JP2011169217A - Various energy conservation cycle combined engine - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To solve the problem that an existing steam turbine has power which is 1/36,000 or small of platinum ball power, brings stagnation output close to 0 by a half of a stationary blade and exposes humanity to a risk of extinction through the rise of seawater temperature by 7°C. <P>SOLUTION: In a various energy conservation cycle combined engine, for instance, by taking all moving blade gravity large substance gravity solar heat turbine drive, the maximum atmospheric constant-speed, constant-volume power is set to be almost 36,000 time platinum sphere power of an existing steam turbine. Air heated by sunlight is compressed to be high temperature with one and more stage heat pump so that individual air respectively heated by solar light is recovered through heating and compression thereof so as to be dividedly reserved and utilized in the increase of cold mass + limitlessly high pressure heat 50+ cold 28a. The extinction of humanity is prevented by the speedup of a natural phenomenon, the substantial increase of human food and prevention of the rise of seawater temperature by 7°C in the process of driving a generator and ship. When driving a solar thermal gravitational rotation aircraft, fuel injection combustion ultra-high pressure rocket injection is applied to heat + cool from the vicinity of the maximum flying altitude of existing aircraft. Cost of reaching space is minimized by aiming at no fuel cost flight in the atmosphere or the like. A same day trip to anywhere on Earth, travel in outer space or the like are fully achieved through the heyday of space flight. <P>COPYRIGHT: (C)2011,JPO&INPIT

Description

In the present invention, the existing best steam turbine power generation has the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / sec. Work is equipped with half static blades alternately with moving blades, the rotational output approaches 0, the seawater temperature rises by 7 degrees with all the generated heat, the sea surface rises in temperature, and natural phenomena become impossible. There is a great risk of approaching the extinction of mankind in around 100 years, and as a technology to prevent the extinction of mankind, all-turbine turbine 8G essential ratio gravity material gravity turbine 8G is essential, and the atmospheric pressure, the same speed, and the same volumetric power are used. As the total moving blade ratio critical material gravity solar thermal turbine 8G power generation close to the 36,000 times platinum ball power of 1, the 1st stage heat pump 1G is used to heat the solar heating air to a high compression temperature and the 1st stage compression heat recovery unit 2C Air heat exchanger 2X Heat recovery with separate sunlight 28a of sunlight heating, challenge the infinite increase of the cold 28a mass including 2 to multiple stages, compress multiple times with 2 to 2 stage heat pump 1G, 2 to 2 stage compression heat recovery unit 2C Similarly to the first stage multiple times, the water heat exchanger 2Y and the specific material heat exchanger 2Z also collect heat according to the application and store it in an unlimited amount of high-pressure superheated steam 50 heat + compressed air 28a cold heat for various applications. As the various energy conservation cycles to be used, all the blade ratio critical material gravity solar heat turbine 8G power generation and ship driving process speeds up natural phenomena, supplying nitrogen, oxygen, CO2 etc. to seawater with cold and nutrients, The present invention relates to various energy conservation cycle coalescence engine technologies that greatly increase food to generate seawater temperature rise 0 CO2 exhaust 0 power generation and the like to prevent human extinction.

  The existing jet gas turbine is almost the same as the steam turbine in order to make the rotation output and injection pressure close to 0 and the injection propulsion output to be small, making it impossible to make space flight capable of making 16 orbits of the earth on the air resistance 01 day. In the same way as the specific material gravity solar thermal power generation, all blades specific material gravity thermal turbine 8G + all blades specific material gravity cooling turbine 8G drive, and many power generation by turbine output close to 3.6 times power As a machine drive and heat pump drive, it is divided and stored as many high-temperature and large-mass heat 50 + cold heat 28a by a large number of 1 to multi-stage heat pumps 1G heat production, supplied to the combined engine injection unit 78, and fuel injection ignition to the cold heat 28a Combustion, heat the heat 50 at the outer periphery and the inner periphery infinitely as a high-pressure and high-speed combustion flow, approach the heat 50 approaching the atmospheric pressure 100 degrees multiple times to 1200 degrees, The injection pressure is 24MPa (existing steam turbine pressure) and the infinitely high pressure, and it is a combined engine injection unit 78 capable of injecting 10 to 100 times the pressure of the existing jet 100 to 200 times pressure. 16 round trips and other trips anywhere on the earth are possible, aiming at 1000 times the jet propulsion output and rotation output, and propulsion propulsion with the rotation output approaching 36,000 times work rate when flying in the atmosphere The present invention relates to various energy storage cycle coalescing engine technologies that make various types of airplanes aiming at zero CO2 emissions.

  Existing ships use steam turbines, gas turbines, and even lower performance engines, and have little rotational output and injection propulsion output, and consume a huge amount of fuel for low-speed movement. , All blade ratio critical material gravity thermal turbine 8G + all blade ratio critical material gravity cooling / heating turbine 8G drive, many generator drive and 1-stage heat pump 1G drive by turbine output approaching 3.6 times power Or a large number of electric drives 1 to a multistage heat pump 1G by heat production, divided and stored indefinitely high-pressure heat 50 + cold heat 28a, supplied to the water jet 79 and burned to the cold heat 28a (oxidant) by fuel injection ignition combustion , Heat the superheated steam 50 at the outer circumference and inner circumference to an unlimited high pressure and high speed combustion flow, bring the superheated steam approaching the atmospheric pressure of 100 degrees closer to 1200 degrees several times, and set the injection pressure to 2 The water jet 79 is capable of 100-200 times the pressure of existing jets and 10 times the calorific value of the existing jet, and the jet propulsion output and the rotational output are targeted 1000 times, and 3.6 at the time of screw propulsion. The present invention relates to technologies for various energy storage cycle coalescing engines that are driven by a screw with a rotational output approaching 10,000 times the work rate, and in the case of a screw drive, various ships aiming for zero CO2 emissions.

  Considering the elementary school science without brainwashing, the existing best steam turbine power generation at the same atmospheric pressure and same volumetric power kg kg m / sec is slightly less than 1 / 36,000 of the platinum ball gravity turbine 8G power, Stops the steam speed and has half the workless blades alternately with the moving blades, bringing the rotational output close to 0, raising the seawater temperature by 7 degrees with all the generated heat, making the whole sea surface temperature rise impossible, Increasing extreme weather without an upper limit The danger of human beings approaching extinction is increasing around 100 years. The green earth is a miracle product and there is a great risk of approaching other stars. According to the explanation of the power station, if the rise in seawater temperature is 7 degrees or less, there is no influence on the environment, but for example, 7 degrees in the sea area where the seawater temperature is 30 degrees If it rises, the typhoon wind speed will be 300m / second, etc., and there is a danger that mankind will be extinct due to heavy rain of seawater. If China continues to grow 10%, the increase in seawater temperature will be doubled in 10 years to 4 in 20 years The speed of typhoons and seasonal winds is 100m / sec in the worst prediction, and there is a concern that Japanese agriculture and forestry will be destroyed due to heavy rain of suctioned seawater over the seawater. It is necessary to develop technology that meets the worst expectations.

