the vertical blade mercury turbine (8H) all blade combustion part (30B). Various energy storage cycle coalescing engines that are compressed by the heat and recovered by the heat exchanger (2Z) with reduced diameter compression chamber.   Compressed exhaust energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) at an exhaust saturation temperature of about 230 degrees in the vertical blade mercury turbine (8H) all blade combustion part (30C). Various energy storage cycle coalescing engines that are compressed by the heat and recovered by the heat exchanger (2Z) with reduced diameter compression chamber.   Refrigerant heat storage compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30D) exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that are compressed by the heat and recovered by the reduced-diameter compression chamber mercury heat exchanger (2Z).   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) at an exhaust saturation temperature of about 230 degrees in the vertical blade mercury turbine (8H) all blade combustion part (30E). Various energy storage cycle coalescing engines that are compressed by the heat and recovered by the reduced-diameter compression chamber mercury heat exchanger (2Z).   Refrigerant heat storage compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30F) exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that are compressed by the heat and recovered by the reduced-diameter compression chamber mercury heat exchanger (2Z).   Compressor recovering exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with exhaust saturation temperature of around 230 degrees of vertical all blade mercury turbine (8H) all blade combustion part (30G) Various energy storage cycle coalescing engines that are compressed by the heat and recovered by the reduced-diameter compression chamber mercury heat exchanger (2Z).   Refrigerant heat recovery compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30H) exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that are compressed by the heat and recovered by the reduced-diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29A) of the all-wheel impeller mercury turbine (8E). Various energy storage cycle coalescence engines that recover heat with a reduced-diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29B) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescence engines that recover heat with a reduced-diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees in the combustion section (29C) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescence engines that recover heat with a reduced-diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees C of the combustion section (29D) of the all-wheel impeller mercury turbine (8E) combined engine Various energy storage cycle coalescence engines that recover heat with a reduced-diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered air storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the combustion blade (29E) of the all-wheel impeller mercury turbine (8E) combined engine combustion section (29E). Various energy storage cycle coalescence engines that recover heat with a reduced-diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 ° C. of the combustion section (29F) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescence engines that recover heat with a reduced-diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees in the combustion section (29G) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescence engines that recover heat with a reduced-diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29H) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescence engines that recover heat with a reduced-diameter compression chamber mercury heat exchanger (2Z).   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) The combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) The combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) The combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) The combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) The combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) The combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) The combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) The combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange Combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29X), and the reduced diameter compression chamber mercury heat exchange Combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the vertical blade mercury turbine (8H) full blade combustion part (30A). Various energy storage cycle coalescing engines that compress and recover the compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the vertical blade mercury turbine (8H) all blade combustion part (30B). Various energy storage cycle coalescing engines that compress and recover the compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Compressed exhaust energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) at an exhaust saturation temperature of about 230 degrees in the vertical blade mercury turbine (8H) all blade combustion part (30C). Various energy storage cycle coalescing engines that compress and recover the compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Refrigerant heat storage compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30D) exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress and recover the compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) at an exhaust saturation temperature of about 230 degrees in the vertical blade mercury turbine (8H) all blade combustion part (30E). Various energy storage cycle coalescing engines that compress and recover the compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Refrigerant heat storage compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30F) exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress and recover the compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Compressor recovering exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with exhaust saturation temperature of around 230 degrees of vertical all blade mercury turbine (8H) all blade combustion part (30G) Various energy storage cycle coalescing engines that compress and recover the compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Refrigerant heat recovery compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30H) exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress and recover the compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29A) of the all-wheel impeller mercury turbine (8E). Various energy storage cycle coalescing engines that recover compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29B) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescing engines that recover compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees in the combustion section (29C) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescing engines that recover compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees C of the combustion section (29D) of the all-wheel impeller mercury turbine (8E) combined engine Various energy storage cycle coalescing engines that recover compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered air storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the combustion blade (29E) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescing engines that recover compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 ° C. of the combustion section (29F) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescing engines that recover compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees in the combustion section (29G) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescing engines that recover compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29H) of the all-wheel impeller mercury turbine (8E) combined engine. Various energy storage cycle coalescing engines that recover compression heat one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion injection various energy storage cycle combined engine.   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion injection various energy storage cycle combined engine.   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion injection various energy storage cycle combined engine.   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion injection various energy storage cycle combined engine.   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion injection various energy storage cycle combined engine.   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion injection various energy storage cycle combined engine.   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion injection various energy storage cycle combined engine.   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion injection various energy storage cycle combined engine.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange Combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29X), and the reduced diameter compression chamber mercury heat exchange. Combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y).   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the vertical blade mercury turbine (8H) full blade combustion part (30A). Various energy storage cycle coalesced engines that are compressed by the above and are compressed into high pressure air by repeating compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the vertical blade mercury turbine (8H) all blade combustion part (30B). Various energy storage cycle coalesced engines that are compressed by the above and are compressed into high pressure air by repeating compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Compressed exhaust energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) at an exhaust saturation temperature of about 230 degrees in the vertical blade mercury turbine (8H) all blade combustion part (30C). Various energy storage cycle coalesced engines that are compressed by the above and are compressed into high pressure air by repeating compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Refrigerant heat storage compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30D) exhaust saturation temperature around 230 degrees Various energy storage cycle coalesced engines that are compressed by the above and are compressed into high pressure air by repeating compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) at an exhaust saturation temperature of about 230 degrees in the vertical blade mercury turbine (8H) all blade combustion part (30E). Various energy storage cycle coalesced engines that are compressed by the above and are compressed into high-pressure air by repeating compression heat recovery one or more times with a reduced-diameter compression chamber mercury heat exchanger (2Z).   Refrigerant heat storage compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30F) exhaust saturation temperature around 230 degrees Various energy storage cycle coalesced engines that are compressed by the above and are compressed into high pressure air by repeating compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   Compressor recovering exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with exhaust saturation temperature of around 230 degrees of vertical all blade mercury turbine (8H) all blade combustion part (30G) Various energy storage cycle coalesced engines that are compressed by the above and are compressed into high-pressure air by repeating compression heat recovery one or more times with a reduced-diameter compression chamber mercury heat exchanger (2Z).   Refrigerant heat recovery compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30H) exhaust saturation temperature around 230 degrees Various energy storage cycle coalesced engines that are compressed by the above and are compressed into high pressure air by repeating compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29A) of the all-wheel impeller mercury turbine (8E). Then, various energy storage cycle coalescing engines that generate high-pressure air by repeating compression heat recovery one or more times with a reduced-diameter compression chamber mercury heat exchanger (2Z).   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29B) of the all-wheel impeller mercury turbine (8E) combined engine. Then, various energy storage cycle coalescing engines that generate high-pressure air by repeating compression heat recovery one or more times with a reduced-diameter compression chamber mercury heat exchanger (2Z).   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all-blade combustion section (30A) to reduce friction loss to provide various rotary output drive devices Various energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) provide all-blade combustion section (30B) to reduce friction loss to provide various rotary output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion part (30C) that reduces friction loss by water repellent action (3G) to provide various rotary output drive devices Various energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to provide a total blade combustion part (30D) that reduces friction loss to provide various rotary output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to provide all blade combustion part (30E) to reduce friction loss and to make various rotary output drive equipment Various energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) provide all-blade combustion section (30F) to reduce friction loss to provide various rotary output drive devices Various energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) provide all-blade combustion section (30G) to reduce friction loss to provide various rotary output drive devices Various energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all-blade combustion section (30H) that reduces friction loss to provide various rotary output drive devices Various energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss due to mercury surface tension Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade blade combustion section (30B) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30A) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact with mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30A) that increases rotational output by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30B) that increases rotational output by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30C) that increases rotational output by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30D) that increases rotational output by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30E) that increases rotational output by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30G) that increases the rotational output by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30H) that increases rotational output by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact, and various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that reduces friction loss by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, and various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30D) that reduces friction loss by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade drive unit (30E) that reduces friction loss by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30G) that reduces friction loss by rolling contact with various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact, and various rotary output drive equipment Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) which increases rotational output by gravity of high temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss due to surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by high-temperature mercury (1d) surface tension. Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) which reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that reduces friction loss by the surface tension of various rotary output drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion unit (29A) to reduce friction loss Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29B) to reduce friction loss, various rotary output drive equipment Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion engine (29C) that reduces friction loss Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion part (29D) to reduce friction loss and various rotary output drive equipment Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29E) to reduce friction loss, and various rotary output drive equipment Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion unit (29F) that reduces friction loss Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion engine (29G) that reduces friction loss Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29H) to reduce friction loss, various rotary output drive equipment Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury. Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury. Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of mercury Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) to reduce friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) to reduce friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) to reduce friction loss by rolling contact of mercury, and various energy storage as rotary output drive equipment Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various energy storage as various rotary output drive equipment Cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact with various rotary output drive devices, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact with various rotary output drive devices, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by rolling contact of high-temperature mercury (1d), and various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) for increasing rotational output by rolling contact of high-temperature mercury (1d), and various rotational output drive devices, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high-temperature mercury (1d), and various rotational output drive devices, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d), and various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by rolling contact of high-temperature mercury (1d), and various rotational output drive devices, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by rolling contact of high-temperature mercury (1d), and various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) for reducing friction loss by rolling contact of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of high-temperature mercury (1d), various rotary output drive devices, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact, and various rotary output drive equipment, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) for reducing friction loss by rolling contact of high temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of high-temperature mercury (1d), various rotary output drive devices, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d), various rotary output drive devices, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of high-temperature mercury (1d), various rotary output drive devices, Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d) and various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d) to provide various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotary output drive devices Various energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d) and various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d) to provide various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases the rotational output by the gravity of high-temperature mercury (1d) to provide various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d) to provide various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) to provide various rotational output drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) for reducing friction loss due to surface tension of high temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30B) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30C) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30E) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30G) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30H) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30A) to reduce friction loss by surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss due to mercury surface tension Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to mercury surface tension. Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by rolling contact with mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact with various heating equipment using warm heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by rolling contact of high temperature mercury (1d). Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30C) that increases rotational output due to rolling contact with various heating equipment using warm heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by rolling contact with various heating equipment using heating Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by rolling contact with various heating equipment using warm heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various heating equipment using warm heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all blade combustion section (30G) that increases rotational output by rolling contact with various heating equipment using warm heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases the rotational output by rolling contact with various heating equipment using warm heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact, and various heating equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that reduces friction loss by rolling contact and various heating equipment that uses heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, and various heating equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, and various heating equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact, and various heating equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, and various heating equipment that uses heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact and various heating equipment that uses heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact, and various heating equipment that uses heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29A) to reduce friction loss, including various heating equipment using heating Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29B) to reduce friction loss, including various heating equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29C) to reduce friction loss, including various heating equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29D) to reduce friction loss, including various heating equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29E) to reduce friction loss, including various heating equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29F) to reduce friction loss, including various heating equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29G) to reduce friction loss, including various heating equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29H) to reduce friction loss, including various heating equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotations including various heating equipment using heating Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various rotations including various heating equipment using heating Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotations including various heating equipment using heating Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, and various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotations including various heating equipment using heating Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotations including various heating equipment using heating Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotations including various heating equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotations including various heating equipment using heating Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various heating equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a coalesced engine combustion section (29B) that increases the rotational output by rolling contact, and various heating equipment that uses heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various types of heating equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various heating equipment that uses heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact, and various heating equipment that uses heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact, and various types of heating equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a coalesced engine combustion section (29G) that increases rotational output by rolling contact, and various heating equipment that uses heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact, and various types of heating equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion part (29A) that reduces friction loss by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact Various heating equipment devices Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29C) to reduce friction loss by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that reduces friction loss by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion part (29F) that reduces friction loss by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29G) that reduces friction loss by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact Various heating facility equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) which increases rotational output by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss and a moving blade combustion section (30C) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30E) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30G) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss with a moving blade combustion section (30H) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to mercury surface tension Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by rolling contact with mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact with various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotational output by rolling contact with various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact with various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30D) that increases rotational output by rolling contact, and various cooking equipment that uses heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by rolling contact of high temperature mercury (1d). Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases the rotational output by rolling contact with various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact with various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases the rotational output by rolling contact with various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact, and various cooking equipment that uses heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, and various cooking equipment that uses heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact, and various cooking equipment that uses heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, and various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, and various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact Various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, and various cooking equipment that uses heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact Various cooking equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) which increases rotational output by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29A) to reduce friction loss, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29B) to reduce friction loss, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29C) to reduce friction loss, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29D) that reduces friction loss, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Shrink compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29E) to reduce friction loss, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29F) to reduce friction loss, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29G) to reduce friction loss, including various cooking equipment equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29H) to reduce friction loss, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotations including various cooking facilities and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotations including various cooking equipment and equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29B) to increase rotational output by rolling contact Various cooking equipment using warm heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29D) that increases rotational output by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact Various cooking equipment using warm heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29H) that increases rotational output by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29B) that reduces friction loss by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29C) that reduces friction loss by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29F) that reduces friction loss by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) to reduce friction loss by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact Various cooking equipment using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30D) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30E) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30F) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30G) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to mercury surface tension Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to mercury surface tension. Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by rolling contact with mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by rolling contact with mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by rolling contact with mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact with mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by rolling contact with mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30A) that increases rotational output by rolling contact with hot water and various hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact with hot water (V) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases the rotational output by rolling contact with various hot water-use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact with hot water, and various types of hot water use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact with hot water, and various types of hot water equipment using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by rolling contact of high-temperature mercury (1d) and various types of energy Conservation cycle coalescence organization.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact with various hot water-use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases rotational output by rolling contact with various hot water-use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30A), and various hot water use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, and various hot water use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, and various hot water use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, and various hot water use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact and various hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, and various hot water equipment using hot heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, and various hot water use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, and various hot water use hot water equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29A) to reduce friction loss, including various types of hot water equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29B) to reduce friction loss Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29C) to reduce friction loss Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29D) to reduce friction loss Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29E) to reduce friction loss Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29F) to reduce friction loss Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29G) to reduce friction loss Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29H) to reduce friction loss Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotations including various hot water equipment using warm heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury and various rotations including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotations including various hot water facility equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, and various rotations including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury and various rotations including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotations including various hot water facility equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and various rotations including various hot water facility equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, and various rotations including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) to reduce friction loss by rolling contact of mercury, various rotations including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) to reduce friction loss by rolling contact of mercury, various rotations including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) to reduce friction loss by rolling contact of mercury, various rotations including various hot water equipments Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) to reduce friction loss by rolling contact of mercury, various rotations including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, various rotations including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) to reduce friction loss by rolling contact of mercury, various rotations including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water facility equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water equipments Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) to increase rotational output by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output due to rolling contact with various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact Various hot water facility equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact with various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29H) that increases rotational output by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29A) that reduces friction loss by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29B) that reduces friction loss by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29C) that reduces friction loss by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29F) that reduces friction loss by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion part (29G) that reduces friction loss by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29H) that reduces friction loss by rolling contact Various hot water equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output due to the gravity of various hot water-use hot water equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30A) to reduce friction loss by water repellent action (3G), including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30B) to reduce friction loss by water repellent action (3G), including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury jet pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30C) to reduce friction loss, including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30D) to reduce friction loss, including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30E) to reduce friction loss, including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) to reduce friction loss by water repellent action (3G), including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss, including a moving blade combustion section (30G), including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all blade combustion part (30H) to reduce friction loss, including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by mercury surface tension, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by mercury surface tension, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by surface tension of mercury and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by mercury surface tension, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by mercury surface tension, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by mercury surface tension, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by the surface tension of mercury and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by mercury surface tension, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by rolling contact of mercury, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotations including various dishwashers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30A) that increases the rotational output by rolling contact with various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by rolling contact of high temperature mercury (1d) and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact with various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by rolling contact with high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by rolling contact of high-temperature mercury (1d) and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases the rotational output by rolling contact with various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that increases the rotational output by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury jet pump (6Z) and high temperature mercury (1d) rolling blade contact section (30B) that reduces friction loss by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury jet pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury jet pump (6Z) and high temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact Various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29A) to reduce friction loss, including various dishwashers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29B) to reduce friction loss, including various dishwashers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29C) to reduce friction loss, including various dishwashers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion engine (29D) to reduce friction loss and various types including dishwashers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), including various dishwashers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29F) to reduce friction loss, including various dishwashers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion engine (29G) to reduce friction loss, various types including dishwashers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water-repellent action (3G) equipped with coalesced engine combustion section (29H) to reduce friction loss, including various dishwashers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to surface tension of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact with various dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact, and various dishwashers that use heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact with various dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact with various dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact with various dishwashers that use heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact with various types of dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that reduces friction loss by rolling contact, and various dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, and various dishwashers that use heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact. Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29E) that reduces friction loss by rolling contact with various types of dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that reduces friction loss by rolling contact with various dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact with various types of dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that reduces friction loss by rolling contact with various dishwashers using heat Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) and includes various dishwashers that use heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and includes various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and includes various dishwashers that use heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d) and includes various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30A) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30B) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury jet pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30D) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30E) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30F) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30G) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30H) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss due to the surface tension of mercury, including various washing dryers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to the surface tension of mercury, including various washing dryers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss due to the surface tension of mercury, including various washing dryers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, including various washing dryers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, including various washing dryers that use heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, including various washing dryers that use heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss due to the surface tension of mercury, including various washing dryers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to mercury surface tension, including various washing dryers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, including various washing dryers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by rolling contact of mercury, including various washing dryers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, including various washing dryers using heat Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by rolling contact with mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact with various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases the rotation output by rolling contact with hot various washing dryers that use heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30C) to increase rotational output by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases the rotational output by rolling contact with various hot-water washing dryers Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various hot-water washing dryers Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases the rotational output by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases rotational output by rolling contact with various hot-water washing dryers Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) for reducing friction loss by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that reduces friction loss by rolling contact, and various types of washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30D) that reduces friction loss by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) which reduces friction loss by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30G) that reduces friction loss by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact, and various washing dryers using heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) for reducing friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) to reduce friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) to reduce friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29B) to reduce friction loss, including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by water repellent action (3G), including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29D) to reduce friction loss, including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29E) to reduce friction loss, including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by water repellent action (3G), including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by water repellent action (3G), including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29H) to reduce friction loss, including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by the surface tension of mercury and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotations including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various types of laundry dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact, and various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by rolling contact of high-temperature mercury (1d) Various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact Various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29B) that reduces friction loss by rolling contact Various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact Various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29D) that reduces friction loss by rolling contact Various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) to reduce friction loss by rolling contact Various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29F) that reduces friction loss by rolling contact Various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact Various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced combustion unit (29H) that reduces friction loss by rolling contact Various washing dryers using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all blade combustion section (30A) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30B) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30C) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with all blade combustion part (30D) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30E) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30F) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with all blade combustion part (30G) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with all blade combustion section (30H) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that reduces friction loss by mercury surface tension, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30D) that reduces friction loss due to mercury surface tension, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30G) that reduces friction loss due to the surface tension of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by rolling contact of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) to reduce friction loss by rolling contact of mercury, and various rotations including various hot water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30A) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-heated blade combustion section (30B) that increases the rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) and all-heated blade combustion section (30C) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30F) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30G) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact, and various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30D) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30G) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a moving blade combustion section (30A) that increases the rotational output by the gravity of various hot water pipe buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a moving blade combustion section (30B) that increases the rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30C) that increases the rotational output by gravity, and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30D) that increases the rotational output by gravity, and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a moving blade combustion section (30E) that increases the rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30F) that increases the rotational output by gravity, various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30G) that increases the rotational output by gravity, various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a moving blade combustion section (30H) that increases the rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by surface tension of high temperature mercury (1d) and various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) which reduces friction loss by surface tension of high temperature mercury (1d) and various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by surface tension of high temperature mercury (1d) and various hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29A) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29B) to reduce friction loss and various types including hot water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29C) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29D) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29E) that reduces friction loss and various types of hot water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29F) to reduce friction loss and various types including various hot water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29G) to reduce friction loss and various types of hot water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29H) to reduce friction loss, including various hot water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by mercury surface tension, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact, and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a coalesced engine combustion section (29G) that increases rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact, and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact, various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29E) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29F) that reduces friction loss by rolling contact, and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact with various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and includes various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d), including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and includes various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) and includes various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), including various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion combustion section (29H) that reduces friction loss by surface tension of various hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30A) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30B) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30E) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30G) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30H) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss due to surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, including various cooling equipment using cold Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss due to surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by mercury surface tension, and various types of cooling equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, including various cooling equipment using cold Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various types of cooling equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various types of cooling equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various types of cooling equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various types of cooling equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various types of cooling equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that increases rotational output by rolling contact, and various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact with various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact with various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30D) that increases rotational output by rolling contact with various cooling equipment using cold Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact with various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact with various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30H) that increases rotational output by rolling contact with various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, and various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, and various cooling equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29A) to reduce friction loss, including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29B) to reduce friction loss, including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29C) to reduce friction loss, including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29D) to reduce friction loss, including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion section (29E) to reduce friction loss, including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29F) to reduce friction loss, including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29G) to reduce friction loss, including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with coalesced engine combustion section (29H) to reduce friction loss, including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) to reduce friction loss by rolling contact of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotations including various cooling equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by rolling contact with high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that increases rotational output by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29G) that increases rotational output by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact of high temperature mercury (1d) Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of high temperature mercury (1d) Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29F) that reduces friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) to reduce friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30F) to reduce friction loss and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by water repellent action (3G) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various rotary output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various rotational output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that reduces friction loss by the surface tension of mercury and various rotary output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury and various rotary output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury and various rotary output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various rotational output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various rotary output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various rotary output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotational output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury and various rotary output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotational output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various rotational output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotational output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotational output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotational output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotational output drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that increases rotational output by rolling contact, and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases rotational output by rolling contact and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all blade combustion section (30C) to increase rotational output by rolling contact, including various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact with various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by rolling contact of high-temperature mercury (1d), and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases rotational output by rolling contact, and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact with various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that increases rotational output by the gravity of various types, including various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustor (30D) that increases rotational output by gravity of high temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases the rotational output by the gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that increases rotational output by the gravity of various types, including various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that increases rotational output by gravity, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that reduces friction loss due to surface tension and various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that reduces friction loss by surface tension and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that reduces friction loss by surface tension and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that reduces friction loss by surface tension and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30E) that reduces friction loss by surface tension and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that reduces friction loss due to surface tension and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), including various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) with all-blade combustion section (30H) that reduces friction loss by surface tension, and includes various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotational outputs including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotational outputs including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various rotational outputs including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G) and various rotational outputs including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G) and various rotational outputs including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotational outputs including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29G) that reduces friction loss, and various rotational outputs including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29H) that reduces friction loss, and various rotational outputs including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various generators A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various generators A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact, and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) and various rotations including various generators Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by water repellent action (3G) and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G) and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30C) to reduce friction loss by water repellent action (3G) and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G) and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by water repellent action (3G) and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) for all-blade combustion section (30F) to reduce friction loss and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by water repellent action (3G) and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with all blade combustion part (30H) to reduce friction loss and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to surface tension of mercury, and various rotary output drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various rotary output drive equipment including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact of mercury, and various rotary output drive equipment including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various rotary output drive equipment including various motors A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases the rotational output by rolling contact, and various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact and various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact and various motors including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30A) that increases the rotational output by the gravity of various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30B) that increases rotational output by the gravity of various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30C) that increases the rotational output by the gravity of various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30D) that increases the rotational output by the gravity of various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30E) that increases the rotational output by the gravity of various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d) and various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases the rotational output by the gravity of high-temperature mercury (1d) and various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-speed mercury (1d) all-blade combustion section (30H) that increases rotational output by the gravity of various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that reduces friction loss by surface tension and various motors including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by surface tension of high temperature mercury (1d) and various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that reduces friction loss by the surface tension of various types including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various rotational output drives including various motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various rotational output drives including various motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), various rotational output drives including various motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G) and various rotational output drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G), combined engine combustion section (29E) that reduces friction loss, and various rotational output drives including various motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various rotational output drives including various motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G) and various rotational output drives including various motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) and various rotational output drives including various motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various rotary output drive devices including various electric motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotary output drive devices including various motors Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with combined engine combustion section (29A) that increases rotational output by rolling contact, and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases the rotational output by rolling contact, and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact, and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by rolling contact of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by rolling contact of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of high temperature mercury (1d), various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29B) that reduces friction loss by rolling contact, various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29C) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29D) that reduces friction loss by rolling contact, various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that reduces friction loss by rolling contact, and various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29G) that reduces friction loss by rolling contact and various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29H) that reduces friction loss by rolling contact and various rotations including various motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various rotational outputs including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various rotational outputs including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various rotational outputs including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d) and various rotational outputs including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various rotational outputs including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various rotations including various electric motors Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30A) to reduce friction loss, including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by water repellent action (3G), including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30C) to reduce friction loss, including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30D) to reduce friction loss, including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30E) to reduce friction loss, including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30F) to reduce friction loss, including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30G) to reduce friction loss, including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30H) to reduce friction loss, including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by mercury surface tension, various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by mercury surface tension, and various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury and various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by the surface tension of mercury, and various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by mercury surface tension, and various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by mercury surface tension, and various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by mercury surface tension, and various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by rolling contact of mercury, various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact of mercury, various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) to reduce friction loss by rolling contact of mercury, various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) to reduce friction loss by rolling contact of mercury, various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) to reduce friction loss by rolling contact of mercury, various rotations including various hot water piping greenhouses Various energy storage cycle coalescence engine as output drive equipment.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that increases the rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30B) that increases rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30C) to increase rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30D) that increases rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that increases rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30F) that increases the rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30G) that increases rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blades with all-blade combustion section (30H) that increases rotational output by rolling contact Various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water pipes Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30G) to reduce friction loss by rolling contact, and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a moving blade combustion section (30B) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30C) that increases the rotational output by gravity, various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity moving all-blade combustion section (30D) to increase the rotational output by gravity, various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity turbine all-blade combustion section (30E) to increase the rotational output by gravity, various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a moving blade combustion section (30F) that increases the rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity moving all blade combustion unit (30G) to increase the rotational output by gravity, various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity moving all blade combustion section (30H) to increase the rotational output by gravity, various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by surface tension of high temperature mercury (1d) and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by surface tension of high temperature mercury (1d) and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29A) to reduce friction loss Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29B) to reduce friction loss Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), including various hot water piping greenhouses Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29D) to reduce friction loss, including various hot water piping greenhouses Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various types including hot water piping greenhouses Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G) and various hot water pipes including greenhouses Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29G) to reduce friction loss Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various types including hot water piping greenhouses Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by mercury surface tension, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by mercury surface tension, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) to reduce friction loss by mercury surface tension, various rotary outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by mercury surface tension, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29A) that increases the rotational output by rolling contact, various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases the rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases the rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact, and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29E) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29F) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact, and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact with various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d), including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), and includes various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), including various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) and includes various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high-temperature mercury (1d), and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d), and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d), and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water piping greenhouses Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30A) to reduce friction loss, and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30B) to reduce friction loss, and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30C) to reduce friction loss, and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30D) to reduce friction loss, and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30E) to reduce friction loss, and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce the friction loss and all blade combustion section (30G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, including various hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss due to the surface tension of mercury, including various hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, including various hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury, including various hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, including various hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, including various hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, including various hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, including various hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury and various types including hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, and various types including hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various types including hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, and various types including hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by rolling contact of mercury, and various types including hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, and various types including hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by rolling contact of mercury, and various types including hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various types including hot water storage equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30A) to increase rotational output by rolling contact with various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that increases the rotational output by rolling contact with various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30C) to increase rotational output by rolling contact with various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30D) that increases rotational output by rolling contact with various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that increases rotational output by rolling contact with various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30G) that increases the rotational output by rolling contact with various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that increases the rotational output by rolling contact with various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water storage equipment (30B) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) which reduces friction loss by rolling contact, and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) which increases rotational output by gravity of high temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss due to surface tension of high temperature mercury (1d) and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by surface tension of high temperature mercury (1d) and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss due to surface tension of high temperature mercury (1d) and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) to reduce friction loss by surface tension of high temperature mercury (1d) and various hot water storage equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29A) to reduce friction loss, including various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29B) to reduce friction loss, including various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29C) to reduce friction loss, including various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29D) to reduce friction loss, including various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29E) to reduce friction loss, including various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29F) to reduce friction loss, including various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29G) to reduce friction loss, including various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29H) to reduce friction loss, including various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) to reduce friction loss by rolling contact of mercury and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and various rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29B) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29F) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30D) to reduce friction loss, and various hot water piping equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30G) to reduce friction loss, and various hot water piping equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30H) to reduce friction loss, and various hot water piping equipment Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to the surface tension of mercury, including various types of hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury, including various hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss due to mercury surface tension, including various hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss due to mercury surface tension, including various hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss due to mercury surface tension, including various hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss due to mercury surface tension, including various hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss due to mercury surface tension, including various hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by the surface tension of mercury, including various hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by rolling contact of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various types including various hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30A) that increases rotational output by rolling contact with various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact with various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that increases rotational output by rolling contact, and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30D) that increases rotational output by rolling contact with various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30E) that increases rotational output by rolling contact with various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30F) that increases rotational output by rolling contact with various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30G) that increases the rotational output by rolling contact with various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact with various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact with various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by surface tension of high temperature mercury (1d) and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by surface tension of high temperature mercury (1d) and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by surface tension of high temperature mercury (1d) and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by surface tension of high temperature mercury (1d) and various hot water piping equipment Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29A) to reduce friction loss, including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29B) to reduce friction loss, including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29C) to reduce friction loss, including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29D) to reduce friction loss, including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29E) to reduce friction loss, including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29F) to reduce friction loss, including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29G) to reduce friction loss, including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with combined engine combustion section (29H) to reduce friction loss, including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) to reduce friction loss by rolling contact of mercury, various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotations including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29C) that increases rotational output by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29A) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact Various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29G) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high temperature mercury (1d) and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high temperature mercury (1d) and various hot water piping equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water-repellent action (3G) equipped with all blade combustion part (30A) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30B) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30C) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all-blade combustion section (30D) to reduce friction loss, including various chilled water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30E) to reduce friction loss, including various chilled water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all-blade combustion section (30F) to reduce friction loss, including various chilled water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water-repellent action (3G) with all-blade combustion section (30G) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with all-blade combustion section (30H) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that reduces friction loss due to the surface tension of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that reduces friction loss by surface tension of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) to reduce friction loss by rolling contact of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) to reduce friction loss by rolling contact of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) to reduce friction loss by rolling contact of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) to reduce friction loss by rolling contact of mercury, and various rotations including various cold water piping buildings Various energy storage cycle coalescence engine as output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that increases rotational output by rolling contact with various cold and hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blades with all-blade combustion section (30B) that increases rotational output by rolling contact, and various chilled water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30C) that increases rotational output by rolling contact with various cold and hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that increases rotational output by rolling contact with various hot and cold water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30F) that increases rotational output by rolling contact with various hot and cold water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30G) that increases rotational output by rolling contact with various cold and hot water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that increases rotational output by rolling contact with various hot and cold water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot and cold water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with high temperature mercury (1d). Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot and cold water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact with various hot and cold water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30G) that reduces friction loss by rolling contact, and various chilled water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact, and various chilled water piping buildings Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30A) that increases the rotational output by gravity. Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity turbine all-blade combustion section (30B) that increases the rotational output by gravity, various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30C) to increase the rotational output by gravity, various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a moving blade combustion section (30D) that increases the rotational output by the gravity of various hot water pipe buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity moving all-blade combustion section (30E) to increase the rotational output by gravity, various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30F) that increases the rotational output by gravity, and various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity rotor all-blade combustion section (30G) to increase the rotational output, and various cold and hot water pipe buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity moving all-blade combustion section (30H) that increases the rotational output by gravity, various cold and hot water pipe buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29A) that reduces friction loss, and various types including cold water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29B) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29C) to reduce friction loss and various types including cold water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29D) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29E) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29F) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29G) that reduces friction loss, and various types including various cold water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29H) to reduce friction loss, including various cold water piping buildings Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by mercury surface tension, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by mercury surface tension, and various rotary outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by mercury surface tension, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact with mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) to reduce friction loss by rolling contact of mercury, and various rotational outputs including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29A) that increases the rotational output by rolling contact with various cold and hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact with various cold and hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact with various chilled water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact with various cold and hot water pipe buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact with various cold and hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact, and various cold and hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact with various cold and hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29E) that reduces friction loss by rolling contact, and various cold and hot water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29F) that reduces friction loss by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact with various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact, and various chilled water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) and includes various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and includes various chilled water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) combined coal combustion combustion section (29A) that reduces friction loss by surface tension of various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) combined coal combustion combustion section (29E) that reduces friction loss by surface tension of various cold water piping buildings Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss due to surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss and all blade combustion section (30A) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss and all blade combustion parts (30C) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30E) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30F) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce the friction loss and all blade combustion parts (30G) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion section (30H) to reduce friction loss Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss due to mercury surface tension, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, including various refrigeration equipment using cold Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss due to mercury surface tension, and various types of refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss due to surface tension of mercury, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various types including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that increases the rotational output by rolling contact, and various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by rolling contact with high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by rolling contact of high temperature mercury (1d) and various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact with various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30E) that increases rotational output by rolling contact, and various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) which increases rotational output by rolling contact of high temperature mercury (1d) and various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by rolling contact of high temperature mercury (1d) and various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact and various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by rolling contact between high temperature mercury (1d) and various refrigeration equipment using cold heat Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact and various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) which increases rotational output by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30A) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines as various rotational output drive devices including   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29A) to reduce friction loss, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29B) to reduce friction loss, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29C) to reduce friction loss, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29E) to reduce friction loss, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29F) to reduce friction loss, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29G) to reduce friction loss, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29H) to reduce friction loss, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various rotations including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by rolling contact of high-temperature mercury (1d) Various