  Considering the elementary school science without brainwashing, the existing best steam turbine power generation at the same atmospheric pressure and same volumetric power kg kg m / sec is slightly less than 1 / 36,000 of the platinum ball gravity turbine 8G power, The work is equipped with half static blades alternately with moving blades, and the rotational output is approaching zero. However, in high schools and universities, the existing engine is explained as the best engine, and when you return to elementary school science without brainwashing and think about the best engine, the unit of work is heavy because the weight unit is kg weight m / second equal weight x speed. There is a background that there is no trace that thought that the rotation output generation with the material at high speed is the theoretical best engine. Therefore, for example, if a full-blade mercury gravity solar turbine 8G drive generator, airplanes and ships are used in a facility for supplying heat, electricity and cold while the airplane ship is stopped, brainwashing has prevented the invention for a long period of time. In the course of this process, the fuel cost will approach zero or zero, and the operating profit rate will be enormous, such as 10 times the existing operating profit ratio. There is a background that can be done.

The atmospheric pressure, the same speed, the same volumetric power, kg weight m / second, and a mercury work rate of 23,000 times that of the existing steam turbine power generation, such as liquid metals such as mercury and liquid lead, metal balls, and coated metal balls Accelerating gravity acceleration vertically downward significantly increases output generation even with acceleration of gravitational acceleration alone rather than an input that increases the head at low speed, increasing the number of turbines + increasing the head to 1000 m or more and increasing the output without limit. There is a background. The maximum acceleration on the earth is almost infinite in gravitational acceleration, and the theoretical best engine gravity solar power generation with 0 seawater temperature rise, 0 CO2 exhaust and 0 fuel cost, etc., and the heat pump 1G is the most efficient with the heat and geothermal heat of the earth Various types of automobiles that are used frequently and have a limited amount of resources such as fossil fuels, recovering and using heat and cold, and generating power near infinity or near the infinity, using batteries or electric drives such as gravity solar power generation There is a background in which extremely inexpensive power storage battery drive and electric drive prevention of global warming can be obtained, such as prime, various kinds of ships, full-scale electrified housing, and factory electrification.

Japanese Patent No. 1607151, Patent No. 1609617, Patent No. 1645350, Patent No. 1924889, Patent No. 1912522, Patent No. 1959305, Patent No. 1986119, Patent No. 2646636, 1992 U.S. Pat. No. 5,133,305, 1993 U.S. Pat. US Pat. No. 5,429,078, 1997 US Pat. No. 5,701,864, PCT International Application No. PCT / JP97 / 01814, US Pat. No. 6,119,650, Chinese Patent No. 8818, EU British Patent No. 902175, PCT International Application No. PCT / JP97 / 02250 No. 6,263,664.

There are 326 applications for PCT international application priority claim applications, such as Japanese Patent Application No. 2009-048869, application date March 3, 2009 to Japanese Patent Application No. 2010-007805, application date January 18, 2010 .

  At existing thermal power plants in the world, the seawater temperature is increased by 7 degrees Celsius with the total amount of heat generated, and the sea area is increased 1000 times in 100 years. Increased torrential rain, etc. without limit, and by covering the land with salt cover due to heavy rains of seawater, etc., the land food of mankind has been reduced as much as possible, and the natural phenomenon of supplying nutrients to the sea surface cooling seabed in winter is not allowed As possible, phytoplankton, seaweeds, corals, etc. will be drastically reduced, fish will be drastically reduced to 1/100, etc. by the food chain. Increasingly, for example, typhoons and seasonal winds are becoming huge in abnormal weather with no upper limit such as 300 m / sec, and there is a problem of delaying human extinction by preventing global warming in order to increase the danger of human extinction.

Heat production 1 to multiple stage heat pump 1G is driven by all-blade specific material gravity turbine 8G direct drive or generator 1 electricity, and infinitely high pressure heat (superheated steam heat) and cold heat (compressed air mass) , Fuel cost 0 CO2 Exhaust 0, infinite production, thermal + cold driven gravity solar power generation, gravity solar thermal ship, gravity solar thermal airplane, power generation and ship sucking CO2 together with the atmosphere Supply nutrients such as cold oxygen, nitrogen and CO2 to the ocean floor and the sea, increase phytoplankton, seaweeds, corals and fish, etc., and increase human food. 16 times around the earth, day trips anywhere on the earth, and CO2 exhaust 0 flight aim in the atmosphere, etc., limited oil resources etc. are used to the minimum necessary, and to leave offspring and global warming To prevent droughts, torrential rains, typhoons and seasonal winds from becoming enormous, and to produce 10 times the amount of electricity generated in the existing world, to produce a variety of gravity solar thermal power, Electricity driven vehicles, full electrified housing prime, factory electrification prime, warm and cold use prime, generating seawater temperature 0, CO2 exhaust 0 and fuel cost 0, preventing global warming and extinction of mankind Postpone.

When the gravity turbine 8G drive is used for all rotor blade ratio material, the effect of using an infinite head is great, and when generating power with the atmospheric pressure, the same speed and the same volumetric power approaching 36,000 times those of the existing steam turbine power generation. The effect of increasing power generation is great. Driven by all-blade ratio critical material gravity thermal turbine 8G + all-blade ratio critical material gravity cooling / heating turbine 8G, the power generation rate, flight speed, and ship speed are increased by approaching 36,000 times the power when the head is limited. The effect of leaving the resources to the offspring is great because the fuel consumption can be reduced to 0 or a little, and various gravity power generation, various gravitational solar thermal ships and various gravitational solar thermal airplanes drive CO2 with the atmosphere and various gravitational turbines, respectively. Turbine drive and generator 1 Power drive Compressed heat recovery multiple times with 1 to multiple-stage heat pump 1G, divided into ultrahigh pressure heat + cold heat, used for generator 1, screw 7C, propeller 7A and rotation Since the blades 7B drive various gravity turbines to drive the water jet 79 and the coalesced engine injection unit 78 with hot 50 + cold 28a, the same fuel amount is rotated 100 to 1000 times. And the injection promote the output aim, there is an aim effect a 10-speed level, and the like of an existing ship, an airplane at 100 times the amount of power generation and fuel costs insignificant in fuel costs 0.

In the case of power generation or ships with seawater temperature rise 0 or CO2 exhaust 0, a huge amount of CO2 is inhaled together with the atmosphere, and all of it is supplied as nutrients such as nitrogen, oxygen, and CO2 in the cold 28a to the seabed and sea, and is a natural phenomenon Speedup 2a Increases the food of underwater microorganisms, greatly increases the digestive capacity of nutrients such as CO2 of underwater microorganisms to tens of thousands of airborne microorganisms and forests, proliferates phytoplankton, seaweeds and corals, Proliferate fish in the food chain, increase human food, and have the effect of delaying human extinction.

Various gravitational solar thermal airplanes have the effect of aiming for space utilization with the same fuel amount of 100 to 1000 times rotation output and injection propulsion output. For example, the injection propulsion output is 100 times the pressure of existing jets, 10 times the calorific value, and 1000 times the time of propulsion. The target for output is propeller flight with zero fuel amount in the atmosphere, rotor blade flight, and jet propulsion aim. Since the superheated steam expansion speed is the maximum in vacuum, the existing space rocket ground mass injection is considered the worst, near the highest flight altitude of the existing aircraft It has the effect of propelling higher power rockets, reducing the fuel cost for reaching space to 1/100 or less, aiming to make the best use of space in various ships and airplanes in the existing world, and leaving resources to descendants.

Explanatory drawing of gravity blade 8G for all blade ratio material (Example 1) Explanatory drawing of gravity blade thermal turbine 8G for all blade ratio material (Example 2) Explanatory drawing of gravity moving / cooling turbine 8G for all blade ratio material (Example 3) Explanatory drawing of the solar heater 2 (Example 4) Explanatory drawing of screw ship 39D (Example 5) Explanatory drawing of water suction 79X screw ship 39D (Example 6) Explanatory drawing of water suction 79X ship 38C (Example 7) Explanatory drawing of air suction 79Z ship 38B (Example 8) Explanatory drawing of air suction 79Z screw ship 39E (Example 9) Explanatory drawing of union engine injection part 78B solar gravity airplane 39A (Example 10) Combined engine injection unit 78B solar gravity rotating airplane 39B explanatory diagram (Example 11) Explanatory drawing of water jet 79U (Example 12) Explanatory drawing of water jet 79X (Example 13) Explanatory drawing of water jet 79S (Example 14) Explanatory drawing of water jet 79T (Example 15) Explanatory drawing of water jet 79Y (Example 16) Explanatory drawing of water jet 79Z (Example 17) Explanatory drawing of the union engine injection part 78W (Example 18) Explanatory drawing of the union engine injection part 78V (Example 19) Explanatory drawing of the union engine injection part 78A (Example 20) Explanatory drawing of the union engine injection part 78B (Example 21)

  The previous application was for the purpose of inventing the next theoretical best engine, so it was best to understand only by yourself and impossible to understand by a third party. We will challenge the realization of possible inventions. The existing engine was brainwashed and the invention was blocked for a long time. For example, the current best steam turbine power generation at the same pressure and volumetric capacity kg kg m / sec was reduced to 1 / 36,000 of the platinum ball power, The blades are placed alternately with the moving blades and weired to bring the rotational output close to 0, increasing the seawater temperature by 7 degrees with all the heat generated by the steam turbine power generation, and increasing the typhoon and seasonal wind updraft around Japan around 20 years Then, there is a danger that the extinction of mankind will approach in about 100 years, such as a heavy rain of suction seawater is expected over the sea. That is, since the invention becomes too large due to many fatal defects of the existing technology, a part of the invention is described in the explanation of the reference numerals, and the part described repeatedly in the previous application is omitted. The three types are horizontal axis turbines that are close to existing turbines and easy to understand, so we will try to materialize the invention as an explanation of the omitted examples.

In the gravity turbine 8G power generation of the all-blade specific material gravity turbine of FIG. 1, all four blade turbines are the same except for the difference in shape, such as gravity use and heat pump drive. Of the three types of thermal acceleration / cooling acceleration / vacuum acceleration, the all-blade specific gravity gravity turbine 8G, which uses specific gravity gravity acceleration, is used in the turbine outer box 77a with a head drop of 1 to 120 stages and unlimited use. The turbine blade angle is strong against impact and the optimum speed of the critical material 2E is used. When using a metal sphere, the impact is reduced by using an ultra-small sphere to protect the turbine blade, and the coating of elastic elastic material such as silicon-coated ultra-small sphere is applied. Protects the turbine blades, and the turbine blades are coated with cemented carbide to prevent the turbine blades from wearing, and the specific material 2E is raised and stored at the top by the specific material riser 2F. Material 2E is injected by specific material accelerator 6W, gravity acceleration part 1g gravity core acceleration vacuum acceleration to optimum speed, driving all blade ratio material gravity turbine 8G, horizontal axis 1h is provided at the turbine joint By rotating the rotation direction alternately, the generator 1 and many 1-stage heat pumps 1G not shown in the figure are driven outside the turbine outer casing 77a, and the rotation of the inner blade group 60C of the outer blade group 60D having a diameter of 1 to 12 times larger is rotated. The direction is alternately changed in the counter rotating device 84 or the rotating direction is alternately switched by the counter rotating gear device 84Y, thereby generating power with negligible vibration and noise.

Electricity demand and heat demand are almost infinite, and generator 1 and 1 to 1 stage multi-stage heat pump 1G drive are essential, and all blade ratio critical material gravity turbine 8G horizontal axis 1h drive and horizontal axis 1h drive generator power drive 1 The air is sucked and compressed at about 20 to 100 degrees by the stage heat pump 1G, and the other atmosphere 28a is heated by the first stage compression heat recovery unit 2C air heat exchanger 2X, and heated at about 20 to 100 degrees by the first stage heat pump 1G. Heat production that repeats heat recovery at 100 to 500 degrees, etc., in the compressed air, or compression that heats the separate air 28a in the 2 to multi-stage compression heat recovery unit 2C air heat exchanger 2X and compresses it with the single-stage heat pump 1G Challenge to increase the mass of air-cooled heat 28a, 2 to multi-stage compression heat recovery unit 2C2 to multi-stage heat pump 1G selective use, challenge to high pressure ultra-high pressure cold heat 28a without any limitation of multiple-time compression multiple-time heat recovery, 200 24-400 MPa compressed air before and after degrees 8a cold + 400 degrees around 24 to 400MPa Superheated steam 50 divided heat and use, for example, injecting heat 50 into methane hydrate, recovering and using methane, kitchen revolution to drive rice cookers and washing dryers with heat 50, heating Use heating 50 or cooling 28a for air conditioning or cooling, etc. Heating and cooling revolutions for endless applications such as greenhouse cultivation and ice production.

The inner rotor blade group 60C and outer rotor blade group 60D can be fully automated as much as possible, and can be assembled into a fitting bolt assembly with the same diameter and the same shape for each stage to enable a multistage rotor blade group and a multistage turbine, A large-diameter portion that supports large weight and an additional hydraulic floating part 80a, and a gravity acceleration unit 1g that accelerates the bearing 80 and specific material are provided, and the generator 1 is driven by the joint of the gravity acceleration unit 1g. The generator 1 is driven out of the turbine outer box 77a, and the all blades specific gravity material gravity turbine 8G is driven by the specific material acceleration 6W acceleration and gravity vacuum acceleration. The gravity acceleration unit 1g makes the optimum speed, the multi-generator power generation and the low-speed rotation power generation close to 36,000 times the existing steam turbine power generation, and the existing turbine 1 to 26 times the cross section of the wing cross section 4 In order to generate the rolling contact rotation output of the specific critical substance 2E, in the exhaust process, the vacuum driven turbine exhaust can be cooled by the air extractor 51 so that it can be subjected to high-temperature cooling, etc. Combines various energy conservation cycle coalescence engines that are the world's most profitable by generating electricity with rising CO2 emissions, 0 fuel costs, and preventing global warming.