cold-use refrigeration equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29C) that increases rotational output by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that increases rotational output by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various cold-use refrigeration equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various cold-use refrigeration equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by rolling contact of high temperature mercury (1d) Various cold-use refrigeration equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various cold-use refrigeration equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion part (29E) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29G) to reduce friction loss by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various cold-use refrigeration equipment Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases the rotational output by the gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss and all blade combustion section (30A) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) for all-blade combustion section (30B) to reduce friction loss and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss and all blades combustion section (30C) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) for all-blade combustion section (30D) to reduce friction loss and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) for all-blade combustion section (30E) to reduce friction loss and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with all blade combustion part (30F) to reduce friction loss and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss and all blade combustion section (30G) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss and all blade combustion section (30H) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by the surface tension of mercury, and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion section (30H) that reduces friction loss by the surface tension of mercury and various water suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) to reduce friction loss by rolling contact of mercury and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various water suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30D) that reduces friction loss by rolling contact of mercury and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury and various water suction injection including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury and various water suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that increases rotational output by rolling contact, and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases rotational output by rolling contact and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all blade combustion section (30C) to increase rotational output by rolling contact, including various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact with various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by rolling contact of high-temperature mercury (1d), and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases rotational output by rolling contact, and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact with various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that increases rotational output by the gravity of various types, including various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustor (30D) that increases rotational output by gravity of high temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases the rotational output by the gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that increases rotational output by the gravity of various types, including various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that increases rotational output by gravity, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) that reduces friction loss due to surface tension and various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that reduces friction loss by surface tension and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that reduces friction loss by surface tension and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that reduces friction loss by surface tension and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30E) that reduces friction loss by surface tension and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that reduces friction loss due to surface tension and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss due to surface tension of high-temperature mercury (1d), including various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) with all-blade combustion section (30H) that reduces friction loss by surface tension, and includes various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) to reduce friction loss by water repellent action (3G), various water suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) to reduce friction loss by water repellent action (3G), various water suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G) and various water suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G) and various water suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), various water suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29F) to reduce friction loss and various water suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G) and various water suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various water suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss due to the surface tension of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to the surface tension of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss due to the surface tension of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various generators Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact, and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d), and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d) and various water including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), and various water suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) for all-blade combustion section (30B) to reduce friction loss and various water suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with all blade combustion part (30C) to reduce friction loss and various water suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) to reduce friction loss and all blade combustion part (30D), various water suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) for all-blade combustion section (30E) to reduce friction loss and various water suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with all blade combustion part (30F) to reduce friction loss and various water suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) for all-blade combustion section (30G) to reduce friction loss and various water suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) for all-blade combustion section (30H) to reduce friction loss and various water suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss due to surface tension of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion section (30C) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by the surface tension of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion section (30G) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion part (30H) that reduces friction loss by the surface tension of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by rolling contact of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by rolling contact of mercury and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various water suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury and various water suction injection drives including various motors Various energy storage cycle coalescing engines as equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases the rotational output by rolling contact, and various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases the rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30H) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact and various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact and various motors including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d) and various waters including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by the gravity of various waters including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d) and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d) and various waters including various electric motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), and various waters including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by the gravity of high-temperature mercury (1d) and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d) and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by surface tension of high-temperature mercury (1d) and various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that reduces friction loss by surface tension and various motors including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by surface tension of high temperature mercury (1d) and various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss due to surface tension of high-temperature mercury (1d), including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that reduces friction loss by the surface tension of various types including various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) and various motors Various energy storage cycle coalescing engine as water suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G) and various water suction injections including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with a combined engine combustion section (29B) that reduces friction loss and various water suction injections including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), various water suction injection including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G) and various water suction injections including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), various water suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29F) to reduce friction loss and various water suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) with coalescence engine combustion section (29G) to reduce friction loss and various water suction injections including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water repellent action (3G) combined coal combustion combustion section (29H) to reduce friction loss and various water suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by the surface tension of mercury and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by the surface tension of mercury and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss due to the surface tension of mercury and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by rolling contact of mercury and various water suction injection drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury and various water suction injection drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by rolling contact of mercury and various water suction injection drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of mercury and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury and various water suction injection drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by rolling contact of mercury and various water suction injection drive devices including various motors A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various water suction injection drive devices including various electric motors A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29A) that increases the rotational output by rolling contact with various water including various electric motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) combined coal combustion unit (29B) that increases rotational output by rolling contact, and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29C) that increases rotational output by rolling contact and various water including various electric motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) combined coal combustion unit (29D) that increases rotational output by rolling contact and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) which increases rotational output by rolling contact of high temperature mercury (1d) and various water including various electric motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29F) that increases the rotational output by rolling contact with various water including various electric motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) combined coal combustion unit (29G) that increases rotational output by rolling contact, and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29H) that increases rotational output by rolling contact and various water including various electric motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29E) that reduces friction loss by rolling contact and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29F) that reduces friction loss by rolling contact and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) and various water suctions including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d), and various water suctions including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d), and various water suctions including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various water suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d) and various water suctions including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various water suctions including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various water suctions including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various water suctions including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by surface tension of high temperature mercury (1d) and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by surface tension of high-temperature mercury (1d) and various water including various electric motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by surface tension of high temperature mercury (1d) and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by surface tension of high-temperature mercury (1d) and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by surface tension of high temperature mercury (1d) and various water including various electric motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by surface tension of high-temperature mercury (1d) and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29G) that reduces friction loss by surface tension of high-temperature mercury (1d) and various water including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by surface tension of high temperature mercury (1d) and various water including various electric motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) to reduce friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) to reduce friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) to reduce friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and water-repellent action (3G) to reduce friction loss and all blade combustion parts (30G) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by water repellent action (3G) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by the surface tension of mercury. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30C) that reduces friction loss by the surface tension of mercury. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury. Energy conservation cycle coalescence engine.   Reduced-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that reduces friction loss due to mercury surface tension. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by rolling contact of mercury Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30C) that reduces friction loss by rolling contact of mercury. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30D) that reduces friction loss by rolling contact of mercury Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by rolling contact of mercury. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by rolling contact of mercury Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30G) that reduces friction loss by rolling contact of mercury. Energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury Energy conservation cycle coalescence engine.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) rolling blade contact section (30A) that increases rotational output by rolling contact, and various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact with various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact with various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact with various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact with various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) rolling blade contact section (30F) that increases rotational output by rolling contact, and various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) rolling blade contact part (30G) that increases rotational output by rolling contact, and various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that increases rotational output by rolling contact with various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that reduces friction loss by rolling contact, and various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact with various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact, and various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact, and various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact, and various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, and various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact, and various air suction injection drive devices A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d) and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) for reducing friction loss by surface tension of high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by surface tension of high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by surface tension of high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by surface tension of high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) for reducing friction loss by surface tension of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by surface tension of high temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by surface tension of high temperature mercury (1d) and various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by surface tension of high-temperature mercury (1d) A variety of energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) to provide various air suction injection drive devices Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury. Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury. Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury. Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury. Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury. Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined energy combustion unit (29C) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined energy combustion unit (29D) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion combustion section (29B) that increases rotational output by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29C) that increases rotational output by rolling contact with various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29D) that increases the rotational output by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29G) that increases rotational output by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) and a combined engine combustion section (29H) that increases rotational output by rolling contact with various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29A) that reduces friction loss by rolling contact, and various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29C) that reduces friction loss by rolling contact, and various air suction injection drive equipment Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29E) that reduces friction loss by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29F) that reduces friction loss by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced diameter compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced combustion unit (29G) that reduces friction loss by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29H) that reduces friction loss by rolling contact, and various air suction injection drive devices Various energy conservation cycle coalescing engines.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29F) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d), and various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) for reducing friction loss by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29G) that reduces friction loss by the gravity of high-temperature mercury (1d), and various air suction injection drive devices, Various energy conservation cycle coalescence engine.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and includes various heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   Includes a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30G) that reduces friction loss due to the surface tension of mercury, and includes various heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and includes various heating equipment using heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It is equipped with a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and includes various heating equipments using heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a moving blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It is equipped with a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a moving blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It is equipped with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a moving blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and includes various types of heating equipment that uses heat. Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact with various heating equipment using warm heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that increases rotational output by rolling contact, and various heating equipment that uses heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that increases rotational output by rolling contact with various heating equipment using warm heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact, and various heating equipment using heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact with various heating equipment using warm heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various heating equipment using warm heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30G) that increases rotational output by rolling contact, and various heating equipment using heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30H) that increases rotational output due to rolling contact of various heating equipment using heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30A) that reduces friction loss by rolling contact, and various heating equipment using heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30B) that reduces friction loss by rolling contact with various heating equipment using warm heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, and various heating equipment using heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30D) that reduces friction loss by rolling contact with various heating equipment using heating Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, and various heating equipment that uses heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact and various heating equipment that uses heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, and various heating equipment using heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact, and various heating equipment using heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29A) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29B) to reduce friction loss Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29C) to reduce friction loss Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29D) to reduce friction loss, and various types of heating equipment using warm heat Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29E) that reduces friction loss Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29F) that reduces friction loss Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion part (29G) to reduce friction loss Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with coalescence engine combustion section (29H) that reduces friction loss Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29B) that reduces friction loss due to the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss due to the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29F) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29H) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29C) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29E) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various types of heating equipment that use heat Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29H) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various heating equipment using warm heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases the rotational output by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact, and various heating equipment using warm heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact, and various heating equipment using heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact, and various heating equipment using heat Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion part (29A) that reduces friction loss by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact Various heating facilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact Various heating facility equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact Various heating equipment with various heat sources Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion part (29E) that reduces friction loss by rolling contact Various heating equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Compact heat compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29F) that reduces friction loss by rolling contact Various heating equipments Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact Various heating facility equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact Various heating facility equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by water repellent action (3G), including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by water repellent action (3G), including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by water repellent action (3G), including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G), including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by water repellent action (3G), including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blades combustion section (30A) that reduces friction loss by the surface tension of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by mercury surface tension, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by mercury surface tension, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by mercury surface tension, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30H) that reduces friction loss by mercury surface tension, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blades combustion section (30A) that reduces friction loss by rolling contact of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blades combustion section (30F) that reduces friction loss by rolling contact of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, and various air suction including various generators Various energy storage cycle coalescing engines as injection drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases rotational output by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases rotational output by rolling contact, and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that increases rotational output by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases rotational output by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that increases rotational output by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases rotational output by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that increases rotational output by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact and includes various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by the gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that increases rotational output by the gravity of various types, including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustor (30C) that increases rotational output by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that increases rotational output by the gravity of various types, including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) whose rotational output is increased by gravity, and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that increases rotational output by gravity, and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29A) that reduces friction loss by water repellent action (3G), and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29B) that reduces friction loss by water repellent action (3G), and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29C) that reduces friction loss by water repellent action (3G), various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29D) that reduces friction loss by water repellent action (3G), and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29E) that reduces friction loss by water repellent action (3G), and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29G) that reduces friction loss by water repellent action (3G), and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29H) that reduces friction loss by water repellent action (3G), various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and united engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29C) that reduces friction loss by the surface tension of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29D) that reduces friction loss by the surface tension of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29G) that reduces friction loss by the surface tension of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29A) that reduces friction loss by rolling contact of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29B) that reduces friction loss by rolling contact of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29C) that reduces friction loss by rolling contact of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29D) that reduces friction loss by rolling contact of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29E) that reduces friction loss by rolling contact of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29F) that reduces friction loss by rolling contact of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29G) that reduces friction loss by rolling contact of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29H) that reduces friction loss by rolling contact of mercury, and various air suction injections including various generators Various energy storage cycle coalescing engines as driving equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by rolling contact of high-temperature mercury (1d) and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact, and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29F) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact, including various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact and various generators Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and united engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and united engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d), and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and united engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d), and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined air combustion unit (29A) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and united engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and united engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and united engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined air combustion unit (29G) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various generators Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blades combustion section (30A) that reduces friction loss by water repellent action (3G), and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blades combustor (30C) that reduces friction loss by water repellent action (3G) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by water repellent action (3G), and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30H) that reduces friction loss by water repellent action (3G), and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various air suction injections including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and various air suction injections including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various air suction injections including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various air suction injections including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various air suction injections including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various air suction injections including various electric motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various air suction injection including various motors Various energy storage cycle coalescing engines as driving equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact, and various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases rotational output by rolling contact, and various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30E) that increases the rotational output by rolling contact, and various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30G) that increases rotational output by rolling contact, and various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all blade combustion section (30H) that increases rotational output by rolling contact with various motors including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by rolling contact of high-temperature mercury (1d) and various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, including various motors Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that increases rotational output by the gravity of various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), various air suction including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), various air suction including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29C) that reduces friction loss by water repellent action (3G), various air suction including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), various air suction including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), various air suction including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), various air suction including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), various air suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), various air suction including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29A) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29B) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29C) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29D) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29E) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29F) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29G) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29H) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various electric motors Various energy storage cycle coalescing engines as equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29A) that increases rotational output by rolling contact with various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with a combined engine combustion section (29B) that increases rotational output by rolling contact with various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29C) that increases rotational output by rolling contact, and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29D) that increases rotational output by rolling contact, and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29E) that increases rotational output by rolling contact, and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) and combined engine combustion section (29F) that increases rotational output by rolling contact with various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29G) that increases rotational output by rolling contact, and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29H) that increases rotational output by rolling contact, and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29A) that reduces friction loss by rolling contact and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d), combined air combustion unit (29B) that reduces friction loss by rolling contact, various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29C) that reduces friction loss by rolling contact, various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29D) that reduces friction loss by rolling contact and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d), combined air combustion unit (29E) that reduces friction loss by rolling contact, and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d), combined coal combustion section (29F) that reduces friction loss by rolling contact, and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29G) that reduces friction loss by rolling contact, and various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d), combined air combustion unit (29H) that reduces friction loss by rolling contact, various air including various motors Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various air suctions including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various air suctions including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various air suctions including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), and various air suctions including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various air suctions including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), and various air suctions including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), and various air suctions including various electric motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various air suctions including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), various air suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by gravity of high-temperature mercury (1d) and various air suctions including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d), various air suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to gravity of high-temperature mercury (1d), various air suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d), various air suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by gravity of high-temperature mercury (1d), various air suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to gravity of high-temperature mercury (1d), various air suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d), various air suction including various motors Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30F) that reduces friction loss due to the surface tension of mercury and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30G) that reduces friction loss due to the surface tension of mercury and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30H) that reduces friction loss due to the surface tension of mercury and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by rolling contact of mercury and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It is equipped with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion part (30D) that reduces friction loss by rolling contact of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It is equipped with a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury and includes various hot water storage equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30B) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30C) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30F) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30G) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30H) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30H) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various hot and cold water storage equipment with a reduced compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30A) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various hot and cold water storage equipment equipped with a reduced pressure compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and a full blade combustion section (30C) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various hot and cold water storage equipment equipped with a compact compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and a full blade combustion section (30D) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various hot and cold water storage equipment equipped with a reduced pressure compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and a full blade combustion section (30E) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various hot and cold water storage equipment equipped with a reduced pressure compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and a full blade combustion section (30G) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various hot and hot water storage equipment with a reduced compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30H) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30A) to reduce friction loss and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30B) to reduce friction loss and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by gravity of high temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30D) to reduce friction loss and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) to reduce friction loss by gravity of high-temperature mercury (1d) and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30G) to reduce friction loss and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30H) to reduce friction loss and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29A) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29D) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29G) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, including various types of hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and a combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, including various types of hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various types including hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and a combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, and various types of hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, including various types of hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, including various types of hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29A) that reduces friction loss by rolling contact of mercury, various types including various hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29B) that reduces friction loss by rolling contact of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29C) that reduces friction loss by rolling contact of mercury, including various hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29D) that reduces friction loss by rolling contact of mercury, and various types including various hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29E) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29F) that reduces friction loss by rolling contact of mercury, and various types including various hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29G) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various types including various hot water storage equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact with various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29G) that increases rotational output by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29H) that increases rotational output by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light heat compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29E) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29F) that reduces friction loss by rolling contact, and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact and various hot water storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), and various hot water storage equipment Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), and various hot water storage equipment Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d), and various hot water storage equipment Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various hot water storage equipment Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), and various hot water storage equipment Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water repellent action (3G) and all blade combustion part (30B) to reduce friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) to reduce friction loss by water repellent action (3G), including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30D) that reduces friction loss by water repellent action (3G), including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G), including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water repellent action (3G) and all blade combustion part (30F) to reduce friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30G) that reduces friction loss by water repellent action (3G), including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water repellent action (3G) and all blade combustion part (30H) to reduce friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various types of air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various types of air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) that reduces friction loss by the surface tension of mercury and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30D) that reduces friction loss by the surface tension of mercury and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30E) that reduces friction loss by the surface tension of mercury and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by the surface tension of mercury and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by the surface tension of mercury and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various types of air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and various types of air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, and various air including various rocket fuels Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) that increases rotational output by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30B) that increases rotational output by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30C) that increases rotational output by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30D) that increases rotational output by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that increases the rotational output by rolling contact, equipped with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30F) that increases rotational output by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with all-blade combustion section (30G) that increases rotational output by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all-blade combustion section (30H) that increases rotational output by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, equipped with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, equipped with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, equipped with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, equipped with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, equipped with various rocket fuels Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30B) that increases the rotational output, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30C) that increases rotational output, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity rotor all-blade combustion section (30D) that increases rotational output, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30E) that increases rotational output, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30F) that increases rotational output, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30G) that increases the rotational output, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30H) that increases rotational output, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30A) that reduces friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30B) to reduce friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30C) to reduce friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30D) to reduce friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30E) to reduce friction loss by gravity of high-temperature mercury (1d), including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30F) to reduce friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity blade all-blade combustion section (30G) to reduce friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30H) to reduce friction loss, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), and various types including various rocket fuels Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various types including various rocket fuels Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and various types including various rocket fuels Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), and various types including various rocket fuels Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), various types including various rocket fuels Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29A) that reduces friction loss due to mercury surface tension, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29F) that reduces friction loss by the surface tension of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29D) that reduces friction loss by rolling contact of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29E) that reduces friction loss by rolling contact of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29F) that reduces friction loss by rolling contact of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various air suction including various rocket fuels Various energy storage cycle coalescing engines as injection drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalescence engine combustion section (29A) that increases rotational output by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29C) that increases rotational output by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29D) that increases rotational output by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that increases rotational output by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalescence engine combustion section (29H) that increases rotational output by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalition engine combustion section (29B) that reduces friction loss by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalition engine combustion section (29C) that reduces friction loss by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that reduces friction loss by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalescing engine combustion section (29F) that reduces friction loss by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29G) that reduces friction loss by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalition engine combustion section (29H) that reduces friction loss by rolling contact, including various rocket fuels Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30H) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion part (30A) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30D) that reduces friction loss by the surface tension of mercury and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30G) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion part (30H) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by rolling contact of mercury and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30C) that reduces friction loss by rolling contact of mercury and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   Includes refrigeration equipment that uses cold energy and has a reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by rolling contact of mercury. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by rolling contact of mercury and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion section (30H) that reduces friction loss by rolling contact of mercury and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that increases rotational output by rolling contact, and uses various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that increases rotational output by rolling contact, and uses various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that increases rotational output by rolling contact, and uses various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30D) that increases rotational output by rolling contact with various cold storage equipment using cold Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact with various cold storage equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30F) that increases the rotational output by rolling contact, and uses various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion part (30G) that increases rotational output by rolling contact with various cold storage equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30H) that increases rotational output by rolling contact with various cold storage equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30D) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29A) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29D) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29G) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment that uses cold energy Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29B) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment that uses cold energy Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29E) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29G) that reduces friction loss by rolling contact of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29H) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29B) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29E) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29F) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29G) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29H) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) which increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and includes various hot water piping equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury and includes various hot water piping equipment Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and includes various hot water piping equipment Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30D) that reduces friction loss due to the surface tension of mercury and includes various hot water piping equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury and includes various hot water piping equipment Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury and includes various hot water piping equipment Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and includes various hot water piping equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and includes various hot water piping equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and includes various hot water piping equipment Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and includes various hot water piping equipment Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and includes various hot water piping equipment Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and includes various hot water piping equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and includes various hot water piping equipment Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and includes various hot water piping equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and includes various hot water piping equipment Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and includes various hot water piping equipment. Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30B) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30C) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30E) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30F) to increase rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30G) that increases rotational output by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30H) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section that reduces friction loss by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light heat compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30A) that increases rotational output by the gravity of various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and hot compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30B) that increases rotational output by gravity, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and hot compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity turbine all-blade combustion section (30C) to increase the rotational output, various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and hot compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity turbine all-blade combustion section (30E) that increases the rotational output by gravity, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and hot compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity turbine all-blade combustion section (30F) that increases the rotational output by gravity, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and hot compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) gravity blade all-blade combustion section (30G) that increases the rotation output, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) to reduce friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) to reduce friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) gravity blade all combustion blade combustion section (30G) to reduce friction loss and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) gravity blade all-blade combustion section (30H) to reduce friction loss and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29D) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with coalesced engine combustion section (29G) to reduce various frictional hot water piping equipment Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss due to mercury surface tension, and various types including hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various types including various hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, including various hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, including various hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29B) that reduces friction loss by rolling contact of mercury, including various types of hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various types including various hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various types including various hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29E) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various types including hot water piping equipment Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29B) that increases rotational output by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29C) that increases rotational output by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with combined engine combustion section (29F) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with combined engine combustion section (29G) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact with various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29A) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29B) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29C) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29F) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29G) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29H) that reduces friction loss by rolling contact, and various hot water piping equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30B) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30G) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion part (30B) that reduces friction loss by the surface tension of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion part (30D) that reduces friction loss by the surface tension of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30F) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30H) that reduces friction loss by the surface tension of mercury, and various air suction including vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30A) that reduces friction loss by rolling contact of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30C) to reduce friction loss by rolling contact of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, and various air suction including various vertical rise and fall Various energy storage cycle coalescing engines as injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion part (30A) that increases rotational output by rolling contact, and includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases rotational output by rolling contact, and includes various vertical rises and drops Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases rotational output by rolling contact, and includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases rotational output by rolling contact and includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases rotational output by rolling contact, and includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases rotational output by rolling contact, and includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases rotational output by rolling contact and includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases rotational output by rolling contact and includes various vertical rises and drops Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30C) to reduce friction loss by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30G) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29B) that reduces friction loss by water repellent action (3G), and various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29C) that reduces friction loss by water repellent action (3G), and various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29D) that reduces friction loss by water repellent action (3G), and various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29E) that reduces friction loss by water repellent action (3G), and various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), and various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29G) that reduces friction loss by water repellent action (3G), and various types of air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29H) that reduces friction loss by water repellent action (3G), and various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various air suction injections including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss due to the surface tension of mercury Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and united engine combustion section (29H) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various air suction injections including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29C) that reduces friction loss by rolling contact of mercury, and various air suction injections including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by rolling contact with mercury Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various air suction injections including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29F) that reduces friction loss by rolling contact of mercury, and various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various air suction injection including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29H) that reduces friction loss by rolling contact of mercury, and various air suction injections including various vertical rise and fall Various energy storage cycle coalescing engines as driving equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact, and various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29E) that increases rotational output by rolling contact, and various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact, and various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact, and various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that reduces friction loss by rolling contact, and various types including vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29E) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact, including various vertical rise and fall Various energy storage cycle coalescing engine as air suction jet drive equipment.   A variety of air including vertical rise and fall with a combined compression combustion chamber (2Z) mercury injection pump (6Z) and a combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including vertical rise and fall with a combined compression combustion chamber (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression and compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including vertical rise and fall with a combined compression combustion chamber (2Z) mercury injection pump (6Z) and a combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined coal combustion unit (29G) that increases rotational output by gravity, and various types of air including various vertical rises and drops Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including vertical rise and fall with a combined compression combustion chamber (29H) that increases the rotational output by gravity of a compact compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29D) which reduces friction loss by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression and compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), including various supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by water repellent action (3G), including various supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30C) that reduces friction loss by water repellent action (3G), including various supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30D) that reduces friction loss by water repellent action (3G), including various supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water repellent action (3G) and all blade combustion part (30E) to reduce friction loss and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blade combustion section (30F) that reduces friction loss by water repellent action (3G), including various supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by water repellent action (3G), including various supersonic flights Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by water repellent action (3G), including various supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by the surface tension of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by the surface tension of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30C) that reduces friction loss by the surface tension of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion part (30D) that reduces friction loss by the surface tension of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30E) that reduces friction loss by the surface tension of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion part (30G) that reduces friction loss by the surface tension of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion part (30H) that reduces friction loss by the surface tension of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by rolling contact of mercury, and various air suction including supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, and various air suction including supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, and various air suction including supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, and various air suction including various supersonic flight Various energy storage cycle coalescing engines as injection drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases rotational output by rolling contact and includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with full blade combustion part (30B) that increases rotational output by rolling contact, and includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases rotational output by rolling contact and includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with full blade combustion part (30D) that increases rotational output by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with full blade combustion part (30E) that increases rotational output by rolling contact and includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with full blade combustion part (30F) that increases rotational output by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases rotational output by rolling contact and includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases rotational output by rolling contact, and includes various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, including various supersonic flight Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30A) whose rotational output is increased by gravity, including various supersonic flights Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion part (30B) that increases rotational output by gravity of high-temperature mercury (1d), including various supersonic flights Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that increases rotational output by gravity, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d) and various supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) to reduce friction loss by gravity of high-temperature mercury (1d) and various supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29A) that reduces friction loss by water repellent action (3G), and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29B) that reduces friction loss by water repellent action (3G), and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29C) that reduces friction loss by water repellent action (3G), and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29D) that reduces friction loss by water repellent action (3G), and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29E) that reduces friction loss by water repellent action (3G), and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29G) that reduces friction loss by water repellency (3G), and various air including supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29H) that reduces friction loss by water repellent action (3G), and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by mercury surface tension, and various air suction injection including various supersonic flight Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29A) that reduces friction loss by rolling contact of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29C) that reduces friction loss by rolling contact of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29F) that reduces friction loss by rolling contact of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29G) that reduces friction loss by rolling contact of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various air suction injections including various supersonic flights Various energy storage cycle coalescing engines as driving equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with a combined engine combustion section (29H) that increases the rotational output by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that reduces friction loss by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact, and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that reduces friction loss by rolling contact and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that reduces friction loss by rolling contact and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that reduces friction loss by rolling contact and various types including supersonic flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   A variety of air including supersonic flight with a combined compression combustion chamber (2Z) mercury injection pump (6Z) and a combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d) and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalesced engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various air including supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including supersonic flight with a combined compression combustion chamber (2Z) mercury injection pump (6Z) and a combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including various supersonic flights with a combined compression combustion chamber (2Z) mercury injection pump (6Z) and a combined engine combustion section (29F) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various air including a supersonic flight with a combined compression combustion chamber (2Z) mercury injection pump (6Z) and a combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including supersonic flight with a combined compression combustion chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and a combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various supersonic flights Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air including supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including supersonic flight with a compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z) and a combined engine combustion section (29C) that reduces friction loss by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various air including a supersonic flight with a combined compression combustion chamber (2D) mercury injection pump (6Z) and a combined engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air including supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion unit (29F) that reduces friction loss by gravity and various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air, including supersonic flight, equipped with a compact compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and a combined engine combustion section (29G) that reduces friction loss by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) combined coal combustion section (29H) that reduces friction loss by gravity, and various air including supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blades combustion section (30A) that reduces friction loss by water repellent action (3G), and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30B) that reduces friction loss by water repellent action (3G), and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) that reduces friction loss by water repellent action (3G), and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30D) that reduces friction loss by water repellent action (3G) and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30E) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blades combustion section (30F) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blades combustion section (30G) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water repellent action (3G) and all blade combustion part (30H) to reduce friction loss and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various air suction injections including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various air suction injections including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and various air suction injections including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various air suction injections including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by mercury surface tension, and various air suction injection including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various air suction injections including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and various air suction injections including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and various air suction injections including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30A) that reduces friction loss by rolling contact of mercury, and various air suction injections including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, and various air suction injection including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, and various air suction injection including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and various air suction jets including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, and various air suction injection including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, and various air suction injection including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various air suction jets including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and various air suction injections including various space flights Various energy storage cycle coalescing engines as driving equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30A) that increases rotational output by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30B) that increases rotational output by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that increases rotational output by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30D) that increases rotational output by rolling contact and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30E) that increases rotational output by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30F) that increases rotational output by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30G) that increases rotational output by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30H) that increases rotational output by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), including various space flights Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, including various space flights Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, and various types including space flight Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, including various space flights Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact and various types including various space flights Various energy storage cycle coalescing engine as air suction jet drive equipment.   A variety of air, including various space flights, with a compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30A) that increases the rotational output by the gravity of high-temperature mercury (1d). Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30D) that increases rotational output by gravity, and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30F) that increases rotational output by gravity, and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that increases rotational output by gravity, and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30H) that increases rotational output by gravity, and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30B) that reduces friction loss by the gravity of various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) all-blade combustion section (30C) that reduces friction loss by gravity, and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air, including various space flights, with a reduced compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30D) that reduces friction loss by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air, including various space flights, with a compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30F) that reduces friction loss by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29C) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by mercury surface tension, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and united engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29B) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29D) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, and various air suction injection drives including various space flights Various energy storage cycle coalescing engines as equipment.   A variety of air, including various space flights, equipped with a combined engine combustion section (29A) that increases rotational output by rolling contact of a reduced compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air, including various space flights, equipped with a combined engine combustion section (29B) that increases the rotational output by rolling contact of the reduced compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various air, including various space flights, equipped with a combined engine combustion section (29C) that increases rotational output by rolling contact of a reduced compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including various space flights, equipped with a combined engine combustion section (29D) that increases rotational output by rolling contact of a reduced compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various air, including various space flights, equipped with a combined engine combustion section (29E) that increases rotational output by rolling contact of a reduced compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air, including various space flights, equipped with a combined engine combustion section (29F) that increases rotational output by rolling contact of a reduced compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including various space flights, equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact of a reduced compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various air, including various space flights, equipped with a combined engine combustion section (29H) that increases rotational output by rolling contact of a reduced compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various air, including various space flights, equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact between a reduced compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various air, including various space flights, equipped with a combined engine combustion section (29B) that reduces friction loss by rolling contact of a compact compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion unit (29C) that reduces friction loss by rolling contact and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion unit (29D) that reduces friction loss by rolling contact and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Various air, including various space flights, equipped with a combined engine combustion section (29E) that reduces friction loss by rolling contact between a compact compression chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) combined coal combustion unit (29F) that reduces friction loss by rolling contact and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced combustion unit (29G) that reduces friction loss by rolling contact and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion unit (29H) that reduces friction loss by rolling contact and various air including various space flights Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by the gravity of high-temperature mercury (1d) and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by the gravity of high-temperature mercury (1d) and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to gravity of high-temperature mercury (1d) and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to gravity of high-temperature mercury (1d), and various air suction including various space flights Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30H) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion part (30A) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30D) that reduces friction loss by the surface tension of mercury and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30G) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion part (30H) that reduces friction loss by the surface tension of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by rolling contact of mercury and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30C) that reduces friction loss by rolling contact of mercury and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   Includes refrigeration equipment that uses cold energy and has a reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by rolling contact of mercury. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by rolling contact of mercury and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion section (30H) that reduces friction loss by rolling contact of mercury and includes various refrigeration equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that increases rotational output by rolling contact, and uses various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that increases rotational output by rolling contact, and uses various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that increases rotational output by rolling contact, and uses various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30D) that increases rotational output by rolling contact with various cold storage equipment using cold Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact with various cold storage equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30F) that increases the rotational output by rolling contact, and uses various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion part (30G) that increases rotational output by rolling contact with various cold storage equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30H) that increases rotational output by rolling contact with various cold storage equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30D) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29A) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29D) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29G) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment that uses cold energy Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29B) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, and various types including refrigeration equipment that uses cold energy Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29E) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29G) that reduces friction loss by rolling contact of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29H) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29A) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29B) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29E) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29F) that reduces friction loss by rolling contact Various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29G) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29H) that reduces friction loss by rolling contact Various cold storage equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) which increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines as various air suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion part (30A) that reduces friction loss by the surface tension of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion section (30H) that reduces friction loss by the surface tension of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a moving blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion part (30B) that reduces friction loss by rolling contact of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by rolling contact of mercury, and includes various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by rolling contact of mercury, and includes various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a moving blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion section (30F) that reduces friction loss by rolling contact of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a whole blade combustion part (30G) that reduces friction loss by rolling contact of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a moving blade combustion section (30H) that reduces friction loss by rolling contact of mercury, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30A) that increases rotational output by rolling contact, and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30B) that increases rotational output by rolling contact with various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact section (30C) that increases rotational output by rolling contact, and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that increases rotational output by rolling contact, and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30F) that increases rotational output by rolling contact, and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all blade combustion section (30G) that increases rotational output by rolling contact with various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that increases rotational output by rolling contact, and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30B) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various types of air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various types of air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various types of air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) to reduce friction loss by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) to reduce friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) to reduce friction loss by gravity of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29B) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29D) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29G) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29H) that reduces friction loss by water repellent action (3G). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29A) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various types of cooling equipment that uses cold energy Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29B) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29C) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29D) that reduces friction loss by rolling contact of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29E) that reduces friction loss by rolling contact of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29G) that reduces friction loss by rolling contact of mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29H) that reduces friction loss by rolling contact with mercury. Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by rolling contact with high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d) Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29A) that reduces friction loss by rolling contact Various cooling equipment using cold Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29B) that reduces friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29C) that reduces friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29D) that reduces friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion unit (29E) that reduces friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Light and cold compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29F) that reduces friction loss by rolling contact Various cooling facility equipment Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29G) that reduces friction loss by rolling contact Various cooling equipment using cold Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29H) that reduces friction loss by rolling contact Various cooling equipment using cold energy Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30A) that reduces friction loss by water repellent action (3G), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by water repellent action (3G), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blade combustion section (30D) that reduces friction loss by water repellent action (3G), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by water repellent action (3G), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by water repellent action (3G), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30G) that reduces friction loss by water repellent action (3G), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by water repellent action (3G), including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30C) that reduces friction loss by the surface tension of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30D) that reduces friction loss by the surface tension of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blade combustion section (30G) that reduces friction loss by mercury surface tension, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by mercury surface tension, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30A) that reduces friction loss by rolling contact of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) to reduce friction loss by rolling contact of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by rolling contact of mercury, and various air suction including various satellite installations Various energy storage cycle coalescing engines as injection drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases rotational output by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases rotational output by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases rotational output by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases rotational output by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases rotational output by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases rotational output by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that increases rotational output by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30E) that reduces friction loss by rolling contact, including various satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, including various artificial satellite installations Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) all-blade combustion section (30G) that increases the rotational output by the gravity of various types, including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion part (30B) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d) and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29A) that reduces friction loss by water repellent action (3G), and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29B) that reduces friction loss by water repellent action (3G), and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29C) that reduces friction loss by water repellent action (3G), and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29D) that reduces friction loss by water repellent action (3G), and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29E) that reduces friction loss by water repellent action (3G), and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29F) that reduces friction loss by water repellent action (3G), and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29G) that reduces friction loss by water repellent action (3G), and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined air combustion unit (29H) that reduces friction loss by water repellent action (3G), and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, and various air suction injections including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, and various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, and various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, and various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, and various air suction injections including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, and various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29C) that reduces friction loss by rolling contact of mercury, and various air suction injections including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29D) that reduces friction loss by rolling contact of mercury, and various air suction injection including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29E) that reduces friction loss by rolling contact of mercury, and various air suction injections including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29F) that reduces friction loss by rolling contact of mercury, and various air suction injections including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined combustion unit (29G) that reduces friction loss by rolling contact of mercury, and various air suction injections including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined air combustion unit (29H) that reduces friction loss by rolling contact of mercury, and various air suction injections including various satellite installations Various energy storage cycle coalescing engines as driving equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that increases rotational output by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that increases rotational output by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that increases rotational output by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that increases rotational output by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that increases rotational output by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29A) that reduces friction loss by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact, including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact, including various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29F) that reduces friction loss by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29G) that reduces friction loss by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) equipped with coalesced engine combustion section (29H) that reduces friction loss by rolling contact, and various satellite installations Various energy storage cycle coalescing engine as air suction jet drive equipment.   Various compression air chambers including heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air chambers including heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air chambers including heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including the installation of various satellites with a combined compression combustion chamber mercury heat exchanger (2Z) mercury injection pump (6Z) and a combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) which increases rotational output by gravity of high-temperature mercury (1d) and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air chambers including heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion unit (29A) that reduces friction loss due to gravity and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion unit (29B) that reduces friction loss by gravity and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air chambers including heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various satellites Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion unit (29F) that reduces friction loss by gravity and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Compact air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) combined air combustion unit (29G) that reduces friction loss by gravity and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Various compression air compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blade combustion section (30A) that reduces friction loss by water repellent action (3G), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by water repellent action (3G), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water-repellent action (3G), all blade combustion section (30C) to reduce friction loss, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water-repellent action (3G) equipped with all-blade combustion section (30D) to reduce friction loss and water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by water repellent action (3G), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with all blade combustion part (30F) to reduce friction loss, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water-repellent action (3G), all blade combustion part (30G) to reduce friction loss, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water-repellent action (3G), all blade combustion section (30H) that reduces friction loss, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30A) that reduces friction loss by mercury surface tension, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30B) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blades combustion section (30D) that reduces friction loss by surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30E) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blades combustion section (30F) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30B) to reduce friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30C) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30D) to reduce friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blades combustion section (30E) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30F) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30G) to reduce friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30A) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases rotational output by rolling contact, water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30C) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases rotational output by rolling contact, water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases rotational output by rolling contact, water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact with water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, water jet (78M) Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, water jet (78M) various Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, water jet (78M) various Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, water jet (78M) various Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, water jet (78M) various Various energy storage cycle coalescence engine as various water suction jet drive equipment including generators.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-pressure mercury (1d) gravity turbine all-blade combustion section (30E) that increases rotational output by gravity, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) to reduce friction loss by gravity of high temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) to reduce friction loss by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30E) to reduce friction loss by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss due to gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) to reduce friction loss by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and water jet (78M) generators equipped with a combined engine combustion section (29A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and water jet (78M) generators equipped with a combined engine combustion section (29B) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z) and water jet (78M) various generators equipped with coalescence engine combustion section (29G) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z) and water jet (78M) various generators equipped with combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29B) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29G) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29H) that reduces friction loss by the surface tension of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29B) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, water jet (78M) various generators Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29A) that increases rotational output by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29B) that increases rotational output by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29C) that increases rotational output by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29D) that increases rotational output by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29E) that increases rotational output by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29F) that increases rotational output by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29G) that increases rotational output by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29H) that increases the rotational output by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced combustion unit (29A) that reduces friction loss by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29B) that reduces friction loss by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29C) that reduces friction loss by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29D) that reduces friction loss by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29E) that reduces friction loss by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29F) that reduces friction loss by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29G) that reduces friction loss by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29H) that reduces friction loss by rolling contact, water jet (78M) various power generation Various energy storage cycle coalescing engines as various water suction / injection drive devices including machinery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), various water jet (78M) generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d) and various water jet (78M) generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to gravity of high-temperature mercury (1d), water jet (78M) various generators Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water jet (78M) various motors equipped with all blade combustion section (30A) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water jet (78M) various motors equipped with all blade combustion section (30B) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water jet (78M) various motors equipped with all blade combustion part (30C) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water-repellent action (3G), all-blade combustion section (30D) to reduce friction loss, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water jet (78M) various motors equipped with all blade combustion section (30E) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury jet pump (6Z), water jet (78M) various motors equipped with all blade combustion section (30F) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and water jet (78M) various motors equipped with all blade combustion section (30G) to reduce friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and water-jet (78M) motors equipped with all-blade combustion section (30H) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, water jet (78M) various electric motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by mercury surface tension, water jet (78M) various motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, water jet (78M) various electric motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by mercury surface tension, water jet (78M) various electric motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, water jet (78M) various electric motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by mercury surface tension, water jet (78M) various motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by the surface tension of mercury, water jet (78M) various electric motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blades combustion section (30H) that reduces friction loss by the surface tension of mercury, water jet (78M) various electric motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by rolling contact of mercury, water jet (78M) various motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by rolling contact of mercury, water jet (78M) various motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, water jet (78M) various motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, water jet (78M) various electric motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, water jet (78M) various motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, water jet (78M) various motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) to reduce friction loss by rolling contact of mercury, water jet (78M) various motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury, water jet (78M) various motors Various energy storage cycle coalescing engines including various water suction / injection drive devices.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30A) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases rotational output by rolling contact, water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30C) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30D) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) with all-blade combustion section (30E) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) with all-blade combustion section (30F) that increases rotational output by rolling contact with water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases rotational output by rolling contact, water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases rotational output by rolling contact, water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30C) that reduces friction loss by rolling contact with water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30D) that reduces friction loss by rolling contact, water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, water jet (78M) various Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, water jet (78M) various Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30G) that reduces friction loss by rolling contact, water jet (78M) various Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, water jet (78M) various Various energy storage cycle coalescing engines as various water suction / injection drive devices including electric motors.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30B) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30E) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30G) which increases rotational output by gravity of high temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all rotor blade combustion section (30H) which increases rotational output by gravity of high temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) to reduce friction loss by gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) to reduce friction loss by gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), water repellent action (3G), combined engine combustion section (29C) to reduce friction loss, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and water jet (78M) motors equipped with a combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalesced engine combustion section (29A) that reduces friction loss by the surface tension of mercury, including various motors for water jet (78M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and includes various water jet (78M) electric motors. Various energy storage cycle coalescing engines as various water suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalescence engine combustion section (29C) that reduces friction loss by the surface tension of mercury, and includes various motors for water jet (78M). Various energy storage cycle coalescing engines as various water suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalescence engine combustion section (29D) that reduces friction loss by the surface tension of mercury, and includes various water jet (78M) motors. Various energy storage cycle coalescing engines as various water suction / injection drive devices.   It includes a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, and includes various water jet (78M) motors. Various energy storage cycle coalescing engines as various water suction / injection drive devices.   It has a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, and includes various water jet (78M) electric motors. Various energy storage cycle coalescing engines as various water suction / injection drive devices.   It has a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalescence engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and includes various water jet (78M) electric motors. Various energy storage cycle coalescing engines as various water suction / injection drive devices.   It includes a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, and includes various water jet (78M) motors. Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29A) that reduces friction loss by rolling contact of mercury, including water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29B) for reducing friction loss by rolling contact of mercury, including water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by rolling contact of mercury, including water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29D) that reduces friction loss by rolling contact of mercury, including water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by rolling contact of mercury, including water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29F) that reduces friction loss by rolling contact of mercury, including water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, water jet (78M) including various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29H) that reduces friction loss by rolling contact of mercury, including water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalition engine combustion section (29A) that increases rotational output by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by rolling contact of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29C) that increases rotational output by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d), various water jet (78M) electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by rolling contact of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29F) that increases rotational output by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Light-compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29G) that increases rotational output by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29H) that increases rotational output by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29A) that reduces friction loss by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced combustion unit (29B) that reduces friction loss by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29C) that reduces friction loss by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29D) that reduces friction loss by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29E) that reduces friction loss by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29F) that reduces friction loss by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29G) that reduces friction loss by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29H) that reduces friction loss by rolling contact, water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d), water jet (78M) various electric motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29D) that reduces friction loss due to gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss due to gravity of high-temperature mercury (1d) and various water jet (78M) motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d) and various water jet (78M) motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss due to gravity of high-temperature mercury (1d) and various water jet (78M) motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss due to gravity of high-temperature mercury (1d), water jet (78M) various motors Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30A) to reduce friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30A) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine injection unit (78K) combined engine injection unit (78K) combined engine combustion unit (29H) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines with various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as air suction jet drive equipment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Combining engine injection part (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion part (30A) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Combining engine injection part (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion part (30B) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Combining engine injection section (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30C) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Combining engine injection part (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion part (30D) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Combining engine injection part (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion part (30E) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Combining engine injection part (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion part (30F) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Combining engine injection section (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30G) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Combining engine injection section (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30H) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various combat Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Combining engine injection part (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion part (30D) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Combining engine injection unit (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion unit (30H) that reduces friction loss by rolling contact of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including combat capability.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss due to surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) to reduce friction loss by the surface tension of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30A) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion part (29A) that reduces friction loss by surface tension of mercury, combined engine injection part (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines with various air suction jet drive devices including air combat capability.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30C) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30E) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30H) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) to reduce friction loss by rolling contact of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cockpits Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cockpits.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including cockpit.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced-compression-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30A) that reduces friction loss by the surface tension of mercury, combined control engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by surface tension of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) to reduce friction loss by the surface tension of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by surface tension of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by surface tension of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30F) that reduces friction loss by surface tension of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined control engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, and various controls of combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced-compression-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30B) that reduces friction loss by rolling contact of mercury, and various controls for combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined control engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury and various controls of combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, and various controls of combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced-compression-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined control engine injection section (78K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, and various controls of combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by rolling contact of mercury and various controls of combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced diameter compression chamber Mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) for reducing friction loss by rolling contact of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber Mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) for reducing friction loss by rolling contact of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber Mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various control chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various control rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including control room.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30A) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) to reduce friction loss by rolling contact of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including space travel.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30C) that reduces friction loss by surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss due to surface tension of mercury, combined engine injection part (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion unit (30G) that reduces friction loss by surface tension of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part (78K) with a reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion part (30H) that reduces friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion part (29C) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion part (29G) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including guest rooms.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30A) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including cargo compartment.   Reduced diameter compression chamber Mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced-compression-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber Mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss due to the surface tension of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber Mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber Mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber Mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber Mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various cargo chambers Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cargo compartments.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including cargo compartment.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engine as various air suction jet drive equipment including vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields anywhere in vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines that have been used as various air suction / injection drive devices including airfields wherever vertical ascent and descent.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30A) that reduces friction loss by surface tension of mercury, combined engine injection part (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30E) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30A) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced-compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroids Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various asteroid landings Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various asteroid landings.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive equipment including asteroid landing.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by the surface tension of mercury. Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30G) that reduces friction loss by the surface tension of mercury, combined engine injection part (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by the surface tension of mercury Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30A) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, and combined engine injection part (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, and combined engine injection part (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30G) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various months Various energy storage cycle coalescing engines as various air suction jet drive equipment including surface landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing start.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various moon surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine injection unit (78K) combined engine injection unit (78K) combined engine combustion unit (29G) to reduce friction loss by the surface tension of mercury Various energy storage cycle coalescing engines that are equipped with various air suction injection drive devices including various lunar landing starts.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion part (29E) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various lunar surfaces Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various lunar landing starts.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including lunar landing start.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30A) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30D) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) which reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30F) that reduces friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30H) to reduce friction loss by water repellent action (3G), combined engine injection part (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all rotor blade combustion section (30A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all rotor blade combustion section (30E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all rotor blade combustion section (30F) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30G) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all-blade combustion section (30H) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30D) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30E) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all rotor blade combustion section (30G) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), all blade combustion section (30H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various solar systems Various energy storage cycle coalescing engines as various air suction jet drive devices including escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Light-compression compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30D) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30F) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that increases the rotational output by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30B), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30D), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part that reduces friction loss by rolling contact (30E), combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling blade contact part (30F) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30G) to reduce friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, combined engine injection part (78K ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30A) that increases rotational output by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30B) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30C) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30E) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30F) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) whose rotational output is increased by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full rotor blade combustion section (30H) that increases rotational output by the gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30B) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all-blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29C) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss by water repellent action (3G), and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by water repellent action (3G), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29A) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) escapes various solar systems Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29B) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) escapes various solar systems Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29C) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) escapes various solar systems Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29D) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various solar system escapes Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by the surface tension of mercury, combined engine injection section (78K) escapes various solar systems Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various solar system escapes Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29G) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) various solar system escapes Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss due to mercury surface tension, combined engine injection section (78K) escapes various solar systems Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion part (29A) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various solar system escape Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29B) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various solar system escape Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion part (29C) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various solar system escape Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion part (29D) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various solar system escape Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29E) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various solar system escape Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29F) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) various solar system escape Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion part (29G) that reduces friction loss by rolling contact of mercury, combined engine injection part (78K) various solar system escape Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), combined engine combustion section (29H) that reduces friction loss by rolling contact of mercury, combined engine injection section (78K) escapes various solar systems Various energy storage cycle coalescing engine as various air suction jet drive equipment including speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) which increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by rolling contact of high-temperature mercury (1d) and coalescence engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29F) that increases rotational output by rolling contact of high temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with a combined engine combustion section (29G) that increases rotational output by rolling contact, and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) which increases rotational output by rolling contact of high temperature mercury (1d) and combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are combined engine combustion section (29A) to reduce friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion unit (29B) that reduces friction loss by rolling contact and united engine injection unit (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29C) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Compact compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine injection section (78K) equipped with coalescence engine combustion section (29D) that reduces friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29E) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss by rolling contact of high-temperature mercury (1d) combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29G) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Lightly compressed compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalescing engine combustion section (29H) that reduces friction loss by rolling contact, combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including various solar system escape speeds.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that increases rotational output by the gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d), and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29C) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss by gravity of high-temperature mercury (1d) and various engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), combined engine injection section (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d) and various combined engine injection sections (78K) Various energy storage cycle coalescing engines as various air suction jet drive devices including solar system escape speed.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29A) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29D) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29G) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and combined engine combustion section (29H) that reduces friction loss by water repellent action (3G) Various energy storage cycle coalescing engines as various rotary output drive devices including.   It has a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalesced engine combustion section (29A) that reduces friction loss by the surface tension of mercury, including various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It has a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29B) that reduces friction loss due to the surface tension of mercury, and includes various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It has a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalescence engine combustion section (29C) that reduces friction loss due to the surface tension of mercury, including various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a combined-combustion engine combustion section (29D) that reduces friction loss due to the surface tension of mercury, including heat-reduced methane hydrate vaporization and recovery. Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalescence engine combustion section (29E) that reduces friction loss by the surface tension of mercury, including various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalescence engine combustion section (29F) that reduces friction loss by the surface tension of mercury, including various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It has a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalescence engine combustion section (29G) that reduces friction loss due to the surface tension of mercury, and includes various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It has a reduced-compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a coalescence engine combustion section (29H) that reduces friction loss due to the surface tension of mercury, including various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a combined-combustion engine combustion section (29A) that reduces friction loss by rolling contact of mercury with a reduced-diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and includes various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a combined-combustion engine combustion section (29B) that reduces friction loss by rolling contact of mercury with a reduced-diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and includes various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a combined-combustion engine combustion section (29C) that reduces friction loss by rolling contact of mercury with a reduced-diameter compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and includes various methane hydrate vaporization and recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a combined-combustion engine combustion section (29D) that reduces friction loss by rolling contact of mercury with a reduced-diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and includes various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a combined-combustion engine combustion section (29E) that reduces friction loss by rolling contact of mercury with a reduced-diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and includes various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a combined-combustion engine combustion section (29F) that reduces friction loss by rolling contact of mercury with a reduced-diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and includes various methane hydrate vaporization and recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a combined-combustion engine combustion section (29G) that reduces friction loss by rolling contact of mercury with a reduced-diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and includes various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   It is equipped with a combined-combustion engine combustion part (29H) that reduces friction loss by rolling contact of mercury with a reduced-diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and includes various methane hydrate vaporization and recovery using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by rolling contact of high-temperature mercury (1d). Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by rolling contact of high-temperature mercury (1d) and various methane hydrate vaporization using heat Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by rolling contact of high-temperature mercury (1d), and various methane hydrate vaporization using heat Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that increases rotational output by rolling contact with various hot methane hydrate vaporization Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases rotational output by rolling contact of high-temperature mercury (1d). Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d). Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that increases rotational output by rolling contact with various hot methane hydrate vaporization Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that increases rotational output by rolling contact with various hot methane hydrate vaporization Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29A) that reduces friction loss by rolling contact Various methane hydrate vaporization using heat Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29B) that reduces friction loss by rolling contact with various hot methane hydrate vaporization Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29C) that reduces friction loss by rolling contact with various hot methane hydrate vaporization Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact with various hot methane hydrate vaporization Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29E) that reduces friction loss by rolling contact with various hot methane hydrate vaporization Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) rolling coalesced engine combustion section (29F) that reduces friction loss by rolling contact Various methane hydrate vaporization using heat Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that reduces friction loss by rolling contact with various hot methane hydrate vaporization Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29H) that reduces friction loss by rolling contact Various methane hydrate vaporization using heat Various energy storage cycle coalescing engine as various rotary output drive equipment including recovery.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Lightweight compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that increases rotational output by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d) and various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29E) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d) and various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss due to gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion part (29H) that reduces friction loss by gravity of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by water repellent action (3G), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with a full blade combustion section (30B) that reduces friction loss and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by water repellent action (3G), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30D) that reduces friction loss by water repellent action (3G), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and all blade combustion part (30E) to reduce friction loss by water repellent action (3G), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with a full blade combustion section (30F) that reduces friction loss and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and water repellent action (3G) equipped with a full blade combustion part (30G) that reduces friction loss and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by water repellent action (3G), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by the surface tension of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30B) that reduces friction loss by the surface tension of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30C) that reduces friction loss by the surface tension of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full rotor blade combustion section (30D) that reduces friction loss by the surface tension of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss due to the surface tension of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30F) that reduces friction loss by the surface tension of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and full blade combustion section (30G) that reduces friction loss by the surface tension of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30H) that reduces friction loss by the surface tension of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30A) that reduces friction loss by rolling contact of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30B) that reduces friction loss by rolling contact of mercury, hot water injection into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30C) that reduces friction loss by rolling contact of mercury, and hot water injection into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30D) to reduce friction loss by rolling contact of mercury, and hot water injection into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30E) that reduces friction loss by rolling contact of mercury to inject hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30F) that reduces friction loss by rolling contact of mercury, and injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion section (30G) that reduces friction loss by rolling contact of mercury to inject hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and all blade combustion part (30H) that reduces friction loss by rolling contact of mercury, injecting hot water into various methane hydrates Various energy storage cycle coalescing engines including various rotational output drive devices.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30A) that increases rotational output by rolling contact, and heats various methane hydrates. Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30B) that increases rotational output by rolling contact, and heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion part (30C) that increases rotational output by rolling contact, and heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30D) that increases rotational output by rolling contact, and heats various methane hydrates. Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) are equipped with all blade combustion section (30E) that increases the rotational output by rolling contact with high-temperature mercury (1d). Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Lightening compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with all blade combustion section (30F) which increases rotational output by rolling contact with hot water to various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with all blade combustion section (30G) that increases rotational output by rolling contact, and heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30H) that increases rotational output by rolling contact, heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30A) that reduces friction loss by rolling contact, heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30B) that reduces friction loss by rolling contact, heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30C) that reduces friction loss by rolling contact, heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30D) that reduces friction loss by rolling contact, heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30E) that reduces friction loss by rolling contact, heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30F) that reduces friction loss by rolling contact, heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact section (30G) that reduces friction loss by rolling contact, heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling blade contact part (30H) that reduces friction loss by rolling contact, heats various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including water injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30A) that increases the rotational output by the gravity of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30B) that increases the rotational output by the gravity of high-temperature mercury (1d), and hot water in various methane hydrates. Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and an all-blade combustion section (30C) that increases the rotational output by the gravity of high-temperature mercury (1d), and hot water in various methane hydrates. Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30D) that increases the rotational output by the gravity of high-temperature mercury (1d), and hot water in various methane hydrates. Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full-blade combustion section (30E) that increases the rotational output by the gravity of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion section (30F) that increases rotational output by gravity of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30G) that increases the rotational output by the gravity of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a full blade combustion section (30H) that increases the rotational output by the gravity of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30A) that reduces friction loss by gravity of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30B) that reduces friction loss by gravity of high-temperature mercury (1d) and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30C) that reduces friction loss by gravity of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30D) that reduces friction loss by gravity of high-temperature mercury (1d) and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion section (30E) that reduces friction loss by gravity of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and full blade combustion section (30F) that reduces friction loss by gravity of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30G) that reduces friction loss by gravity of high-temperature mercury (1d) and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and all blade combustion section (30H) that reduces friction loss by gravity of high-temperature mercury (1d) and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29A) that reduces friction loss by water repellent action (3G), injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29B) that reduces friction loss by water repellent action (3G), injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by water repellent action (3G), injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29D) that reduces friction loss by water repellent action (3G), injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29E) that reduces friction loss by water repellent action (3G), injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by water repellent action (3G), injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29G) that reduces friction loss by water repellent action (3G), and hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29H) that reduces friction loss by water repellent action (3G), injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss by mercury surface tension, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29B) that reduces friction loss by mercury surface tension, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by mercury surface tension, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29D) that reduces friction loss by mercury surface tension, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29E) that reduces friction loss by mercury surface tension, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by mercury surface tension, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by mercury surface tension, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29H) that reduces friction loss by mercury surface tension, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29A) that reduces friction loss by rolling contact of mercury, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29B) that reduces friction loss by rolling contact of mercury, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29C) that reduces friction loss by rolling contact of mercury, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29D) that reduces friction loss by rolling contact of mercury, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29E) that reduces friction loss by rolling contact of mercury, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalescence engine combustion section (29F) that reduces friction loss by rolling contact of mercury, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29G) that reduces friction loss by rolling contact of mercury, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   Reduced diameter compression chamber mercury heat exchanger (2Z), mercury injection pump (6Z), and coalesced engine combustion section (29H) that reduces friction loss by rolling contact of mercury, including hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29A) that increases rotational output by rolling contact of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29B) that increases the rotational output by rolling contact of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29C) that increases rotational output by rolling contact of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29D) that increases the rotational output by rolling contact of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29E) that increases rotational output by rolling contact of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29F) that increases rotational output by rolling contact of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29G) that increases rotational output by rolling contact of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29H) that increases rotational output by rolling contact of high-temperature mercury (1d), and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) are equipped with a combined engine combustion section (29A) that reduces friction loss by rolling contact with hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalesced engine combustion section (29B) that reduces friction loss by rolling contact with hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29C) that reduces friction loss by rolling contact with hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29D) that reduces friction loss by rolling contact with hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high-temperature mercury (1d) rolling coalition engine combustion section (29E) that reduces friction loss by rolling contact with hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalescence engine combustion section (29F) that reduces friction loss by rolling contact with hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29G) that reduces friction loss by rolling contact with hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and high temperature mercury (1d) equipped with coalesced engine combustion section (29H) that reduces friction loss by rolling contact with hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including injection.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29A) that increases the rotational output by the gravity of high-temperature mercury (1d), and injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29B) that increases the rotational output by the gravity of high-temperature mercury (1d), and injects hot water into various methane hydrates. Various energy storage cycle coalescing engines as various rotary output drive devices including.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29C) that increases the rotational output by the gravity of high-temperature mercury (1d), and injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29D) that increases the rotational output by the gravity of high-temperature mercury (1d), and injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29E) that increases the rotational output by the gravity of high-temperature mercury (1d), and injects hot water into various methane hydrates. Various energy storage cycle coalescing engines as various rotary output drive devices including.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29F) that increases the rotational output due to the gravity of high-temperature mercury (1d), and injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   A compact compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29G) that increases the rotational output by the gravity of high-temperature mercury (1d), and injecting hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   A compact heat compression chamber mercury heat exchanger (2Z), a mercury injection pump (6Z), and a combined engine combustion section (29H) that increases the rotational output by the gravity of high-temperature mercury (1d), and injects hot water into various methane hydrates. Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29A) that reduces friction loss due to gravity of high-temperature mercury (1d) and hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices including.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29B) that reduces friction loss due to gravity of high-temperature mercury (1d), and hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29C) that reduces friction loss by gravity of high-temperature mercury (1d) and injects hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Light compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29D) that reduces friction loss due to gravity of high-temperature mercury (1d) and hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and combined engine combustion section (29E) that reduces friction loss by gravity of high-temperature mercury (1d), and injects hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29F) that reduces friction loss due to gravity of high-temperature mercury (1d) and hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29G) that reduces friction loss by gravity of high-temperature mercury (1d), and hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices including.   Reduced compression chamber mercury heat exchanger (2Z) Mercury injection pump (6Z) and coalescence engine combustion section (29H) that reduces friction loss by gravity of high-temperature mercury (1d), and hot water injection into various methane hydrates Various energy storage cycle coalescing engines as various rotary output drive devices including.   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the vertical blade mercury turbine (8H) full blade combustion part (30A). Various energy storage cycle coalescing engines that compress and recover compressed heat in a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to form high-pressure air, and inject and burn fuel in the process of final compressed heat recovery cooling.   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the vertical blade mercury turbine (8H) all blade combustion part (30B). Various energy storage cycle coalescing engines that compress and recover compressed heat in a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to form high-pressure air, and inject and burn fuel in the process of final compressed heat recovery cooling.   Compressed exhaust energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) at an exhaust saturation temperature of about 230 degrees in the vertical blade mercury turbine (8H) all blade combustion part (30C). Various energy storage cycle coalescing engines that compress and recover compressed heat with a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to form high-pressure air and then inject and burn fuel in the process of final compressed heat recovery cooling.   Refrigerant heat storage compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30D) exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress and recover compressed heat with a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to form high-pressure air and then inject and burn fuel in the process of final compressed heat recovery cooling.   Compressed exhaust heat energy is recovered by the intake air (28a) of the vaporized hot air recovery unit (2B) at an exhaust saturation temperature of about 230 degrees in the vertical blade mercury turbine (8H) all blade combustion part (30E). Various energy storage cycle coalescing engines that compress and recover compressed heat with a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to form high-pressure air and then inject and burn fuel in the process of final compressed heat recovery cooling.   Refrigerant heat storage compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30F) exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress and recover compressed heat with a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to form high-pressure air and then inject and burn fuel in the process of final compressed heat recovery cooling.   Compressor recovering exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with exhaust saturation temperature of around 230 degrees of vertical all blade mercury turbine (8H) all blade combustion part (30G) Various energy storage cycle coalescing engines that compress and recover compressed heat in a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to form high-pressure air, and inject and burn fuel in the process of final compressed heat recovery cooling.   Refrigerant heat recovery compressor that recovers exhaust heat by intake air (28a) of vaporized hot air recovery unit (2B) with vertical exhaust blade mercury turbine (8H) full blade combustion part (30H) exhaust saturation temperature around 230 degrees Various energy storage cycle coalescing engines that compress and recover compressed heat with a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to form high-pressure air and then inject and burn fuel in the process of final compressed heat recovery cooling.   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29A) of the all-wheel impeller mercury turbine (8E). Then, compression energy recovery is repeated one or more times in the reduced diameter compression chamber mercury heat exchanger (2Z) to form high-pressure air, and various energy storage cycle coalescence engines that inject and burn fuel in the process of final compression heat recovery cooling.   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29B) of the all-wheel impeller mercury turbine (8E) combined engine. Then, compression energy recovery is repeated at least once in the reduced diameter compression chamber mercury heat exchanger (2Z) to form high-pressure air, and various energy storage cycle coalescence engines that inject and burn fuel in the process of final compression heat recovery cooling.   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees in the combustion section (29C) of the all-wheel impeller mercury turbine (8E) combined engine. Then, compression energy recovery is repeated one or more times in the reduced diameter compression chamber mercury heat exchanger (2Z) to form high-pressure air, and various energy storage cycle coalescence engines that inject and burn fuel in the process of final compression heat recovery cooling.   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees C of the combustion section (29D) of the all-wheel impeller mercury turbine (8E) combined engine Then, compression energy recovery is repeated at least once in the reduced diameter compression chamber mercury heat exchanger (2Z) to form high-pressure air, and various energy storage cycle coalescence engines that inject and burn fuel in the process of final compression heat recovery cooling.   The exhaust heat quantity is compressed by the recovered air storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees of the combustion blade (29E) of the all-wheel impeller mercury turbine (8E) combined engine. Then, compression energy recovery is repeated at least once in the reduced diameter compression chamber mercury heat exchanger (2Z) to form high-pressure air, and various energy storage cycle coalescence engines that inject and burn fuel in the process of final compression heat recovery cooling.   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 ° C. of the combustion section (29F) of the all-wheel impeller mercury turbine (8E) combined engine. Then, compression energy recovery is repeated one or more times in the reduced diameter compression chamber mercury heat exchanger (2Z) to form high-pressure air, and various energy storage cycle coalescence engines that inject and burn fuel in the process of final compression heat recovery cooling.   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of around 230 degrees in the combustion section (29G) of the all-wheel impeller mercury turbine (8E) combined engine. Then, compression energy recovery is repeated one or more times in the reduced diameter compression chamber mercury heat exchanger (2Z) to form high-pressure air, and various energy storage cycle coalescence engines that inject and burn fuel in the process of final compression heat recovery cooling.   The exhaust heat quantity is compressed by the recovered energy storage compressor by the intake air (28a) of the vaporized hot air recovery unit (2B) with the exhaust saturation temperature of about 230 degrees in the combustion section (29H) of the all-wheel impeller mercury turbine (8E) combined engine. Then, compression energy recovery is repeated one or more times in the reduced diameter compression chamber mercury heat exchanger (2Z) to form high-pressure air, and various energy storage cycle coalescence engines that inject and burn fuel in the process of final compression heat recovery cooling.   Vertically moving blade gas turbine (8A) All blade combustion portion (30A) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and a reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Various energy storage Cycle coalescence engine.   Vertically moving blade gas turbine (8A) All blade combustion section (30B) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) to reduce the diameter of the compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Various energy storage Cycle coalescence engine.   Vertically moving blade gas turbine (8A) All blade combustion section (30C) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Various energy storage Cycle coalescence engine.   Vertical-type all-blade gas turbine (8A) all-blade combustion section (30D) The combustion gas reservoir (95a) is provided in an annular shape above the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Various energy storage Cycle coalescence engine.   Vertical-type all-blade gas turbine (8A) all-blade blade combusting section (30E) The nozzle (6) on the circumference is provided with a combustion gas reservoir (95a) in an annular shape to reduce the compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Various energy storage Cycle coalescence engine.   Vertically moving blade gas turbine (8A) All blade combustion section (30F) A nozzle (6) on the circumference of the nozzle (6) is provided with an annular combustion gas reservoir (95a) in an annular compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Various energy storage Cycle coalescence engine.   Vertically moving blade gas turbine (8A) All blade combustion portion (30G) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Various energy storage Cycle coalescence engine.   Vertical-rotor blade gas turbine (8A) All-blade combustion section (30H) Combustion gas reservoir (95a) is provided in the upper part of the nozzle (6) on the circumference, and the reduced diameter compression chamber mercury heat exchanger (2Z) Combustion gas 49 supplied to combustion gas reservoir (95a) Combustion gas control valve (24) Open combustion gas 49 supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Various energy storage Cycle coalescence engine.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of the combustion blade (29a) of the all-wheel impeller gas turbine (8a) combined engine combustion section (29D), and the reduced diameter compression chamber mercury heat exchange Combustion gas 49 is connected to the combustor (2Z) and supplied to the combustion gas reservoir (95a) Combustion gas control valve (24) The open combustion gas 49 is supplied to the combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Various energy conservation cycle coalescing engines.   Combustion gas reservoir (95a) is provided in a cylindrical shape at the upper part in the axial direction meshing with (8a) and (8a) of all rotor blade propeller gas turbine (8a) coalescence engine combustion section (29X), and reduced diameter compression chamber mercury heat exchange. Combustion gas 49 is supplied to the combustion gas reservoir (95a) and the combustion gas control valve (24) is supplied to the combustor (1Y). The fuel injection is ignited from the combustion combustion gas rocket nozzle (6M). Various energy conservation cycle coalescing engines.   A vertical all blade mercury turbine (8H) all blade combustion section (30A) compresses exhaust heat with a recovered energy storage compressor and repeats compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z) Combined with various energy storage cycle engines that produce high-pressure air and mass-produce fuel-injected combustion combustion gas 49 in the process of final compression heat recovery and cooling.   A vertical all-blade mercury turbine (8H) all-blade combustion section (30B) compresses exhaust heat with a recovered energy storage compressor and repeats compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z) Combined with various energy storage cycle engines that produce high-pressure air and mass-produce fuel-injected combustion combustion gas 49 in the process of final compression heat recovery and cooling.   A vertical all-blade mercury turbine (8H) all-blade combustion section (30C) compresses exhaust heat with a recovery energy storage compressor and repeats compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z) Combined with various energy storage cycle engines that produce high-pressure air and mass-produce fuel-injected combustion combustion gas 49 in the process of final compression heat recovery and cooling.   A vertical all blade mercury turbine (8H) all blade combustor (30D) exhaust heat quantity is compressed by a recovery energy storage compressor, and compression heat recovery is repeated at least once by a reduced diameter compression chamber mercury heat exchanger (2Z). Combined with various energy storage cycle engines that produce high-pressure air and mass-produce fuel-injected combustion combustion gas 49 in the process of final compression heat recovery and cooling.   A vertical all-blade mercury turbine (8H) all-blade combustion section (30E) compresses exhaust heat with a recovery energy storage compressor and repeats compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z) Combined with various energy storage cycle engines that produce high-pressure air and mass-produce fuel-injected combustion combustion gas 49 in the process of final compression heat recovery and cooling.   A vertical all-blade mercury turbine (8H) all-blade combustion section (30F) exhaust heat is compressed by a recovered energy storage compressor, and compression heat recovery is repeated at least once in a reduced diameter compression chamber mercury heat exchanger (2Z). Combined with various energy storage cycle engines that produce high-pressure air and mass-produce fuel-injected combustion combustion gas 49 in the process of final compression heat recovery and cooling.   A vertical all blade mercury turbine (8H) all blade combustion section (30G) exhaust heat quantity is compressed by a recovery energy storage compressor, and compression heat recovery is repeated at least once by a reduced diameter compression chamber mercury heat exchanger (2Z). Combined with various energy storage cycle engines that produce high-pressure air and mass-produce fuel-injected combustion combustion gas 49 in the process of final compression heat recovery and cooling.   A vertical all blade mercury turbine (8H) all blade combustion section (30H) exhaust heat quantity is compressed by a recovery energy storage compressor and compression heat recovery is repeated at least once by a reduced diameter compression chamber mercury heat exchanger (2Z). Combined with various energy storage cycle engines that produce high-pressure air and mass-produce fuel-injected combustion combustion gas 49 in the process of final compression heat recovery and cooling.   Combustion section (29A) of all-wheel impeller mercury turbine (8E) combined engine combustion section (29A) compresses exhaust heat with a recovered energy storage compressor, and compresses heat with a reduced diameter compression chamber mercury heat exchanger (2Z) one or more times to increase the pressure Various energy storage cycle coalescing engines that mass-produce fuel-injected combustion combustion gas 49 in the process of air and final compression heat recovery cooling.   Combustion unit (29B) of all blade impeller mercury turbine (8E) combined engine combustion section (29B) Compressed exhaust heat with a recovered energy storage compressor, and compressed heat recovery with a reduced diameter compression chamber mercury heat exchanger (2Z) at least once to increase the pressure Various energy storage cycle coalescing engines that mass-produce fuel-injected combustion combustion gas 49 in the process of air and final compression heat recovery cooling.   Combustion unit (29C) of all blade impeller mercury turbine (8E) combined engine combustion part (29C) Compressed exhaust heat with a recovered energy storage compressor, and compressed heat recovery with a reduced diameter compression chamber mercury heat exchanger (2Z) at least once to increase the pressure Various energy storage cycle coalescing engines that mass-produce fuel-injected combustion combustion gas 49 in the process of air and final compression heat recovery cooling.   Combustion unit (29D) of all blade impeller mercury turbine (8E) Compressed exhaust heat by recovered energy storage compressor, and compression heat recovery is repeated one or more times by the reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that mass-produce fuel-injected combustion combustion gas 49 in the process of air and final compression heat recovery cooling.   Combustion unit (29E) of all blade impeller mercury turbine (8E) Compressed exhaust heat with a recovered energy storage compressor, and compression heat recovery is repeated at least once with a reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that mass-produce fuel-injected combustion combustion gas 49 in the process of air and final compression heat recovery cooling.   Combustion part (29F) of all blade impeller mercury turbine (8E) combined engine combustion part compresses exhaust heat with a recovered energy storage compressor, and compresses heat recovery with a reduced diameter compression chamber mercury heat exchanger (2Z) at least once to increase the pressure Various energy storage cycle coalescing engines that mass-produce fuel-injected combustion combustion gas 49 in the process of air and final compression heat recovery cooling.   Combustion part (29G) of all blade impeller mercury turbine (8E) combined engine combustion part compresses exhaust heat with a recovered energy storage compressor, and compresses heat recovery with a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to increase the pressure Various energy storage cycle coalescing engines that mass-produce fuel-injected combustion combustion gas 49 in the process of air and final compression heat recovery cooling.   Combustion unit (29H) of all blade impeller mercury turbine (8E) combined engine combustion part compresses exhaust heat with recovered energy storage compressor, and compression heat recovery is repeated at least once with reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that mass-produce fuel-injected combustion combustion gas 49 in the process of air and final compression heat recovery cooling.   Vertical all blade gas turbine (8A) All blade combustion section (30A) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) expands and injects in a circular direction.   Vertical-type all blade gas turbine (8A) All blade combustion section (30B) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) expands and injects in a circular direction.   Vertical all blade gas turbine (8A) All blade combustion section (30C) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) expands and injects in a circular direction.   Vertical all blade gas turbine (8A) All blade combustion section (30D) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) expands and injects in a circular direction.   Vertical all blade gas turbine (8A) All blade combustion section (30E) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) expands and injects in a circular direction.   Vertical-type all blade gas turbine (8A) All blade combustion section (30F) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) expands and injects in a circular direction.   Vertical all-blade gas turbine (8A) All-blade combustion section (30G) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) expands and injects in a circular direction.   Vertical all blade gas turbine (8A) All blade combustion section (30H) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) expands and injects in a circular direction.   All blade impeller gas turbine (8a) coalescence engine combustion section (29D) combustion gas control valve (24) open combustion gas 49 is supplied to the combustor (1Y) and injected from the fuel injection ignition combustion combustion gas rocket nozzle (6M) Various energy storage cycle coalescing engines that are expanded in the axial direction by the nozzle injection section (6a).   All blade impeller gas turbine (8a) coalescence engine combustion section (29X) combustion gas control valve (24) open combustion gas 49 is supplied to the combustor (1Y) and injected from the fuel injection ignition combustion combustion gas rocket nozzle (6M) Various energy storage cycle coalescing engines that are expanded in the axial direction by the nozzle injection section (6a).   A vertical all blade mercury turbine (8H) all blade combustion section (30A) compresses exhaust heat with a recovered energy storage compressor and repeats compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z) Various energy storage cycle coalescing engines that produce high-pressure air and mass-produce combustion gas 49 with a large amount of fuel injection combustion oxygen remaining in the process of final compression heat recovery cooling.   A vertical all-blade mercury turbine (8H) all-blade combustion section (30B) compresses exhaust heat with a recovered energy storage compressor and repeats compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z) Various energy storage cycle coalescing engines that produce high-pressure air and mass-produce combustion gas 49 with a large amount of fuel injection combustion oxygen remaining in the process of final compression heat recovery cooling.   A vertical all-blade mercury turbine (8H) all-blade combustion section (30C) compresses exhaust heat with a recovery energy storage compressor and repeats compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z) Various energy storage cycle coalescing engines that produce high-pressure air and mass-produce combustion gas 49 with a large amount of fuel injection combustion oxygen remaining in the process of final compression heat recovery cooling.   A vertical all blade mercury turbine (8H) all blade combustor (30D) exhaust heat quantity is compressed by a recovery energy storage compressor, and compression heat recovery is repeated at least once by a reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that produce high-pressure air and mass-produce combustion gas 49 with a large amount of fuel injection combustion oxygen remaining in the process of final compression heat recovery cooling.   A vertical all-blade mercury turbine (8H) all-blade combustion section (30E) compresses exhaust heat with a recovery energy storage compressor and repeats compression heat recovery one or more times with a reduced diameter compression chamber mercury heat exchanger (2Z) Various energy storage cycle coalescing engines that produce high-pressure air and mass-produce combustion gas 49 with a large amount of fuel injection combustion oxygen remaining in the process of final compression heat recovery cooling.   A vertical all-blade mercury turbine (8H) all-blade combustion section (30F) exhaust heat is compressed by a recovered energy storage compressor, and compression heat recovery is repeated at least once in a reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that produce high-pressure air and mass-produce combustion gas 49 with a large amount of fuel injection combustion oxygen remaining in the process of final compression heat recovery cooling.   A vertical all blade mercury turbine (8H) all blade combustion section (30G) exhaust heat quantity is compressed by a recovery energy storage compressor, and compression heat recovery is repeated at least once by a reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that produce high-pressure air and mass-produce combustion gas 49 with a large amount of fuel injection combustion oxygen remaining in the process of final compression heat recovery cooling.   A vertical all blade mercury turbine (8H) all blade combustion section (30H) exhaust heat quantity is compressed by a recovery energy storage compressor and compression heat recovery is repeated at least once by a reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that produce high-pressure air and mass-produce combustion gas 49 with a large amount of fuel injection combustion oxygen remaining in the process of final compression heat recovery cooling.   