  In the case of 8G power generation of all-blade specific material gravity solar thermal turbine 8G in Fig. 2, the explanation is given in the four types of all-blade turbine 8G internal turbine 8G solar thermal utilization (geothermal utilization is also the same), thermal acceleration, cold acceleration, vacuum acceleration Among the three types, the specific critical material gravity thermal acceleration acceleration use, the all blades specific gravity material gravity thermal turbine 8G is installed in 1 to 10 stages vertically in the turbine outer box 77a, and the number of units suitable for the application is used. Ascending apparatus 2F raises and stores a specific critical substance at the top, and FIG. 4 sunlight heater 2 or deformation causes intake air 28a to be heated by sunlight, long lens 2d and heat absorbing material 2B, The horizontal axis 1h drive generator power drive, the first stage heat pump 1G makes the suction compression around 800 degrees, and the first stage compression heat recovery unit 2C air heat exchanger 2X heats the solar-heated air 28a to 500 degrees 1 stage heat po Compressive heat recovery to high pressure refrigeration 28a at 1200 ° C, etc., to produce an infinite increase in the amount of cold recovered, 2 to 2 stage compression heat recovery unit 2C2 to multiple stage heat pump 1G selection use, multiple compression and multiple heat The high-pressure ultra-high-pressure cold 28a is produced without limitation, and is divided and stored into 24-200MPa compressed air 28a cold around 200 degrees + 24-400MPa superheated steam 50-heated around 400 degrees. Injected and accelerated with warm heat 50, with the gravitational acceleration unit 1g to the optimum speed of gravity core acceleration, a horizontal axis 1h is provided between the turbines, and a generator 1 and a number of heat pumps 1G not shown outside the turbine outer box 77a Is driven, and the rotation direction of the 1 to 12 times diameter turbine blades is alternated to generate power generation with negligible vibration and noise.

Since all the blade specific material gravity solar thermal turbine 8G uses the specific material 2E, the turbine blade angle is set to the angle that is strong against impact and the specific material 2E optimum speed is used. Use of coated elastic steel balls made of isoelastic elastic material, etc. to prevent wear of turbine blades mirrored with coated cemented carbide, etc., 1 to multi-stage compression heat recovery unit 2C, water heat exchanger 2Y and air heat exchange respectively 2X and specific material heat exchanger 2Z are driven and solar heat is used as a seed, and 1 to multi-stage heat pump 1G and 1 to multi-stage compressed heat recovery unit 2C are used to generate a near-infinite temperature 50 (compressed air heat quantity). The superheated steam 50) and the cold 28a (compressed air mass) are divided and stored, the superheated steam 50 is accelerated, and the total moving blade ratio material gravity solar thermal turbine 8G is driven. In the process of exhausting the thermal turbine 8G, Mixer 2 As a result, the low temperature seawater in the deep sea is sucked in as much as possible, the cold heat recovery unit 103 of the cooling turbine 8G exhaust cools the seawater by the cold air mixing after the cold recovery, and the natural phenomenon speed-up device 2a circulates to supply the seabed. Mixing and dissolving nitrogen, oxygen, CO2, etc. of the cold heat 28a to the natural turbine speeding up 2a, the hot turbine 8G exhaust heat 50 is cooled to condensate and superheated by the condensate pump 1F and the water heat exchanger 2Y. Steam 50 is used to increase the digestive capacity of nutrients such as CO2 supplied to marine microorganisms tens of thousands times that of forests, thereby preventing global warming.

Supplying nutrients such as nitrogen, oxygen and CO2 to seawater Accelerates natural phenomena, proliferates phytoplankton, seaweeds and corals, etc. Increases human food such as fish in the food chain etc. The cooling turbine 8G is driven by the specific critical material 2E whose driving temperature has been raised and the thermal turbine 8G is driven in a vacuum, and the specific critical material is cooled to lower the cooling temperature, and the thermal turbine is circulated to increase the driving temperature. The blade group 60D is provided with an additional thrust bearing 80a for hydraulic levitation to support a large weight, and can be fully automatic processed as much as possible by making fitting bolts assembling bolts with the same diameter and approximately the same shape for each stage, enabling a multistage blade group and a multistage turbine. At the same time, fully automatic machining and assembly are facilitated, and the gravity acceleration part 1g joint for accelerating specific substances is provided with a horizontal shaft 1h through-hole for driving the generator 1, so that the generator 1 and heat pump 1G Is driven outside the turbine outer box 77a, and the specific turbine gravity turbine 8G, which is close to 36,000 times that of the existing steam turbine power generation, has the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / sec. 2 to 26 times the blade cross-sectional area increased surface area of the turbine blade 4X is injected into the turbine blade cross-section 4X, and the gravity and solar heat is utilized to the maximum by generating the rolling contact rotation output of the specific material 2E. A combined energy storage cycle engine that recovers heat, manufactures and stores cold + warm heat, and uses it for various applications such as power generation, ship drive and airplane drive.

Similarly, the all-blade ratio critical material gravity solar cooling / cooling turbine 8G in FIG. 3 is also used to prevent the wear of turbine blades such as coated cemented carbide, and is installed vertically in multiple stages to increase the temperature by driving the thermal turbine. The specific critical material 2E is stored in the uppermost position by the specific critical material raising device 2F, injected by the specific critical material accelerator 6W, accelerated by the compressed air 28a, the cold acceleration gravity acceleration unit 1G, and the core ratio of all blades The material gravity refrigeration turbine 8G is driven by rolling contact with the optimum speed of the specific critical material 2E, and the compressed air 28a approaching absolute 0 degree is heated in the driving process with the specific critical material whose temperature is increased, and the volume speed of the compressed air 28a is increased. Then, the turbine output is increased to cool the specific critical material, the thermal turbine 8G is driven by the cooled specific critical material, and the cooling is performed by the cool recovery unit 103 in the exhaust process as a circulation to raise the specific critical material temperature. Used in the recovered alcohol cold heat 1C, etc., and the cold turbine exhaust cold energy after cold recovery is mixed with seawater by the cold seawater mixer 2H in FIG. 2, and the natural phenomenon speedup device 2a natural phenomenon speedup 2a in the process of hot turbine exhaust cooling Then, feed the nutrients such as nitrogen, oxygen and CO2 to the sea floor, and increase the food of human beings to make the whole blade ratio material gravity gravity cooling turbine 8G.

In the process of generating the rotating power of all rotor blade specific material gravity cooling turbine 8G, increase the heating volume speed of compressed air 28a approaching absolute 0 degree with specific material 2E and add to the gravitational acceleration to increase the rotating output of turbine Then, cold heat is recovered from the cold turbine exhaust by the cold heat recovery unit 103, and the remaining cold low-temperature compressed air 28a is sucked and compressed by the air extractor 51, and injected and mixed into the cooling seawater of the hot turbine exhaust by the cold hot water mixer 2H. Cooling and cooling, the thermal turbine exhaust is cooled and condensed and injected into seawater, etc., and injected by the natural phenomenon acceleration device 2a, the natural phenomenon is accelerated and nutrients such as nitrogen, oxygen and CO2 are supplied to the seabed, The inner rotor blade group 60C and the outer rotor blade group 60D are provided with an additional thrust bearing 80a for hydraulic levitation to support a large weight, enabling a multi-stage turbine, and a large amount of ultra-high pressure cold / heat as in FIG. The energy conservation cycle to be produced, the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / sec, are made close to 36,000 times that of the existing steam turbine power generation, and the existing turbine blade cross-sectional area is cut 2 to 26 times Various energy conservation cycle coalescing engines that inject onto the turbine blade cross section 4X with the area to generate rolling contact rotation output of the specific material 2E and make maximum use of gravitational energy and solar thermal energy.

  The solar heater 2 shown in FIG. 4 uses various water surfaces, collects sunlight with the maximum amount of heat in a straight line with the long lens 2d, raises the temperature of the heat absorbing material 2B, and increases the width of the long lens 2d. Path 28A The air 28a temperature is increased at zero fuel cost, the temperature is increased by 3 days in one day, etc., so that all existing lens cross sections can be selected and used, and the selected lens cross section is linearly extended to generate sunlight. Condensed in a straight line so that all lens materials can be selected and used, and a long cylinder such as a cylinder is provided by surrounding a heat insulating material 2c such as foamed plastic with a semi-cylindrical outer box 77B, and a heat resistant material 2A is provided therein. The air 28a is heated by a plate-like heat absorbing material 2B that is heated to high temperature by solar heat, and a plurality of wide and long lenses 2d and the like are provided on the upper portion so as to be sealed and thermally insulated by a joint 80A + clamp 80B. Can be extended with a joint 80A, 180 degrees direction change In this case, a U-shaped air pipe is connected in parallel, and the solar heater 2 is rotated 180 degrees from the east to the west on the water to make a right angle with the sunlight. , By heating the air 28a, the suction compression 800-1200 degrees is possible with the 1-stage heat pump 1G, and the air is heated and compressed, so that solar heat production and geothermal heat production (substituting explanation with solar heat production) 2, the 1-multistage heat pump 1G described in FIG. 2 is used for infinite heat production of ultra-high pressure cold + ultra-high pressure heat, and heat such as water jet 79 and hot water 50 of the combined engine injection section 78 + cold 28a injection, etc. Use prime and cold energy prime.

In the generation of rotational output of the screw ship 39D in FIG. 5, the ship with a small demand for electricity, heat 50, and cold 28a is driven by the all-blade ratio critical material gravity turbine 8G in FIG. The material 2E gravity vacuum acceleration turbine 8G drive, the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / second, close to 36,000 times that of the existing steam turbine power generation, according to the amount of resources such as silicon-coated ultra-small diameter steel balls, Combined with existing screw ship, 1000 times rotation output, etc. Specific material 2E Low speed use is possible, large screw high speed drive etc. is set to 5 times speed of existing ship, CO2 exhaust 0 fuel cost 0 heat consumption 0 operation profit rate Various energy conservation cycle coalescence engines aiming for 10 times as many targets as various medium-sized and large-sized screw ships 39D.

  The water jet 79X water suction / injection screw ship 39D drive in FIG. 6 has the necessary number of all-blade ratio critical material gravity solar turbines 8G in FIG. 2, FIG. 3, and has the modification of the solar heater 2 in FIG. Heated air 28a is compressed multiple times with 1 to multiple-stage heat pump 1G and 1 to multiple-stage compression heat exchanger 2C, and heat is recovered multiple times, and divided and stored as hot 50 + cold 28a as in FIG. In the process of injection propulsion, each of the air extractors 51 is driven by driving the screw 7C with the total moving blade ratio critical material gravity solar heat turbine 8G and driving the water jet 79X with the hot 50 + cold heat 28a without limitation. As a combined extractor 51, the suction output is greatly increased, the cold 28a is sucked and merged into the 79X combustion gas high-speed jet optimum pressure section, the oxidant is increased, and the cold turbine 8G exhaust pressure is increased. The output is maximized to the minimum, and the heat of 50x is injected into the 79X superheated steam high-speed jet optimum pressure section, the maximum vacuum is set to maximize the output of the thermal turbine 8G, the natural phenomenon is accelerated, and all of nitrogen, oxygen, CO2, etc. Mixing with seawater, supplying food and nutrients to the microorganisms in the seawater, increasing the microorganisms The water jet 79X water suction injection propulsion is aimed at aiming the digestion ability of the microorganisms tens of thousands of times in the forest, and the natural phenomenon is accelerated most efficiently. 2a Increase human food, aim for 10 times the speed of existing ships, and make various energy conservation cycle coalescing engines aiming for the prime of various medium and large water jet 79X screw ships 39D.

  The water jet 79X water suction / injection ship 38C drive in FIG. 7 has the necessary number of gravity blades 8G of the total moving blade ratio critical material in FIG. 2, FIG. 3, and the solar heater 2 in FIG. 1 to the multistage heat pump 1G and 1 to the multistage compression heat exchanger 2C, the heat is recovered a plurality of times with multiple compression and high temperature, and divided and stored into the hot 50 + cold heat 28a as in FIG. The water jet 79X is driven by heat and cold of high pressure and mass without limitation, and in the process of injection propulsion, each air extractor 51 is used as a confluence extractor 51 to greatly increase the 79X suction output and 79X combustion gas high-speed injection The cold heat 28a is sucked and joined to the flow optimum pressure section, the oxidant is increased, the fuel combustion output is increased, the exhaust pressure of the cold turbine 8G is maximized, the 79X superheated steam 50 high speed injection flow optimum pressure section Increase the injection mass of suction combined propellant with the heat 50, maximize the output of the heat turbine 8G, maximize the output of the thermal turbine 8G, increase the natural phenomenon 2a as in Fig. 6, increase the human food, aim for 10 times the speed of existing ships And various medium-sized and large-sized water jet 79X water suction / injection ship 38C.

  The water jet 79Z air suction jet ship 38B drive of FIG. 8 is provided with the necessary number of all-blade specific gravity gravity solar turbines 8G in FIG. 2 and FIG. 1 to the multistage heat pump 1G and 1 to the multistage compression heat exchanger 2C, the heat is recovered a plurality of times with multiple compression and high temperature, and divided and stored into the hot 50 + cold heat 28a as in FIG. The water jet 79Z is driven by heat 50 + cold heat 28a such as high pressure and large mass without limitation, and in the process of injection propulsion, each air extractor 51 is used as a confluence extractor 51 to greatly increase the 79Z suction output and 79Z combustion gas The turbine exhaust cooling heat 28a is sucked and merged into the optimum high-speed jet flow pressure section, the oxidizer is increased, the fuel combustion output is increased, the exhaust pressure of the cooling turbine 8G is minimized, the rotational output is maximized, and the 79Z superheat In the optimum pressure portion of the gas 50 high-speed jet flow, the heat 50 is sucked and combined and the propellant injection mass is increased, the maximum vacuum is set and the thermal turbine 8G rotational output is maximized, and the natural phenomenon is accelerated as in FIG. Increase the amount of food, aiming at 10 times the speed of existing ships, and various energy conservation cycle coalescing engines aiming at the prime of various medium and large water jets 79Z air suction jet ship 38B.

  The water jet 79Z air suction / injection screw ship 39E drive of FIG. 9 is provided with the necessary number of all-blade specific gravity gravity solar turbines 8G in FIG. 2 and FIG. The heated air 28a is compressed and heated multiple times with 1 to multiple-stage heat pumps 1G and 1 to multiple-stage compression heat exchangers 2C, and heat is recovered multiple times, and divided and stored as hot 50 + cold 28a as in FIG. The blade 7C is driven by the all-blade ratio critical material gravity solar heat turbine 8G, and the water jet 79Z is driven by the hot 50 + cold heat 28a such as high pressure and large mass as much as possible. As a confluence extractor 51, the suction output is greatly increased to 79Z, and the cold heat 28a is sucked and combined into the optimum pressure portion of the 79Z combustion gas high-speed jet flow, the oxidant is increased, and the 8G exhaust pressure is set to the lowest rotational output, 79Z superheated steam 50 high-speed jet flow optimum pressure part is heated 50 to increase the suction merged propellant injection mass, maximum vacuum to maximize the thermal turbine 8G rotational output, As in FIG. 6, the natural phenomenon speed-up 2a increases human food, and aims at 10 times the speed of existing ships, and various energy storage cycle coalescing engines aiming at the prime of various medium and large water jets 79Z air suction jet screw ships 39E.