Combustion section (29A) of all-wheel impeller mercury turbine (8E) combined engine combustion section (29A) compresses exhaust heat with a recovered energy storage compressor, and compresses heat with a reduced diameter compression chamber mercury heat exchanger (2Z) one or more times to increase the pressure Various energy storage cycle coalescing engines that mass-produce combustion gas 49 with a large amount of fuel-injected combustion oxygen remaining in the course of air and final compression heat recovery cooling.   Combustion unit (29B) of all blade impeller mercury turbine (8E) combined engine combustion section (29B) Compressed exhaust heat with a recovered energy storage compressor, and compressed heat recovery with a reduced diameter compression chamber mercury heat exchanger (2Z) at least once to increase the pressure Various energy storage cycle coalescing engines that mass-produce combustion gas 49 with a large amount of fuel-injected combustion oxygen remaining in the course of air and final compression heat recovery cooling.   Combustion unit (29C) of all blade impeller mercury turbine (8E) combined engine combustion part (29C) Compressed exhaust heat with a recovered energy storage compressor, and compressed heat recovery with a reduced diameter compression chamber mercury heat exchanger (2Z) at least once to increase the pressure Various energy storage cycle coalescing engines that mass-produce combustion gas 49 with a large amount of fuel-injected combustion oxygen remaining in the course of air and final compression heat recovery cooling.   Combustion unit (29D) of all blade impeller mercury turbine (8E) Compressed exhaust heat by recovered energy storage compressor, and compression heat recovery is repeated one or more times by the reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that mass-produce combustion gas 49 with a large amount of fuel-injected combustion oxygen remaining in the course of air and final compression heat recovery cooling.   Combustion unit (29E) of all blade impeller mercury turbine (8E) Compressed exhaust heat with a recovered energy storage compressor, and compression heat recovery is repeated at least once with a reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that mass-produce combustion gas 49 with a large amount of fuel-injected combustion oxygen remaining in the course of air and final compression heat recovery cooling.   Combustion part (29F) of all blade impeller mercury turbine (8E) combined engine combustion part compresses exhaust heat with a recovered energy storage compressor, and compresses heat recovery with a reduced diameter compression chamber mercury heat exchanger (2Z) at least once to increase the pressure Various energy storage cycle coalescing engines that mass-produce combustion gas 49 with a large amount of fuel-injected combustion oxygen remaining in the course of air and final compression heat recovery cooling.   Combustion part (29G) of all blade impeller mercury turbine (8E) combined engine combustion part compresses exhaust heat with a recovered energy storage compressor, and compresses heat recovery with a reduced-diameter compression chamber mercury heat exchanger (2Z) one or more times to increase the pressure Various energy storage cycle coalescing engines that mass-produce combustion gas 49 with a large amount of fuel-injected combustion oxygen remaining in the course of air and final compression heat recovery cooling.   Combustion unit (29H) of all blade impeller mercury turbine (8E) combined engine combustion part compresses exhaust heat with recovered energy storage compressor, and compression heat recovery is repeated at least once with reduced diameter compression chamber mercury heat exchanger (2Z). Various energy storage cycle coalescing engines that mass-produce combustion gas 49 with a large amount of fuel-injected combustion oxygen remaining in the course of air and final compression heat recovery cooling.   Vertical all blade gas turbine (8A) All blade combustion section (30A) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) similarly accelerates and injects the nozzle (6) in the circular direction.   Vertical-type all blade gas turbine (8A) All blade combustion section (30B) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) similarly accelerates and injects the nozzle (6) in the circular direction.   Vertical all blade gas turbine (8A) All blade combustion section (30C) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) similarly accelerates and injects the nozzle (6) in the circular direction.   Vertical all blade gas turbine (8A) All blade combustion section (30D) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) similarly accelerates and injects the nozzle (6) in the circular direction.   Vertical all blade gas turbine (8A) All blade combustion section (30E) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) similarly accelerates and injects the nozzle (6) in the circular direction.   Vertical-type all blade gas turbine (8A) All blade combustion section (30F) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) similarly accelerates and injects the nozzle (6) in the circular direction.   Vertical all-blade gas turbine (8A) All-blade combustion section (30G) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) similarly accelerates and injects the nozzle (6) in the circular direction.   Vertical all blade gas turbine (8A) All blade combustion section (30H) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines in which the nozzle injection section (6a) similarly accelerates and injects the nozzle (6) in the circular direction.   All blade impeller gas turbine (8a) coalescence engine combustion section (29D) combustion gas control valve (24) open combustion gas 49 is supplied to the combustor (1Y) and injected from the fuel injection ignition combustion combustion gas rocket nozzle (6M) Various energy storage cycle coalescing engines which perform expansion acceleration injection in the axial direction by the nozzle injection section (6a).   All blade impeller gas turbine (8a) coalescence engine combustion section (29X) combustion gas control valve (24) open combustion gas 49 is supplied to the combustor (1Y) and injected from the fuel injection ignition combustion combustion gas rocket nozzle (6M) Various energy storage cycle coalescing engines which perform expansion acceleration injection in the axial direction by the nozzle injection section (6a).   Various energies that drive the vertical all-blade gas turbine (8A) by mass-producing the combustion gas 49 with a large amount of oxygen remaining with the exhaust heat quantity of the vertical blade mercury turbine (8H) all blade combustion section (30A) Conservation cycle coalescence organization.   Various energies that drive the vertical all-blade gas turbine (8A) by mass-producing the combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical blade mercury turbine (8H) all blade combustion section (30B) Conservation cycle coalescence organization.   Various energies that drive the vertical all-blade gas turbine (8A) by mass-producing the combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical blade mercury turbine (8H) all blade combustion section (30C) Conservation cycle coalescence organization.   Various energies that drive the vertical all-blade gas turbine (8A) by mass-producing the combustion gas 49 with a large amount of oxygen remaining with the exhaust heat quantity of the vertical blade mercury turbine (8H) all blade combustion section (30D) Conservation cycle coalescence organization.   Various energies that drive the vertical all-blade gas turbine (8A) by mass-producing the combustion gas 49 with a large amount of residual oxygen by the exhaust heat quantity of the vertical all-blade mercury turbine (8H) all-blade combustion section (30E) Conservation cycle coalescence organization.   Various energies that drive the vertical all-blade gas turbine (8A) by mass-producing the combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical all-blade mercury turbine (8H) all-blade combustion section (30F) Conservation cycle coalescence organization.   Various energies that drive the vertical all-blade gas turbine (8A) by mass-producing the combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical blade mercury turbine (8H) all blade combustion section (30G) Conservation cycle coalescence organization.   Various types of energy for driving a vertical all-blade gas turbine (8A) by mass-producing a combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical blade mercury turbine (8H) all blade combustion section (30H) Conservation cycle coalescence organization.   Combined with various energy storage cycles for mass production of combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of combustion blade (29A) of all blade impeller mercury turbine (8E) engine and driving all blade impeller gas turbine (8a) organ.   Combining various energy storage cycles for mass production of combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of all rotor blade mercury turbine (8E) engine combustion section (29B) to drive all rotor blade gas turbine gas turbine (8a) organ.   Combining various energy storage cycles to drive mass turbine combustion gas 49 (8a) by mass-producing combustion gas 49 with a large amount of residual oxygen by exhaust heat quantity of engine combustion unit (29C) organ.   Combining various energy storage cycles for mass production of combustion gas 49 with a large amount of residual oxygen by exhaust heat quantity of the combustion blade (29D) of the all blade impeller mercury turbine (8E) and driving the all blade impeller gas turbine (8a) organ.   Combined with various energy storage cycles for mass production of combustion gas 49 with a large amount of residual oxygen by exhaust heat quantity of engine combustion unit (29E) of all-blade bouncing mercury turbine (8E) and driving all-blade bouncing turbine gas turbine (8a) organ.   Combined with various energy storage cycles to drive all-blade bouncer gas turbine (8a) by mass-producing combustion gas 49 with a large amount of residual oxygen by exhaust heat quantity of combustion blade (29F) of all-blade bouncer mercury turbine (8E) organ.   Combined with various energy storage cycle to drive mass turbine combustion gas 49 (8a) by mass-producing combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of combustion unit (29G) organ.   Combined with various energy storage cycles to drive the all-blade bouncer gas turbine (8a) by mass-producing the combustion gas 49 with a large amount of residual oxygen by the exhaust heat quantity of the all-blade bouncer mercury turbine (8E) combined engine combustion section (29H) organ.   Vertical all blade gas turbine (8A) All blade combustion section (30A) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines that similarly drive the acceleration injection saddle type full blade air turbine (8A) even with the nozzle (6) enlarged in the circular direction by the nozzle injection section (6a).   Vertical-type all blade gas turbine (8A) All blade combustion section (30B) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines that similarly drive the acceleration injection saddle type full blade air turbine (8A) even with the nozzle (6) enlarged in the circular direction by the nozzle injection section (6a).   Vertical all blade gas turbine (8A) All blade combustion section (30C) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines that similarly drive the acceleration injection saddle type full blade air turbine (8A) even with the nozzle (6) enlarged in the circular direction by the nozzle injection section (6a).   Vertical all blade gas turbine (8A) All blade combustion section (30D) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines that similarly drive the acceleration injection saddle type full blade air turbine (8A) even with the nozzle (6) enlarged in the circular direction by the nozzle injection section (6a).   Vertical all blade gas turbine (8A) All blade combustion section (30E) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines that similarly drive the acceleration injection saddle type full blade air turbine (8A) even with the nozzle (6) enlarged in the circular direction by the nozzle injection section (6a).   Vertical-type all blade gas turbine (8A) All blade combustion section (30F) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines that similarly drive the acceleration injection saddle type full blade air turbine (8A) even with the nozzle (6) enlarged in the circular direction by the nozzle injection section (6a).   Vertical all-blade gas turbine (8A) All-blade combustion section (30G) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines that similarly drive the acceleration injection saddle type full blade air turbine (8A) even with the nozzle (6) enlarged in the circular direction by the nozzle injection section (6a).   Vertical all blade gas turbine (8A) All blade combustion section (30H) Combustion gas control valve (24) Open combustion gas 49 is supplied to combustor (1Y) Fuel injection Ignition combustion combustion gas rocket nozzle (6M) Then, various energy storage cycle coalescing engines that similarly drive the acceleration injection saddle type full blade air turbine (8A) even with the nozzle (6) enlarged in the circular direction by the nozzle injection section (6a).   All blade impeller gas turbine (8a) coalescence engine combustion section (29D) combustion gas control valve (24) open combustion gas 49 is supplied to the combustor (1Y) and injected from the fuel injection ignition combustion combustion gas rocket nozzle (6M) Various energy storage cycle coalescing engines in which the nozzle nozzle (6a) is similarly accelerated and ejected in the axial direction by the nozzle (6a) to drive the entire moving blade bouncer gas turbine (8a).   All blade impeller gas turbine (8a) coalescence engine combustion section (29X) combustion gas control valve (24) open combustion gas 49 is supplied to the combustor (1Y) and injected from the fuel injection ignition combustion combustion gas rocket nozzle (6M) Various energy storage cycle coalescing engines in which the nozzle nozzle (6a) is similarly accelerated and ejected in the axial direction by the nozzle (6a) to drive the entire moving blade bouncer gas turbine (8a).   Combined with various energy storage cycles that mass-produce combustion gas 49 with a large amount of residual oxygen by exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion section (30A) and inject it from combined engine injection section (78K) organ.   Combined with various energy storage cycles that mass-produce combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustion section (30B) and inject it from combined engine injection section (78K) organ.   Combined with various energy storage cycles that mass-produce combustion gas 49 with a large amount of residual oxygen by exhaust heat quantity of vertical all-blade mercury turbine (8H) all-blade combustion section (30C) and inject from combined engine injection section (78K) organ.   Combined with various energy storage cycles that mass-produce combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical all-blade mercury turbine (8H) all-blade combustion section (30D) and inject from combined engine injection section (78K) organ.   Combined with various energy storage cycles to mass-produce combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustion section (30E) and inject it from combined engine injection section (78K) organ.   Combined with various energy storage cycles that mass-produce combustion gas 49 with a large amount of residual oxygen with exhaust heat from the vertical blade mercury turbine (8H) all blade combustion section (30G) and inject it from the combined engine injection section (78K) organ.   Combined with various energy storage cycles that mass-produce combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustion section (30H) and inject it from combined engine injection section (78K) organ.   Various energy storage cycle coalescence engine that mass-produces combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of all rotor blade mercury turbine mercury turbine (8E) coalescence engine combustion section (29A) and injects it from coalescence engine injection section (78K).   Various energy storage cycle coalescence engine that mass-produces combustion gas 49 with a large amount of oxygen remaining with the exhaust heat quantity of the all-blade impeller mercury turbine (8E) coalescence engine combustion section (29A) and injects it from the coalescence engine injection section (78K).   Various energy storage cycle coalescence engine that mass-produces combustion gas 49 with a large amount of oxygen remaining with the exhaust heat quantity of the all-blade impeller mercury turbine (8E) coalescence engine combustion section (29A) and injects it from the coalescence engine injection section (78K)   Various energy storage cycle coalescence engine that mass-produces combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of all rotor blade mercury turbine mercury turbine (8E) coalescence engine combustion section (29A) and injects it from coalescence engine injection section (78K).   Various energy storage cycle coalescence engine that mass-produces combustion gas 49 with a large amount of oxygen remaining with the exhaust heat quantity of the all-blade impeller mercury turbine (8E) coalescence engine combustion section (29A) and injects it from the coalescence engine injection section (78K).   Various energy storage cycle coalescence engine that mass-produces combustion gas 49 with a large amount of oxygen remaining with the exhaust heat quantity of the all-blade impeller mercury turbine (8E) coalescence engine combustion section (29A) and injects it from the coalescence engine injection section (78K).   Various energy storage cycle coalescence engine that mass-produces combustion gas 49 with a large amount of oxygen remaining with the exhaust heat quantity of the all-blade impeller mercury turbine (8E) coalescence engine combustion section (29A) and injects it from the coalescence engine injection section (78K).   Various energy storage cycle coalescence engine that mass-produces combustion gas 49 with a large amount of oxygen remaining with the exhaust heat quantity of the all-blade impeller mercury turbine (8E) coalescence engine combustion section (29A) and injects it from the coalescence engine injection section (78K).   Vertical-type all-blade gas turbine (8A) All-blade combustion section (30A) Combustion gas control valve (24) Open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and circularly directed by the nozzle injection section (6a). In the same way, the various types of energy storage cycle coalescence engine that drives the acceleration injection vertical all-blade gas turbine (8A) with the expansion nozzle (6).   Vertical-type all blade gas turbine (8A) All blade combustion section (30B) Combustion gas control valve (24) Open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and circularly directed by the nozzle injection section (6a). In the same way, the various types of energy storage cycle coalescence engine that drives the acceleration injection vertical all-blade gas turbine (8A) with the expansion nozzle (6).   Vertical-type all blade gas turbine (8A) All blade combustion section (30C) Combustion gas control valve (24) Open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and circularly directed by the nozzle injection section (6a). In the same way, the various types of energy storage cycle coalescence engine that drives the acceleration injection vertical all-blade gas turbine (8A) with the expansion nozzle (6).   Vertical-type all blade gas turbine (8A) All blade combustion section (30D) Combustion gas control valve (24) Open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and circularly directed by the nozzle injection section (6a). In the same way, the various types of energy storage cycle coalescence engine that drives the acceleration injection vertical all-blade gas turbine (8A) with the expansion nozzle (6).   Vertical-type all-blade gas turbine (8A) All-blade blade combustion section (30E) Combustion gas control valve (24) Open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and circularly directed by the nozzle injection section (6a). In the same way, the various types of energy storage cycle coalescence engine that drives the acceleration injection vertical all-blade gas turbine (8A) with the expansion nozzle (6).   Vertical-type all blade gas turbine (8A) All blade combustion section (30F) Combustion gas control valve (24) Open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and circularly directed by the nozzle injection section (6a). In the same way, the various types of energy storage cycle coalescence engine that drives the acceleration injection vertical all-blade gas turbine (8A) with the expansion nozzle (6).   Vertical-type all-blade gas turbine (8A) all-blade blade combustion section (30G) combustion gas control valve (24) open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and circularly directed by the nozzle injection section (6a) In the same way, the various types of energy storage cycle coalescence engine that drives the acceleration injection vertical all-blade gas turbine (8A) with the expansion nozzle (6).   Vertical-type all blade gas turbine (8A) All blade combustion section (30H) Combustion gas control valve (24) Open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and circularly directed by the nozzle injection section (6a). In the same way, the various types of energy storage cycle coalescence engine that drives the acceleration injection vertical all-blade gas turbine (8A) with the expansion nozzle (6).   All-wheel impeller gas turbine (8a) coalescence engine combustion section (30D) combustion gas control valve (24) open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and expanded in the axial direction by the nozzle injection section (6a) Various energy storage cycle coalescing engines that drive the acceleration-jet all-wheel impeller gas turbine (8a).     All-wheel impeller gas turbine (8a) coalescence engine combustion section (30X) combustion gas control valve (24) open combustion gas 49 is injected from the combustion gas rocket nozzle (6M) and expanded in the axial direction by the nozzle injection section (6a) Various energy storage cycle coalescing engines that drive the acceleration-jet all-wheel impeller gas turbine (8a).   Combined engine injection unit (78K) combustion gas injection rocket nozzle (6Y) by mass-producing combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustion part (30A) Various energy storage cycle coalescing engines that inject more.   Combined engine injection unit (78K) combustion gas injection rocket nozzle (6Y) by mass-producing combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion part (30B) Various energy storage cycle coalescing engines that inject more.   Combined engine injection unit (78K) combustion gas injection rocket nozzle (6Y) by mass-producing combustion gas 49 with a large amount of oxygen remaining with exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion unit (30C) Various energy storage cycle coalescing engines that inject more.   Combustion gas injection unit (78K) combustion gas injection rocket nozzle (6Y) by mass production of combustion gas 49 with a large amount of oxygen remaining with exhaust heat quantity of vertical blade turbine (8H) all blade combustion part (30D) Various energy storage cycle coalescing engines that inject more.   Combined engine injection unit (78K) Combustion gas injection rocket nozzle (6Y) by mass-producing combustion gas 49 with a large amount of oxygen remaining with exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustion unit (30E) Various energy storage cycle coalescing engines that inject more.   Combined engine injection unit (78K) combustion gas injection rocket nozzle (6Y) by mass-producing combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion part (30F) Various energy storage cycle coalescing engines that inject more.   Combined engine injection unit (78K) Combustion gas injection rocket nozzle (6Y) by mass production of combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustion part (30G) Various energy storage cycle coalescing engines that inject more.   Combined engine injection unit (78K) combustion gas injection rocket nozzle (6Y) by mass-producing combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion unit (30H) Various energy storage cycle coalescing engines that inject more.   Massive production of combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of all rotor blade mercury turbine mercury turbine (8E) coalescence engine combustion section (29A) and inject from coalescence engine injection section (78K) combustion gas injection rocket nozzle (6Y) Various energy conservation cycle coalescing engines.   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-blade impeller mercury turbine (8E) combined engine combustion section (29B) and inject from the combined engine injection section (78K) combustion gas injection rocket nozzle (6Y) Various energy conservation cycle coalescing engines.   Massive production of combustion gas 49 with a large amount of residual oxygen by exhaust heat quantity of all-rotor impeller mercury turbine (8E) combined engine combustion section (29C) and inject from combined engine injection section (78K) combustion gas injection rocket nozzle (6Y) Various energy conservation cycle coalescing engines.   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-wheel impeller mercury turbine (8E) coalescence engine combustion section (29D) and inject from the coalescence engine injection section (78K) combustion gas injection rocket nozzle (6Y) Various energy conservation cycle coalescing engines.   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29E) and inject from combined engine injection section (78K) combustion gas injection rocket nozzle (6Y) Various energy conservation cycle coalescing engines.   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all-rotor impeller mercury turbine (8E) combined engine combustion section (29F) and inject from combined engine injection section (78K) combustion gas injection rocket nozzle (6Y) Various energy conservation cycle coalescing engines.   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-blade impeller mercury turbine (8E) combined engine combustion section (29G) and inject from the combined engine injection section (78K) combustion gas injection rocket nozzle (6Y) Various energy conservation cycle coalescing engines.   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-wheel impeller mercury turbine (8E) coalescence engine combustion section (29H) and inject from the coalescence engine injection section (78K) combustion gas injection rocket nozzle (6Y) Various energy conservation cycle coalescing engines.   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustor (30A) is mass-produced, and fuel injection is performed by a combined engine injector (78K) combustor (1Y) Various energy storage cycle coalescing engine that injects from combustion combustion gas injection rocket nozzle (6Y).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical blade mercury turbine (8H) all blade combustion section (30B) is mass-produced, and fuel injection is performed by the combined engine injection section (78K) combustor (1Y). Various energy storage cycle coalescing engine that injects from combustion combustion gas injection rocket nozzle (6Y).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical blade mercury turbine (8H) all blade combustion section (30C) is mass-produced, and fuel is injected by the combined engine injection section (78K) combustor (1Y). Various energy storage cycle coalescing engine that injects from combustion combustion gas injection rocket nozzle (6Y).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion section (30D) is mass-produced, and fuel injection is performed by a combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engine that injects from combustion combustion gas injection rocket nozzle (6Y).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion section (30E) is mass-produced, and fuel injection is performed by a combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engine that injects from combustion combustion gas injection rocket nozzle (6Y).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical all-blade mercury turbine (8H) all-blade combustion section (30F) is mass-produced, and fuel injection is performed by a combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engine that injects from combustion combustion gas injection rocket nozzle (6Y).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion section (30G) is mass-produced, and fuel injection is performed by a combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engine that injects from combustion combustion gas injection rocket nozzle (6Y).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical blade-type all-blade mercury turbine (8H) all-blade combustion section (30H) is mass-produced, and fuel is injected by the combined engine injection section (78K) combustor (1Y). Various energy storage cycle coalescing engine that injects from combustion combustion gas injection rocket nozzle (6Y).   Massive production of combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of all rotor blade propeller mercury turbine (8E) coalescence engine combustion section (29A) and fuel injection combustion in coalescence engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines that inject from the combustion gas injection rocket nozzle (6Y).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-wheel impeller mercury turbine (8E) combined engine combustion section (29B), and fuel injection combustion in the combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines that inject from the combustion gas injection rocket nozzle (6Y).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-blade impeller mercury turbine (8E) combined engine combustion section (29C) and fuel injection combustion in the combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines that inject from the combustion gas injection rocket nozzle (6Y).   Massive production of combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29D), and fuel injection combustion in combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines that inject from the combustion gas injection rocket nozzle (6Y).   Massive production of combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of all rotor blade propeller mercury turbine (8E) coalescence engine combustion section (29E), and fuel injection combustion in coalescence engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines that inject from the combustion gas injection rocket nozzle (6Y).   Massive production of combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of all rotor blade propeller mercury turbine (8E) coalescence engine combustion section (29F) and fuel injection combustion in coalescence engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines that inject from the combustion gas injection rocket nozzle (6Y).   Massive production of combustion gas 49 with a large amount of oxygen remaining by exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29G), and fuel injection combustion in combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines that inject from the combustion gas injection rocket nozzle (6Y).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29H), and fuel injection combustion in combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines that inject from the combustion gas injection rocket nozzle (6Y).   Combustion gas 49 is produced by mass production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustion section (30A), and burned by combined engine injection section (78K) combustor (1Y) A superheated steam reservoir (95C) is provided in an annular shape, and the superheated steam 50 is injected from the heated superheated steam rocket nozzle (6L).   Combustion gas 49 is produced by mass production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion section (30B) and burned in the combined engine injection section (78K) combustor (1Y) A superheated steam reservoir (95C) is provided in an annular shape, and the superheated steam 50 is injected from the heated superheated steam rocket nozzle (6L).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of a vertical all-blade mercury turbine (8H) all-blade combustion section (30C) and combustion in the combined engine injection section (78K) combustor (1Y) A superheated steam reservoir (95C) is provided in an annular shape, and the superheated steam 50 is injected from the heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical all-blade mercury turbine (8H) all-blade combustion section (30D) and combustion in the combined engine injection section (78K) combustor (1Y) A superheated steam reservoir (95C) is provided in an annular shape, and the superheated steam 50 is injected from the heated superheated steam rocket nozzle (6L).   Combustion gas 49 is produced by mass production of combustion gas 49 with a large amount of residual oxygen by exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion section (30E), and burned by combined engine injection section (78K) combustor (1Y) A superheated steam reservoir (95C) is provided in an annular shape, and the superheated steam 50 is injected from the heated superheated steam rocket nozzle (6L).   Mass production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical all-blade mercury turbine (8H) all-blade combustion section (30F), and combustion outer circumference in combined engine injection section (78K) combustor (1Y) A superheated steam reservoir (95C) is provided in an annular shape, and the superheated steam 50 is injected from the heated superheated steam rocket nozzle (6L).   Combustion gas 49 is produced by mass production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical all-blade mercury turbine (8H) all-blade combustion section (30G), and combustion is performed by a combined engine injection section (78K) combustor (1Y). A superheated steam reservoir (95C) is provided in an annular shape, and the superheated steam 50 is injected from the heated superheated steam rocket nozzle (6L).   Combustion gas 49 is produced by mass production of combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion section (30H), and burned by combined engine injection section (78K) combustor (1Y) A superheated steam reservoir (95C) is provided in an annular shape, and the superheated steam 50 is injected from the heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29A) and overheated to the combustion outer periphery with combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29B) and overheated to the combustion outer periphery with combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-wheel impeller mercury turbine (8E) combined engine combustion section (29C) and overheated to the combustion outer periphery with the combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-blade propeller mercury turbine (8E) coalescence engine combustion section (29D) and overheated to the combustion outer periphery in the coalescence engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-blade propeller mercury turbine (8E) combined engine combustion section (29E) and overheated to the combustion outer periphery with the combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29F) and overheated to the combustion outer periphery with combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29G) and overheated to the combustion outer periphery with combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29H) and overheated to the combustion outer periphery with combined engine injection section (78K) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical all-blade mercury turbine (8H) all-blade combustion section (30A) is mass-produced and overheated to the combustion periphery with a water jet (78M) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the vertical blade mercury turbine (8H) all blade combustion section (30B) is mass-produced and overheated to the combustion periphery with a water jet (78M) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Mass production of combustion gas 49 with a large amount of residual oxygen with exhaust heat of vertical blade mercury turbine (8H) all blade combustion section (30C), and overheated around combustion periphery with water jet (78M) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Mass production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustion section (30D), and overheated to the combustion periphery with water jet (78M) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Mass production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustor (30E), and overheated to the combustion periphery with water jet (78M) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Mass production of combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion section (30F), and overheated to the outer periphery of combustion with water jet (78M) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Mass production of combustion gas 49 with a large amount of oxygen remaining with exhaust heat quantity of vertical blade mercury turbine (8H) all blade combustion section (30G), and overheated to the outer periphery of combustion with water jet (78M) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Mass production of combustion gas 49 with a large amount of residual oxygen with exhaust heat quantity of vertical all blade mercury turbine (8H) all blade combustion section (30H), and overheated to the combustion periphery with water jet (78M) combustor (1Y) Various energy storage cycle coalescing engines in which a steam reservoir (95C) is provided in an annular shape and superheated steam 50 is injected from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the combustion blade (29A) of the all-wheel impeller mercury turbine (8E) combined engine, and a superheated steam pool on the combustion periphery with a water jet (78M) combustor (1Y) (95C) is provided in an annular shape, and various energy storage cycle combined engines that inject superheated steam 50 from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion part (29B), and superheated steam pool on the combustion outer periphery with water jet (78M) combustor (1Y) (95C) is provided in an annular shape, and various energy storage cycle combined engines that inject superheated steam 50 from a heated superheated steam rocket nozzle (6L).   Mass production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the combustion blade (29C) of the all-wheel impeller mercury turbine (8E) combined engine and overheated steam pool on the outer periphery of combustion with a water jet (78M) combustor (1Y) (95C) is provided in an annular shape, and various energy storage cycle combined engines that inject superheated steam 50 from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-blade impeller mercury turbine (8E) combined engine combustion section (29D), and a superheated steam reservoir on the combustion periphery with a water jet (78M) combustor (1Y) (95C) is provided in an annular shape, and various energy storage cycle combined engines that inject superheated steam 50 from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all-wheel impeller mercury turbine (8E) combined engine combustion section (29E), and superheated steam pools on the outer periphery of combustion with water jet (78M) combustor (1Y) (95C) is provided in an annular shape, and various energy storage cycle combined engines that inject superheated steam 50 from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of all rotor blade propeller mercury turbine (8E) combined engine combustion section (29F), and overheated steam pool on the outer periphery of combustion with water jet (78M) combustor (1Y) (95C) is provided in an annular shape, and various energy storage cycle combined engines that inject superheated steam 50 from a heated superheated steam rocket nozzle (6L).   Massive production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the all-blade impeller mercury turbine (8E) combined engine combustion section (29G), and a superheated steam reservoir on the combustion periphery with a water jet (78M) combustor (1Y) (95C) is provided in an annular shape, and various energy storage cycle combined engines that inject superheated steam 50 from a heated superheated steam rocket nozzle (6L).   Mass production of combustion gas 49 with a large amount of oxygen remaining in the exhaust heat quantity of the combustion blade (29H) of the all-wheel impeller mercury turbine (8E) combined engine, and a superheated steam pool on the combustion periphery with a water jet (78M) combustor (1Y) (95C) is provided in an annular shape, and various energy storage cycle combined engines that inject superheated steam 50 from a heated superheated steam rocket nozzle (6L).   Various energy storage cycle coalescence engine equipped with vertical all blade mercury turbine (8H).   Various energy storage cycle coalescing engine equipped with vertical all blade mercury turbine (8H) all blade combustion section (30X).   Various energy storage cycle coalescence engine equipped with all-wheel impeller mercury turbine (8E).   Various energy storage cycle coalescing engines equipped with all-wheel impeller mercury turbine (8E) coalescence engine combustion section (29X).   Various energy storage cycle coalescing engine equipped with vertical type moving blade mercury turbine (8H) coalescence engine injection part (78K).   Various energy storage cycle coalescing engines equipped with vertical all blade mercury turbine (8H) water jet (78M) and various water suction / injection drive devices.   Various energy storage cycle combined engines of various water suction / injection drive equipment equipped with a water jet (78M) for driving a vertical all blade mercury turbine (8H) with high-temperature mercury (1d).   Various energy storage cycle coalescing engines using water jets (78M) that drive a vertical all blade mercury turbine (8H) with high-temperature mercury (1d) and various water suction / injection drive devices including various generators.   Various waters including various generators that use a water jet (78M) to drive a vertical all blade mercury turbine (8H) with high-temperature mercury (1d) and reduce friction loss by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as suction injection drive devices.   Various energy storage cycle coalescence engines that use a water jet (78M) that drives a vertical all blade mercury turbine (8H) with high-temperature mercury (1d) and reduce friction loss by rolling contact of high-temperature mercury (1d).   Various energy storage cycle coalescing engines equipped with vertical all blade mercury turbine (8H) coalescence engine injection section (78K) and various air suction / injection drive devices.   Various energy storage cycle coalescing engines of various air suction jet driving devices equipped with a coalesced engine injection unit (78K) for driving a vertical type moving blade mercury turbine (8H) with high-temperature mercury (1d).   Combined with various energy storage cycles using a combined engine injection part (78K) that drives a vertical all blade mercury turbine (8H) with high-temperature mercury (1d) and various air suction injection drive devices including various generators organ.   Includes various generators that use a combined engine injection unit (78K) that drives a vertical all blade mercury turbine (8H) with high-temperature mercury (1d) and reduces friction loss due to rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Various energy storage cycle coalescing engines that use a combined engine injection unit (78K) that drives a vertical turbine blade turbine (8H) with high-temperature mercury (1d) to reduce friction loss by rolling contact with high-temperature mercury (1d).   Various energy storage cycle coalescence engine equipped with all-wheel impeller mercury turbine (8E) water jet (78M) and various water suction / injection drive devices.   Various energy storage cycle coalescing engines of various water suction / injection drive devices equipped with a water jet (78M) for driving a whole moving blade propeller mercury turbine (8E) with high-temperature mercury (1d).   Various energy storage cycle coalescing engines using water jets (78M) that drive a high-speed mercury (1d) to drive all-wheel impeller mercury turbine (8E) and various water suction / injection drive devices including various generators.   