  The combined engine injection unit 78B solar gravity airplane 39A drive of FIG. 10 uses the flying body 38a vertical blade 38d as an integral unit, FIG. 2, FIG. In the process of sucking the air 28a from the air suction port 28B of the blade leading edge 38e of the vessel 2 deformed, the solar heating air 28a is heated in the suction air passage 28A constituted by the long lens 2d heat absorbing material 2B. Multiple-stage heat pump 1G and 1 to multiple-stage compression heat exchanger 2C are compressed multiple times to recover heat multiple times, and are divided and stored as hot 50 + cold 28a as in FIG. The hot 50 + cold heat 28a is supplied to the combined engine injection unit 78B, and is supplied to the combined engine injection unit 78B at a pressure of 10 to 100 times the existing jet injection pressure when the universe rises. 50 is heated to inject 10 times the amount of heat, etc., and the propulsion propulsion power reaches 100 to 1000 times that of existing jets in a short time to reach the space. It makes it possible to make day trips anywhere on the earth, such as 16 rounds of the earth a day, with zero or little fuel cost when flying in the atmosphere, and because the injection speed is maximum in vacuum, mass injection over existing space rockets is possible. Think of it as the worst, propelling high-power rockets at the highest flight altitude of existing airplanes and reaching space.

In the process of driving the all-blade ratio critical material gravity cooling / heating turbine 8G when reaching the space, the air passage 28A is used as the air passage 28A in which the air passage inlet 28B is hermetically sealed, and the direct intake sunlight is composed of the long lens 2d and the heat absorbing material 2B. The air 28a is heated by 28A, and the hot 50 + cold 28a is produced and stored most efficiently in the universe. The propulsion in space is propulsion by the superheated steam 50, and the compressed air 28a in space is used to produce the superheated steam 50. Using the turbine 8G1 to drive the multi-stage heat pump 1G, a long-distance space travel is possible, and when returning to the earth, high-pressure high-temperature air 28a including frictional heat is converted into heat for suction and compression, and compressed air 28a The cold turbine 8G is driven, and the exhaust gas is sucked and merged at the optimum pressure portion of the merging extractor 51 and the combined engine injection unit 78B oxidant and used as an oxidant. The steam 50 exhaust also merges to increase the propellant injection mass, the thermal turbine 8G exhaust chamber is set to the highest vacuum at an ultra-high speed flow rate of 78B, the fuel injection ignition combustion injection propulsion output is increased to the oxidant, and the existing jet 10 ~ 100 times pressure 1/10 injection heat quantity 10 times injection propulsion output enlargement, etc. Rotate the combined engine injection part 78B cylindrical rotation part 77G more than 180 degrees to enable reverse injection and vertical ascending vertical descent, The energy conservation cycle will be combined into an airfield anywhere on the rooftop of the building or on the moon.

  The combined propulsion engine 78B solar gravity rotary airplane 39B shown in FIG. 11 generates the propulsion propulsion output in the same manner as in FIG. 10, and FIG. 7B drive, heat production in the same manner as in FIG. 10, solar heating air 28a is compressed multiple times with 1 to multiple stage heat pump 1G and 1 to multiple stage compression heat exchanger 2C, and heat is recovered multiple times, As in FIG. 2, the heat 50 + cold heat 28a is divided and stored, and the heat 50 + cold heat 28a such as high pressure and large mass is supplied to the combined engine injection unit 78B. Is supplied to the combined engine injection section 78B, and the superheated steam 50 on the outer periphery of the fuel injection combustion is heated to the cold heat 28a to inject 10 times the amount of heat and the like, and the injection propulsion output is 100 to 1000 of the existing jet aircraft. To reach the space in a short period of time, make a space use prime near zero fuel cost with various jet propulsion solar thermal gravity rotating airplanes 39B, etc., enabling day trips anywhere on the earth, such as 16 rounds of the earth a day, When flying in the atmosphere, zero fuel costs and a slight propeller 7A flight or rotor wing 7B flight, the jet speed is the highest in vacuum, so the existing space rocket ground mass injection is considered the worst, and high power rocket propulsion at the highest flight altitude of the existing airplane Reach the universe.

At the time of reaching the space, in the process of driving the all-blade ratio critical material gravity cooling and heating turbine 8G, the air passage inlet 28B is changed to the sealed air passage 28A, and the heat recovery superheated steam propellant production is repeated as in FIG. In the space, the superheated steam 50 is most efficiently produced and stored in the 1-multistage heat pump 1G or solar heating, and the propulsion in space is propulsion by the superheated steam 50, and compression in space The air 28a is used for the production of superheated steam 50, and enables a long-distance space travel as a 1-8 multi-stage heat pump 1G driven by the turbine 8G. Then, the cooling turbine 8G is driven by the cold air of the compressed air 28a, and the exhaust gas is sucked and merged at the optimum pressure portion of the merging extractor 51 and the combined engine injection unit 78B oxidant to oxidize. In the same way, superheated steam exhaust also increases the combined propellant injection mass, makes the thermal turbine 8G exhaust chamber the highest vacuum at an ultra-high speed flow rate of 78B, and increases the fuel injection ignition combustion injection propulsion output to the oxidizer. 10 to 100 times pressure 1/10 injection heat quantity 10 times injection propulsion output enlargement, etc., the combined engine injection part 78B cylindrical rotation part 77G is rotated 180 degrees or more to enable reverse injection and vertical ascending vertical descent. Use it as an airfield wherever it is used, on the rooftop of the building, or on the moon, and combine it with various energy conservation cycle engines.

The water suction water jet 79U in FIG. 12 is used instead of the cold / hot seawater mixer 2H, the cold / heat recovery unit 103, etc. in FIG. 2, and the superheated steam 50 in which the superheated steam control valve 25 is stored in an open divided state is used as the combustor 1Y. Supply to the uppermost stream (improvement of the figure) of the superheated steam reservoir 95c on the outer periphery, open the combustion gas control valve 24 to the compressed air control valve 24A, and convert the combustion gas reservoir 49a around the 200 degrees 24-400 MPa combustion gas 49 to the combustion gas reservoir 95a combustor 1Y The fuel control valve 25b is supplied to the most upstream side of the fuel control pump 25b and the fuel injection pump 1D (not shown) injects the optimum temperature fuel in the fuel pipe 1b from the fuel injection nozzle 6X. 50, the combustion temperature is increased by the amount of heating, the superheated steam 50 around 400 degrees in the peripheral superheated steam reservoir 95c is heated to 600 to 900 degrees, etc., both the injection outputs are increased, and the plurality of combustors 1Y The gas injection nozzle 6Y is annularly provided on the outer periphery of the superheated steam reservoir 95c, and the fuel pipe 1b is temperature-controlled at the optimum temperature from the plurality of fuel injection nozzles 6X provided annularly in the first stage combustion injection flow. Combustor multiple optimal distance annular combustion, superheated steam 50 from the outer periphery, optimal distance annular heating superheated steam temperature 600-900 degrees, etc., increase the superheated steam volume, increase the injection speed and increase the combustion gas suction output As a water jet 79U that combines the large expansion speed of the superheated steam 50 and the high-speed combustion of the scramjet, the fuel injection is ignited and burned to the ultrahigh pressure and mass of the cold to maximize the fuel combustion amount and the injection speed.