Various water suctions including various generators that use a water jet (78M) that drives a high-speed mercury (1d) to drive a bladed turbine mercury turbine (8E) with high-temperature mercury (1d) and reduce friction loss by rolling contact with high-temperature mercury (1d) Various energy storage cycle coalescing engines as injection drive devices.   Various energy storage cycle coalescing engines that use a water jet (78M) that drives a full turbine impeller mercury turbine (8E) with high-temperature mercury (1d) and reduce friction loss by rolling contact with high-temperature mercury (1d).   Various energy storage cycle coalescing engines as various air suction injection drive devices that use a coalesced engine injection part (78K) and reduce friction loss of a vertical all blade mercury turbine (8H) by surface tension of high-temperature mercury 1d.   Various energy storage cycle coalescing engines that use a combined engine injection unit (78K) and increase the rotational output of a vertical all blade mercury turbine (8H) by the gravity of high-temperature mercury (1d) as various air suction injection drive devices .   Various energy storage cycles as various air suction injection drive equipment that uses a combined engine injection part (78K) and reduces friction loss with a vertical all blade mercury turbine (8H) by rolling contact of high temperature mercury (1d) Combined organization.   Combined with various energy storage cycle as various air suction injection drive equipment that uses combined engine injection part (78K) and increases rotational output of vertical all blade mercury turbine (8H) by rolling contact of high temperature mercury (1d) organ.   Various energy storage cycle coalescing engines as various air suction injection drive devices that use a combined engine injection part (78K) and reduce friction loss of a vertical all blade mercury turbine (8H) by rolling contact with mercury.   Various energy storage cycle coalescing engines as various air suction injection drive devices that use a coalesced engine injection part (78K) and reduce the friction loss of a vertical all blade mercury turbine (8H) by the surface tension of mercury.   Various energies used as various air suction injection drive equipment including various combat capabilities that use a combined engine injection part (78K) and reduce the friction loss of a vertical all blade mercury turbine (8H) by water repellent action (3G) Conservation cycle coalescence organization.   Using a combined engine injection section (78K), various air suction injection drive devices including various combat capabilities that reduce friction loss of a vertical all blade mercury turbine (8H) by surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Using a combined engine injection section (78K), various air suction injection drive devices including various combat capabilities that increase the rotational output of the vertical all-blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Using a combined engine injection section (78K), various air suction injection drive devices including various combat capabilities that reduce friction loss of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Using a combined engine injection section (78K), various air suction injection drive devices including various combat capabilities that increase the rotational output of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Various energy storage cycles using various combined air suction injection drive equipment including various combat capabilities that use a coalescence engine injection section (78K) and reduce friction loss of vertical all-blade mercury turbine (8H) by rolling contact of mercury Combined organization.   Various energy storage cycles using a combined engine injection unit (78K) and various air suction injection drive devices including various combat capabilities that reduce friction loss of a vertical all blade mercury turbine (8H) by the surface tension of mercury Combined organization.   Various air suction injection drive equipment including various air combat capabilities that use a coalesced engine injection part (78K) and reduce the friction loss of vertical turbine blades (8H) by water repellent action (3G) Energy conservation cycle coalescence engine.   Various air suction injection drive devices including various air combat capabilities that use a combined engine injection part (78K) and reduce friction loss of a vertical all-blade mercury turbine (8H) by surface tension of high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various air combat capabilities that use a combined engine injection section (78K) and increase the rotational output of the vertical all-blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various air combat capabilities that use a combined engine injection section (78K) and reduce friction loss of the vertical all blade mercury turbine (8H) by rolling contact with high temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various air combat capabilities that use a combined engine injection section (78K) and increase the rotational output of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various energies for various air suction injection drive equipment including various air combat capabilities that use a combined engine injection section (78K) to reduce friction loss of a vertical all blade mercury turbine (8H) by rolling contact with mercury Conservation cycle coalescence organization.   Uses a combined engine injection section (78K) and saves various energy as air suction injection drive equipment including various air combat capabilities that reduce the friction loss of the vertical all blade mercury turbine (8H) by the surface tension of mercury Cycle coalescence engine.   Various energies for various air suction injection drive equipment including various cockpits that use a combined engine injection part (78K) to reduce friction loss of a vertical all blade mercury turbine (8H) by water repellent action (3G) Conservation cycle coalescence organization.   Using a combined engine injection section (78K), various air suction injection drive devices including various cockpits that reduce friction loss of a vertical all blade mercury turbine (8H) by surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various cockpits that use a combined engine injection section (78K) and increase the rotational output of a vertical all blade mercury turbine (8H) by surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Using a combined engine injection section (78K), various air suction injection drive devices including various cockpits that reduce friction loss of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various cockpits that use a combined engine injection section (78K) and increase the rotational output of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various energy storage cycles as various air suction injection drive devices including various cockpits that use a combined engine injection part (78K) and reduce friction loss of vertical all blade mercury turbine (8H) by rolling contact of mercury Combined organization.   Various energy storage cycles as various air suction injection drive devices including various cockpits that use a combined engine injection section (78K) and reduce friction loss of vertical turbine blade mercury turbine (8H) by surface tension of mercury Combined organization.   Various types of energy used as various air suction injection drive devices including various control chambers that use a combined engine injection unit (78K) and reduce the friction loss of a vertical all blade mercury turbine (8H) by water repellent action (3G) Conservation cycle coalescence organization.   Using a combined engine injection section (78K), various air suction injection drive devices including various control chambers that reduce friction loss of a vertical all blade mercury turbine (8H) by surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various control chambers that use a combined engine injection section (78K) and increase the rotational output of a vertical all blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Using a combined engine injection unit (78K), various air suction injection drive devices including various control chambers that reduce friction loss of a vertical all blade mercury turbine (8H) by rolling contact of high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various control chambers that use a combined engine injection section (78K) and increase the rotational output of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Various energy storage cycles as various air suction injection drive equipment including various control chambers using combined engine injection part (78K) and reducing friction loss of vertical all blade mercury turbine (8H) by rolling contact of mercury Combined organization.   Various energy storage cycles as various air suction injection drive equipment including various control chambers using coalescence engine injection part (78K) and reducing friction loss of vertical turbine blade turbine (8H) by surface tension of mercury Combined organization.   Uses a combined engine injection unit (78K) and saves various energy as various air suction injection drive devices including various cabins that reduce friction loss of a vertical all-blade turbine (8H) by water repellent action (3G) Cycle coalescence engine.   Various air suction injection drive devices including various cabins that use a coalesced engine injection section (78K) and reduce friction loss of vertical turbine blade turbine (8H) by surface tension of high-temperature mercury (1d) Energy conservation cycle coalescence engine.   A variety of air suction injection drive devices including various cabins that use a combined engine injection section (78K) and increase the rotational output of a vertical all blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d) Energy conservation cycle coalescence engine.   Various air suction injection drive devices including various cabins that use a coalesced engine injection part (78K) and reduce friction loss of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d) Energy conservation cycle coalescence engine.   Various air suction injection drive devices including various cabins that use a combined engine injection section (78K) and increase the rotational output of a vertical all-blade turbine (8H) by rolling contact with high-temperature mercury (1d) Energy conservation cycle coalescence engine.   Combined with various energy storage cycle as various air suction injection drive equipment including various cabins using combined engine injection part (78K) to reduce friction loss of vertical all blade mercury turbine (8H) by rolling contact of mercury organ.   Combined with various energy storage cycle as various air suction injection drive equipment including various guest rooms that use coalescence engine injection part (78K) and reduce friction loss of vertical all-blade mercury turbine (8H) by surface tension of mercury organ.   Various energies for various air suction injection drive devices including various cargo compartments that use a combined engine injection part (78K) and reduce friction loss of vertical turbine blades (8H) by water repellent action (3G) Conservation cycle coalescence organization.   Using a combined engine injection section (78K), various air suction injection drive devices including various cargo chambers that reduce friction loss of the vertical all blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Using a combined engine injection section (78K), various air suction injection drive devices including various cargo chambers that increase the rotational output of a vertical all blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Using a combined engine injection section (78K), various air suction injection drive devices including various cargo chambers that reduce friction loss of a vertical all-blade turbine (8H) by rolling contact with high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Using a combined engine injection section (78K), various air suction injection drive devices including various cargo chambers that increase the rotational output of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Various energy storage cycles as various air suction injection drive devices including various cargo chambers using coalescence engine injection part (78K) and reducing friction loss of vertical all blade mercury turbine (8H) by rolling contact of mercury Combined organization.   Various energy storage cycles as various air suction injection drive equipment including various cargo chambers using coalescence engine injection part (78K) and reducing friction loss of vertical all blade mercury turbine (8H) by surface tension of mercury Combined organization.   Various types of air suction injection drive devices that use a combined engine injection section (78K) and include various vertical ascent and descent that reduce the friction loss of the vertical all blade mercury turbine (8H) by water repellent action (3G) Energy conservation cycle coalescence engine.   Various air suction injection drive devices that use a combined engine injection section (78K) and include various vertical ascent and descent to reduce the friction loss of a vertical all blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various air suction injection drive devices that use a combined engine injection section (78K) and include various vertical ascending and descending speeds that increase the rotational output of the vertical all blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various vertical ascending and descending using a combined engine injection part (78K) and reducing friction loss of a vertical all blade mercury turbine (8H) by rolling contact with high temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various vertical ascending and descending which use the combined engine injection part (78K) and increase the rotational output of the vertical all blade mercury turbine (8H) by rolling contact with high temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various energy storage as various air suction injection drive equipment including various vertical ascending and descending which uses the combined engine injection part (78K) and reduces the friction loss of vertical all blade mercury turbine (8H) by rolling contact of mercury Cycle coalescence engine.   Uses a combined engine injection section (78K) and saves various energy as various air suction injection drive equipment including various vertical ascending and descending which reduces friction loss of vertical turbine blade turbine (8H) by surface tension of mercury Cycle coalescence engine.   Various air suction injection drive devices including airfields everywhere in vertical ascending and descending using a combined engine injection part (78K) and reducing friction loss of vertical all blade mercury turbine (8H) by water repellent action (3G) Various energy conservation cycle coalescing engines.   Using a combined engine injection section (78K), various vertical ascending and descending various air suction injection drives including airfields that reduce friction loss of vertical turbine blade turbine turbine (8H) by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Using a combined engine injection section (78K), various vertical ascending / descending drivings including airfields that increase the rotational output of a vertical all-blade mercury turbine (8H) by surface tension of high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Using a combined engine injection section (78K), various vertical ascending / descending drives including airfields everywhere to reduce friction loss of vertical turbine blade turbine (8H) by rolling contact of high-temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Using a combined engine injection section (78K), various vertical ascending / descending drive to increase the rotational output of a vertical all blade mercury turbine (8H) by rolling contact with high temperature mercury (1d) Various energy storage cycle coalescing engines as equipment.   Using a combined engine injection unit (78K), various vertical ascending and descending devices that reduce the friction loss of a vertical all blade mercury turbine (8H) by rolling contact with mercury. Various energy conservation cycle coalescence engine.   Using a combined engine injection unit (78K), various vertical ascending and descending devices that reduce the friction loss of a vertical all-blade mercury turbine (8H) due to the surface tension of mercury. Various energy conservation cycle coalescence engine.   Various energy as a variety of air suction injection drive equipment including various space trips that use a combined engine injection part (78K) and reduce friction loss of a vertical all blade mercury turbine (8H) by water repellent action (3G) Conservation cycle coalescence organization.   Using a combined engine injection section (78K), various air suction injection drive devices including various space trips that reduce friction loss of a vertical all blade mercury turbine (8H) by surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Using a united engine injection section (78K), various air suction injection drive devices including various space trips that increase the rotational output of a vertical all blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various space trips that use a combined engine injection part (78K) to reduce friction loss of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various space trips that use a combined engine injection section (78K) to increase the rotational output of a vertical all-blade turbine (8H) by rolling contact with high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Various energy storage cycles as various air suction injection drive equipment including various space trips that use a combined engine injection part (78K) and reduce friction loss of vertical all blade mercury turbine (8H) by rolling contact of mercury Combined organization.   Various energy storage cycles as various air suction injection drive equipment including various space trips that use a combined engine injection part (78K) and reduce friction loss of vertical turbine blade turbine (8H) by surface tension of mercury Combined organization.   Various types of energy for various air suction injection drive devices including various asteroid landings that use a combined engine injection part (78K) and reduce friction loss of a vertical all blade mercury turbine (8H) by water repellent action (3AG) Conservation cycle coalescence organization.   Using a combined engine injection section (78K), various air suction injection drive devices including various asteroid landings that reduce the friction loss of the vertical all blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various asteroid landings that use a combined engine injection section (78K) to increase the rotational output of a vertical all blade mercury turbine (8H) by surface tension of high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various asteroid landings that use a combined engine injection part (78K) to reduce friction loss of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d) Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various asteroid landings that use a combined engine injection section (78K) to increase the rotational output of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d). Various energy conservation cycle coalescence engine.   Various energy storage cycles as various air suction injection drive equipment including various asteroid landings that use a combined engine injection part (78K) and reduce friction loss of a vertical all blade mercury turbine (8H) by rolling contact of mercury Combined organization.   Various energy storage cycles as various air suction injection drive equipment including various asteroid landings that use a combined engine injection part (78K) and reduce friction loss of vertical type moving blade mercury turbine (8H) by surface tension of mercury Combined organization.   Various air suction injection drive equipment including various lunar landing start that uses a combined engine injection part (78K) and reduces friction loss of a vertical all blade mercury turbine (8H) by water repellent action (3G) Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various lunar landing starts that use a coalescence engine injection part (78K) and reduce friction loss of vertical turbine blade turbine (8H) by surface tension of high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various air suction injection drive equipment including various lunar landing start that uses a combined engine injection part (78K) and increases the rotational output of a vertical all blade mercury turbine (8H) by surface tension of high temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various air suction injection drive devices including various lunar landing start that uses a combined engine injection part (78K) and reduces friction loss of vertical turbine blade turbine (8H) by rolling contact of high temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various air suction injection drive devices including various lunar landing starts that use a combined engine injection section (78K) and increase the rotational output of a vertical all blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d) Various energy conservation cycle coalescing engines.   Various energy for various air suction injection drive equipment including various lunar landing start that uses a combined engine injection part (78K) and reduces friction loss of vertical all blade mercury turbine (8H) by rolling contact of mercury Conservation cycle coalescence organization.   Various energies for various air suction injection drive equipment including various lunar landing start that uses a combined engine injection part (78K) and reduces friction loss of vertical turbine blade turbine (8H) by surface tension of mercury Conservation cycle coalescence organization.   Various air suction injection drive devices that use a combined engine injection unit (78K) and have various solar system escape speeds that reduce the friction loss of the vertical all blade mercury turbine (8H) by water repellent action (3G) Energy conservation cycle coalescence engine.   Various air suction injection drive devices including various solar system escape speeds that use a combined engine injection part (78K) and reduce friction loss of a vertical all blade mercury turbine (8H) by surface tension of high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various solar system escape speeds that use a combined engine injection section (78K) and increase the rotational output of the vertical all blade mercury turbine (8H) by the surface tension of high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various solar system escape speeds that use a combined engine injection part (78K) and reduce friction loss of a vertical all-blade mercury turbine (8H) by rolling contact with high-temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various air suction injection drive devices including various solar system escape speeds that use the combined engine injection section (78K) and increase the rotational output of the vertical all blade mercury turbine (8H) by rolling contact with low temperature mercury (1d); Various energy conservation cycle coalescence engine.   Various energy storage as various air suction injection drive equipment including various solar system escape speeds that use a combined engine injection part (78K) and reduce friction loss of vertical all blade mercury turbine (8H) by rolling contact of mercury Cycle coalescence engine.   Various energy storage as various air suction injection drive equipment including various solar system escape speeds that use coalescence engine injection part (78K) and reduce friction loss of vertical all blade mercury turbine (8H) by surface tension of mercury Cycle coalescence engine.   Various energy conservation cycle coalescence engine using water jet (78M).   Various energy storage cycle coalescing engines using a coalescing engine injection section (78K).   Various energy storage cycle coalescing engine using combustion gas rocket nozzle (6M).   Various energy storage cycle coalescence engine using combustion gas rocket nozzle (6M) combustor (1Y).   Combustion gas rocket nozzle (6M) combustor (1Y) various energy storage cycle coalescing engine using fuel injection pump (1D).   Combustion gas rocket nozzle (6M) Combustor (1Y) Fuel injection pump (1D) Various energy storage cycle combined engine using fuel control valve (25b).   Combustion gas rocket nozzle (6M) Combustor (1Y) Fuel injection pump (1D) Fuel control valve (25b) Various energy storage cycle coalescence engine using nozzle injection section (6d).   Combustion gas rocket nozzle (6M) Combustor (1Y) Combining engine with various energy storage cycles using combustion gas reservoir (95a).   Combustion gas rocket nozzle (6M) Combustor (1Y) Combustion gas reservoir (95a) Combining various energy storage cycle engines using combustion gas control valve (24).   Combustion gas rocket nozzle (6M) Combustor (1Y) Combustion gas reservoir (95a) Combustion gas control valve (24) Various energy storage cycle combined engine using fuel control valve (25b).   Combustion gas rocket nozzle (6M) Combustor (1Y) Fuel injection pump (1D) Various energy storage cycle combined engine using nozzle injection section (6a).   Combustion gas rocket nozzle (6M) Combustor (1Y) Combining engine with various energy storage cycles using combustion gas reservoir (95d).   Combustion gas rocket nozzle (6M) Combustor (1Y) Combustion gas reservoir (95d) Combustion engine with various energy storage cycles using combustion gas control valve (24).   Combustion gas rocket nozzle (6M) Combustor (1Y) Combustion gas reservoir (95d) Combustion gas control valve (24) Various energy storage cycle combined engine using fuel control valve (25b).   Combustion gas rocket nozzle (6M) Combustor (1Y) Fuel injection pump (1D) Various energy storage cycle combined engine using nozzle injection section (6d).   Various energy storage cycle coalescence engine using combustion gas injection rocket nozzle (6Y).   Various energy storage cycle coalescence engine using combustion gas injection rocket nozzle (6Y) combustor (1Y).   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Various energy storage cycle coalescing engine using combustion gas reservoir (95a).   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Various energy storage cycle combined engine using fuel injection pump (1D).   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) various energy storage cycle coalescing engines.   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Various energy storage cycles using superheated steam rocket nozzle (6L) Combined organization.   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Superheated steam rocket nozzle (6L) Combined engine outer casing ( 77F). Various energy conservation cycle coalescing engines.   Mercury injection pump (6Z) Various energy storage cycle coalescence engine using high temperature mercury (1d).   Mercury injection pump (6Z) Various energy storage cycle coalescing engines using high-temperature mercury (1d) as airplanes.   Mercury injection pump (6Z) Various energy storage cycle coalescing engines using high-temperature mercury (1d) as ships.   Mercury injection pump (6Z) Combined engine with various energy storage cycles using high temperature mercury (1d) as vehicles.   Mercury injection pump (6Z) Combining various energy conservation cycle engines using high-temperature mercury (1d) as combat aircraft.   Mercury injection pump (6Z) Combining various energy conservation cycle engines using high-temperature mercury (1d) as battle ships.   Mercury injection pump (6Z) High energy mercury (1d) combined with various energy conservation cycle engines for combat vehicles.   Mercury injection pump (6Z) Various energy storage cycle coalescing engines using high temperature mercury (1d) as various rotary output drive devices.   Mercury injection pump (6Z) High energy mercury (1d) and various energy storage cycle coalescing engines with various heat, electricity and cold supply facilities.   Mercury injection pump (6Z) Various energy storage cycle coalescing engines using various types of generators using high-temperature mercury (1d).   Mercury injection pump (6Z) High energy mercury (1d), various energy storage cycle coalescing engines with various types of propulsion output drive devices.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical energy blade mercury turbine (8H) combined with various energy storage cycle engines.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical type moving blade mercury turbine (8H) using various energy storage cycle coalescing engines.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical type moving blade mercury turbine (8H), and various energy conservation cycle coalescence engines made into ships.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical all-blade mercury turbine (8H) using various energy storage cycle coalescing engines.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical type moving blade mercury turbine (8H) using various energy conservation cycle coalescing engines as combat airplanes.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical-type all-blade mercury turbine (8H) and various energy conservation cycle coalescence engines made into battle ships.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical type moving blade mercury turbine (8H), combined with various energy conservation cycle engines as combat vehicles.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical-type all-blade turbine (8H) using various rotary output drive equipment and various energy storage cycle coalescence engines.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical-type all-blade mercury turbine (8H) using various heat, electricity and cold supply facilities, combined with various energy storage cycle engines.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical-type all-blade mercury turbine (8H) using various energy storage cycle coalescing engines as various generators.   Mercury injection pump (6Z) High-temperature mercury (1d) Vertical type moving blade mercury turbine (8H), and various energy storage cycle coalescing engines as various injection propulsion output drive devices.   Mercury injection pump (6Z) High-temperature mercury (1d) All-moving blade flywheel Mercury turbine (8E) Various energy conservation cycle coalescing engines.   Mercury injection pump (6Z) High-temperature mercury (1d) All-moving blade impeller Mercury turbine (8E) and various energy conservation cycle coalescing engines made into airplanes.   Mercury injection pump (6Z) High-temperature mercury (1d) All-moving blade impeller Mercury turbine (8E) and various energy conservation cycle coalescing engines made into ships.   Mercury injection pump (6Z) High-temperature mercury (1d) All-moving blade bouncing car Mercury turbine (8E), various energy storage cycle coalescing engines as vehicles.   Mercury injection pump (6Z) High-temperature mercury (1d) All-moving blade flywheel Mercury turbine (8E), combined with various types of energy conservation cycle engines as combat aircraft.   Mercury injection pump (6Z) High-temperature mercury (1d) All-moving-blade flywheel Mercury turbine (8E) and various energy conservation cycle coalescing engines made into battle ships.   Mercury injection pump (6Z) High-temperature mercury (1d) All-moving blade bouncing vehicle Mercury turbine (8E), combined with various energy conservation cycle engines as combat vehicles.   Mercury injection pump (6Z) High-temperature mercury (1d) All-wheel impeller flywheel Mercury turbine (8E) and various energy storage cycle coalescing engines as various rotary output drive devices.   Mercury injection pump (6Z) High-temperature mercury (1d) All-moving blade flywheel Mercury turbine (8E), combined with various energy storage cycle coalescence engines as various heat, electricity and cold supply facilities.   Mercury injection pump (6Z) High-temperature mercury (1d) All-wheel blade bouncing wheel Mercury turbine (8E) Various energy storage cycle coalescing engines made into various generators.   Mercury injection pump (6Z) High-temperature mercury (1d) All blade impeller Mercury turbine (8E) and various energy storage cycle coalescing engines as various injection propulsion output drive devices.   Combined engine combustion section (29X) Various energy storage cycle combined engine using high temperature mercury (1d).   Combined engine with various energy storage cycles using all blade combustion part (30X) high temperature mercury (1d).   Combined engine injection part (78K) High temperature mercury (1d) Various energy storage cycle combined engine using mercury injection pump (6Z).   Combined engine injection unit (78K) Various energy storage cycle combined engine using high temperature mercury (1d).   Various energy storage cycle coalescence engine using water jet (78M) high temperature mercury (1d).   Various energy storage cycle coalescence engine using water jet (78M) high temperature mercury (1d) mercury injection pump (6Z).   Various energy storage cycle coalescing engine using combustion gas rocket nozzle (6M).   Various energy storage cycle coalescence engine using combustion gas rocket nozzle (6M) combustor (1Y).   Various energy conservation cycle coalescence engine using combustor (1Y).   Various energy conservation cycle coalescence engine using high temperature mercury (1d).   Various energy conservation cycle coalescence engine using mercury injection pump (6Z).   Various energy storage cycle coalescence engine using fuel (1b).   Various energy conservation cycle coalescence engine using water repellent action (3G).   Various energy storage cycle coalescing engine using fuel control valve (25b).   Various energy storage cycle coalescence engine using mercury control valve (25d).   Various energy storage cycle coalescence engine using one-way air flow path (9).   Various energy storage cycle coalescence engine using fuel reservoir (95B).   Various energy conservation cycle coalescence engine using mercury reservoir (95D).   Various energy storage cycle coalescing engines using a reduced diameter compression chamber mercury heat exchanger (2Z).   Various energy storage cycle coalescing engines using a cold recovery unit (103b).   Various energy storage cycle coalescing engine using combustion gas injection rocket nozzle (6Y) and superheated steam rocket nozzle (6L).   Various energy storage cycle coalescence engine using combustion gas rocket nozzle (6M) combustor (1Y).   Combustion gas rocket nozzle (6M) Combustor (1Y) Fuel (1b) Various energy storage cycle coalescence engine using air (28a).   Various energy storage cycle coalescing engines that use combustion gas rocket nozzles (6M) as various rotational output drive devices.   Various energy storage cycle coalescing engines that use combustion gas injection rocket nozzles (6Y) as various air suction injection drive devices.   Various energy storage cycle coalescing engines using combustion gas injection rocket nozzles (6Y) as various water suction injection drive devices.   Various energy storage cycle coalescing engines that use superheated steam rocket nozzles (6L) as various rotational output drive devices.   Various energy storage cycle coalescing engines using various superheated steam rocket nozzles (6L) as various air suction / injection drive devices.   Various energy storage cycle coalescing engines that use superheated steam rocket nozzles (6L) as various water suction jet drive devices.   Combustion gas rocket nozzle (6M) Various energy storage cycle coalescence engine that injects combustion gas (49) high temperature mercury (1d) from mercury injection pump (6Z).   Combustion gas rocket nozzle (6M) Various energy storage cycle coalescence engines that inject combustion gas (49) high-temperature mercury (1d) from a mercury injection pump (6Z) to bring the exhaust temperature of the combustion gas close to 0 degrees.   Combustion gas rocket nozzle (6M) Combustion gas (49) High temperature mercury (1d) is injected from mercury injection pump (6Z) to bring combustion gas exhaust temperature close to absolute 0 degree and high temperature mercury exhaust saturation temperature around 230 degrees. Various energy conservation cycle coalescence engine.   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Superheated steam rocket nozzle (6L) Combined engine outer casing ( 77F). Various energy conservation cycle coalescing engines.   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Superheated steam rocket nozzle (6L) Combined engine outer casing ( 77F) Various energy storage cycle coalescing engines using a coalescing engine injection section (78K).   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Superheated steam rocket nozzle (6L) Combined engine outer casing ( 77F) Various energy storage cycle coalescing engines in which the coalesced engine injection unit outer box is rotatable using the coalesced engine injection unit (78K).   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Superheated steam rocket nozzle (6L) Combined engine outer casing ( 77F) Various energy storage cycle coalescing engines in which a plurality of coalescing engine injection parts (78K) are used and a plurality of coalescing engine injection part outer boxes can be rotated within 200 degrees.   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Superheated steam rocket nozzle (6L) Combined engine outer casing ( 77F) Various energy storage cycle coalescing engines that use a plurality of coalescing engine injection units (78K) to allow a plurality of coalescing engine injection unit outer boxes to be appropriately rotated.   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Superheated steam rocket nozzle (6L) Water jet outer box (77D) Various energy conservation cycle coalescence engine using   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Superheated steam rocket nozzle (6L) Water jet outer box (77D) Various energy conservation cycle coalescence engine using water jet (78M).   Combustion gas injection rocket nozzle (6Y) Combustor (1Y) Combustion gas reservoir (95a) Fuel reservoir (95B) Fuel injection pump (1D) Superheated steam reservoir (95C) Superheated steam rocket nozzle (6L) Water jet outer box (77D) Various energy conservation cycle coalescence engine using multiple water jets (78M).   Various energy storage cycle coalescence engine that injects superheated steam (50) from superheated steam rocket nozzle (6L).   Various energy storage cycle coalescence engines that heat the superheated steam (50) by providing an annular superheated steam reservoir (95c) on the outer periphery of the combustor (1Y) before injecting the superheated steam (50) from the superheated steam rocket nozzle (6L).   Combined with various energy storage cycles to heat and inject superheated steam (50) at high temperature by providing an annular superheated steam reservoir (95c) around the combustor (1Y) before injecting superheated steam (50) from the superheated steam rocket nozzle (6L) organ.   Before injecting superheated steam (50) from the superheated steam rocket nozzle (6L), a superheated steam reservoir (95c) is provided in an annular shape around the combustor (1Y) to heat and inject the superheated steam (50) at a high temperature and the combustor (1Y) ) Is a high-temperature combustion high-temperature injection combined with various energy conservation cycle.   Before injecting superheated steam (50) from the superheated steam rocket nozzle (6L), a superheated steam reservoir (95c) is provided in an annular shape around the combustor (1Y) to heat and inject the superheated steam (50) at a high temperature and the combustor (1Y) ) Combustion engine of various energy conservation cycle to increase the combustion quantity of high temperature combustion high temperature injection.   Before injecting superheated steam (50) from the superheated steam rocket nozzle (6L), a superheated steam reservoir (95c) is provided in an annular shape around the combustor (1Y) to heat and inject the superheated steam (50) at a high temperature and the combustor (1Y) ) Combustion engine of various energy conservation cycle that increases both injection propulsion power by high temperature combustion high temperature injection.   Reduced-diameter compression chamber mercury heat exchanger (2Z) Various energy storage cycle coalesced engines that perform high-pressure combustion heat exchange cooling combustion without limitation in the reduced-diameter main combustion chamber / heat exchanger (1).   Reduced-diameter compression chamber mercury heat exchanger (2Z) Reduced-size main combustion chamber and heat exchanger (1) Infinitely high-pressure combustion heat exchange Cooling combustion and various energy to be divided and used for combustion gas heat output + combustion gas mass output Conservation cycle coalescence organization.   Reduced diameter compression chamber mercury heat exchanger (2Z) Reduced diameter main combustion chamber and heat exchanger (1) Unlimited high pressure combustion heat exchange cooling combustion, superheated steam (50) explosive power and high temperature mercury (1d) explosive power + Combustion gas (49) Various energy storage cycle coalescing engines that are used for mass storage in divided explosions.   Reduced diameter compression chamber mercury heat exchanger (2Z) Reduced diameter main combustion chamber and heat exchanger (1) unlimited high pressure combustion heat exchange cooling combustion and around 400 degrees 24-400 MPa superheated steam (50) explosive power and 600- 800 degree saturation pressure abnormal high temperature mercury (1d) + 40 degree or more 24-300MPa combustion gas (49) Various energy preservation cycle coalescence engine which is divided and used for mass explosive force.   Various energy storage cycle coalescence engine equipped with a cold heat recovery device (103) to recover cold heat.   Various energy storage cycle coalescence engine equipped with a cold energy recovery device (103) and recovering cold energy with alcohol (1C).   Various energy storage cycle coalescing engines equipped with a cold heat recovery device (103), which collects and stores cold heat with alcohol (1C) and uses it for heat exchange with materials suitable for the application.   Various energy conservation cycle coalescence engines that replace the vertical all-blade mercury turbine (8H) with a full-blade flywheel mercury turbine (8E).   Various energy storage cycle coalescence engines that replace the vertical all-blade mercury turbine (8H) all-blade combustion section (30X) with an all-blade flywheel mercury turbine (8E) coalescence engine combustion section (29X).   All-blade flywheel mercury turbine (8E) combined engine combustion section (29X) combined engine injection section (78K) instead of vertical all blade mercury turbine (8H) all blade combustion section (30X) combined engine injection section (78K) ) Various energy conservation cycle coalescing engines.   Various types of all-blade impeller mercury turbine (8E) combined engine combustion section (29X) water jet (78M) instead of vertical all-blade mercury turbine (8H) all-blade combustion section (30X) water jet (78M) Energy conservation cycle coalescence engine.   Various energy storage cycle coalescing engines equipped with a vertical all blade mercury turbine (8H) and a vertical all blade gas turbine (8A) on one shaft.   Crankshaft (16) Combined with various energy storage cycle engines that are bent 90 degrees.   Various energy storage cycle coalescing engines that are driven by synchronizing and meshing all blade impeller mercury turbines (8E) and (8E) and extending them vertically and vertically in multiple stages.   Various energy storage cycle coalescence engines that synchronize and mesh all blade impeller gas turbines (8a) and (8a) and drive them in multiple vertical stages.   Various energy storage cycle coalescing engines that drive all-blade impeller mercury turbine (8E) by vertically extending multiple multi-stages by providing injection walls that enable vertical mercury injection.   Various energy storage cycle coalescing engines that drive all-blade impeller gas turbine (8a) by vertically providing multiple injection stages and driving in multiple vertical stages.