Even after the third stage combustion from the outer periphery in the two-stage combustion, the passage of the high-temperature combustion part of the fuel pipe 1b is made small, and the superheated steam 50 injection flow is annularly heated by the combustion gas 49 from the inside and the outside, and the maximum temperature injection of the superheated steam 50 and the theory Enables multiple combustion such as four-stage combustion so that air-fuel ratio combustion is possible, the superheated steam temperature approaching 0 degree absolute at 100 degree atmospheric pressure vacuum is set to 600-900 degrees annular heating from inside and outside, and 50 volumes of superheated steam is water The injection output and the combustion gas suction output are increased to the maximum, the maximum speed injection is performed from the superheated steam injection nozzle 6A and the combustion gas injection nozzle 6Y, and the output for sucking water in front is increased to the maximum. , The injection propulsion output of the superheated steam 50 and the combustion gas 49 is maximized, the injection propulsion output of the water suction jet water jet 79U is maximized, and all of nitrogen, oxygen, CO2 etc. The rate of ultrafast feed mixture dissolved nutrients to maximize, to increase food phenomenal speed 2a mankind, increases water resistance insignificant 2b large vessels speed in various 10x of existing vessels.

The water suction water jet 79X of FIG. 13 is used instead of the cold / hot seawater mixer 2H, the cold / heat recovery unit 103, etc. of FIG. 2, and the superheated steam 50 in which the superheated steam control valve 25 is kept open is stored in the combustor 1Y. It is supplied to the uppermost stream of the superheated steam reservoir 95c on the outer periphery, the combustion gas control valve 24 to the compressed air control valve 24A are opened, and the cooling heat 28a of about 24 to 400 MPa combustion gas 49 around 200 degrees is fed to the uppermost stream of the combustion gas reservoir 95a combustor 1Y. The fuel control valve 25b is opened and the fuel pipe 1b fuel is injected from the fuel injection pump 1D not shown, and the superheated steam 50 on the outer periphery of the ignition combustion is heated in the uppermost stream of the combustor 1Y to burn the combustion temperature. And the like, and the heating power of the superheated steam 50 in the outer peripheral superheated steam reservoir 95c is increased to 600 to 900 degrees or the like. In the superheated steam reservoir 95c, an annular combustion is provided in the single-stage combustion injection flow from the respective fuel injection nozzles 6X. After the second stage combustion, the fuel pipe 1b can be optimally injected with fuel temperature, enabling fuel injection combustion theoretical air-fuel ratio combustion.

The superheated steam 50 approaching absolute 0 degree in the atmosphere at 100 degrees in vacuum is annularly heated from the outer circumference and the inner circumference at the optimum distance, the temperature of the superheated steam 50 is set to 600 to 900 degrees, and the injection speed is increased by increasing the superheated steam volume. As a water jet 79X that combines the large expansion speed of superheated steam and the high-speed combustion of the scramjet, the fuel injection ignition combustion is performed on the cold heat 28a having an ultra-high pressure and a large mass. The superheated steam 50 volume is set to a maximum of about 5000 times the injection speed of water, the superheated steam injection output and the combustion gas suction output are increased to the maximum, and the maximum speed injection is performed from the superheated steam injection nozzle 6A and the combustion gas injection nozzle 6Y. Water jet 79X that sucks and jets water in front and maximizes water suction and jet output, and speeds up natural phenomena that supply nutrients such as nitrogen, oxygen, and CO2 into the sea 2 To increase the food of mankind, to increase water resistance insignificant 2b a large ship speed in the various 10-fold of existing vessels.

The air suction water jet 79S shown in FIG. 14 is a portion where the water suction of the water suction water jet 79U shown in FIG. 12 is changed to air suction, and nutrients such as nitrogen, oxygen and CO 2 are greatly increased and injected into the sea and mixed with the sea water 52a. Is the optimum length, the seawater air mixing part is added and the nutrients are supplied and mixed at ultra high speed in the sea, and the natural phenomenon is accelerated as in Fig. 12a. Increase the water resistance to 2b, which is 10 times greater than

The air suction water jet 79T of FIG. 15 adds a plurality of afterburners 6X to the air suction water jet 79S of FIG. 14, injects fuel into the suction air 28a flow, and joins and burns the cold heat 28a combustion flow 6Y, thereby increasing the amount of fuel combustion. Increase the amount of nutrients such as nitrogen, oxygen, CO2 and so on into the sea to increase the optimum length for mixing with seawater 52a as in FIG. 14, and add seawater 52a air 28a mixing part to the sea The natural phenomenon speed-up 2a greatly increases human food, increases the speed of various medium and large-sized ships to 10 times the existing ship, and makes the water resistance very low 2b.

The air suction water jet 79Y shown in FIG. 16 uses the water suction of the water suction water jet 79X shown in FIG. 13 as air suction, greatly increasing the nutrients such as nitrogen, oxygen, and CO2 into the sea, and mixing the seawater 52a with the optimum length. In addition, the seawater 52a air 28a mixing part is added and the nutrients are supplied and mixed in the sea at an ultra-high speed, the natural phenomenon speeds up 2a. Increase water resistance to 2b.

The air suction water jet 79Z in FIG. 17 adds a plurality of afterburners 6X to the air suction water jet 79Y in FIG. 16, injects fuel into the suction air 28a flow, and joins and burns the cold heat 28a combustion flow 6Y, greatly increasing the amount of fuel combustion Then, the nutrients such as nitrogen, oxygen and CO2 are greatly increased and injected into the sea, and the part mixed with the seawater 52a is set to the optimum length as in FIG. 16, and the seawater 52a air 28a mixing part is added to add the nutrients into the sea. Super high speed feed mixing, natural phenomenon speeding up 2a Mankind's food is greatly increased, speed of various medium and large ships is increased to 10 times that of existing ships and water resistance is reduced to 2b.

The combined engine injection unit 78W in FIG. 18 uses the water suction of the water suction water jet 79U in FIG. 12 as air suction to form a combined engine injection unit 78W. Then, 1 to multiple stage compression heat recovery unit 2C recovers heat multiple times by fuel injection combustion multiple times, and unlimited increase in high pressure combustion gas 49 oxidant and superheated steam 50 propellant, storage gas control The valve 24 is opened, and a combustion gas 49 of about 200 to 24 degrees Celsius is supplied to the uppermost stream of the combustion gas reservoir 95a, and the fuel control valve 25b is opened. The fuel injection pump 1D (not shown) supplies the fuel pipe 1b fuel. It is injected from the fuel injection nozzle 6X, the heating combustion temperature of the superheated steam 50 at the outer periphery of the ignition combustion is increased in the uppermost stream of the combustor 1Y, and the superheated steam reservoir 95c having a long outer periphery is about 400 degrees around 24 to 400 MPa. 50, both the heating output of the combustion chamber 1Y are increased, and a plurality of combustion gas injection nozzles 6Y of the combustor 1Y are provided annularly from the inside of the superheated steam reservoir 95c, and fuel is injected from the fuel injection nozzle 6X of the plurality of single-stage injection combustion flows. Two-stage combustor multi-optimal annular combustion is used to increase the heating injection output and combustion gas suction output of superheated steam 50 from the outer periphery.

A plurality of combustion gas injection nozzles 6Y are provided in the two-stage combustion gas combustion flow, and the fuel injection three-stage combustor multi-optimal distance annular combustion is performed from each fuel injection nozzle 6X, so that the superheated steam 50 injection flow is generated from the inner periphery and the outer periphery. In the same way, if necessary, use high-mass cold heat. If necessary, use four-stage combustion and then multiple combustion, and make the superheated steam close to 100 ° C at atmospheric pressure and close to 0 ° C in vacuum, over 500 ° C. 10 to 100 times pressure 10 times mass injection low-cost injection output, combined with low-temperature injection large expansion speed of superheated steam 50 and high-temperature rocket injection of combustion gas 49, the best combination of the best use of each advantage Combined with high-speed combustion of scramjet + high-pressure injection large expansion speed of steam turbine + vacuum flight of rocket, the combined engine injection part 78W is 36,000 times the normal flight in the atmosphere With the turbine 8G close to the rate, the propellant and oxidant are conserved and increased, aiming at zero fuel cost flight, mainly as the propulsion propulsion by the superheated steam 50, as the prevention of global warming to prepare for space rise, and the cylindrical rotating part 77G is 180 degrees By rotating as described above, vertical ascent, vertical descent, and reverse injection are possible, and everywhere on the earth, it is possible to make day trips, etc. anywhere on the earth, such as airfields and 16 rounds of the earth per day.

A combined engine injection unit 78V in FIG. 19 adds a plurality of afterburners 6X to the combined engine injection unit 78W in FIG. 18, injects fuel into the suction air 28a flow, combines and burns into the cold 28a combustion flow 6Y, and increases the fuel combustion amount. The propulsion output is greatly increased, and the combined engine injection unit 78V super high pressure super large mass cold heat 28a combustion flow 6Y is combined and burned to reach space for a short time, 10 to 100 times pressure 10 times mass injection 1000 times injection propulsion of existing jet aircraft With the aim of output, the cylindrical rotating part 77G can be rotated 180 degrees or more to enable vertical ascent, vertical descent, and reverse injection. But it makes day trips possible.

The union engine injection unit 78A in FIG. 20 deletes the water suction injection unit of the air suction water jet 79Y in FIG. 16 to form the union engine injection unit 78A. Similarly to FIG. 16, the superheated steam 50 is contained in the first stage combustor 1Y. The superheated steam 50 is annularly heated from the inner periphery and the outer periphery by a multi-stage combustor 1Y suitable for the application, such as a two-stage combustor 1Y, a three-stage combustor 1Y, and a four-stage combustor 1Y. Combined engine injection part 78A Ultra high pressure super large mass cold heat 28a combustion flow 6Y fuel injection combustion to reach the space in a short time, cylinder rotation with the aim of 10 to 100 times pressure 10 times mass injection 1000 times injection propulsion output of existing jet aircraft Rotate part 77G more than 180 degrees to enable vertical ascent, vertical descent, and reverse injection, to make the best use of space anywhere such as airfield and 16 laps of the earth every day, enabling day trips anywhere on earth That.

A combined engine injection unit 78B in FIG. 21 is configured by adding a plurality of afterburners 6X to the combined engine injection unit 78A in FIG. 20 to form a combined engine injection unit 78B. Similarly to FIG. 20, the superheated steam 50 is generated by the first-stage combustor 1Y. Annular heating is performed from the inner periphery, and the superheated steam 50 is annularly heated from the inner periphery and the outer periphery by a multi-stage combustor 1Y such as a two-stage combustor 1Y, a three-stage combustor 1Y, or a four-stage combustor 1Y. The combined engine injection part 78B is superheated and burned into the high-pressure, ultra-high-mass cold 28a combustion stream 6Y, and further provided with a plurality of afterburners 6X in the air 28a suction-injection stream. Combustion significant fuel combustion amount addition, reach the space for a short time by using ultra high pressure super large mass cold 28a, aiming for 10 to 100 times pressure 10 times mass injection 1000 times injection propulsion output of existing jet aircraft, Rotate the cylinder rotation part 77G more than 180 degrees to enable vertical ascent, vertical descent, and reverse injection, to make the best use of space, such as airfields and 16 laps of the earth every day, day trips anywhere on the earth enable.

Theoretical best turbine is the all blade ratio critical material gravity turbine 8G, all blade ratio critical material gravity cooling / heating turbine 8G, all blade ratio critical material gravity thermal turbine 8G, etc. m / sec is close to 36,000 times that of existing steam turbine power generation, driving generators and ships, speeding natural phenomena 2a, supplying nutrients such as nitrogen, oxygen and CO2 to seawater, In order to multiply seaweeds, increase food for human beings such as fish and kombu through food chains, etc., and to make the speed of various medium and large ships 10 times faster than existing ships, water resistance is as low as 2b. There is a strong possibility of bringing the ship close to 0 and preventing the extinction of mankind.

Solar-heated air is sucked multiple times with 1 to multiple-stage heat pump 1G, recovered multiple times, and heat is recovered multiple times, and stored and used as hot heat 50 + cold heat 28a such as 24-400 MPa, turbine drive, combined engine injection unit drive and water Because it drives a generator, airplane and ship by jet driving, there is a possibility of CO2 exhaust zero generation prime, solar thermal gravity airplane prime and solar thermal gravity ship prime, and the power generation amount is about 10 times that of the existing world. There is a strong possibility that the ship speed will be about 10 times the speed of the existing ship and the water resistance will be a little 2b as the fuel cost is low. There is a possibility that it will be possible to make day trips anywhere on the earth by making the best use of space, such as airfields and 16 rounds of the earth per day.

  0: Combined engine with various energy storage cycles (storing various types of thermal energy such as solar heat and geothermal heat, using a heat pump to separate and store high-pressure hot and cold heat, and storing heat energy such as 500 or less liquid metals using a heat retaining device. The impact energy is preserved by providing impact reduction means coating on large turbine blades and metal balls, etc., and the impact energy is permanently preserved. The gravitational energy is preserved by using an ascending device to save the gravitational energy by 1000 m. 1C: alcohol cold heat, 1D: fuel injection pump, 1F: condensate pump, 1G: one-stage heat pump (warm heat 50 + cold heat 28a divided storage cold heat recovery mass infinite increase target) 1G: two-stage heat pump (heat heat 1+: Combustor (Characterized by superheated steam 50 heating with ultra high pressure and high speed combustion) 1b Fuel pipe (provided so that the fuel injection temperature becomes the optimum temperature) 1d: Mercury, 1g: Gravity accelerating section, 1h: Horizontal axis, 2: Solar heater (High temperature by collecting sunlight linearly with long lens) 2a: Acceleration of natural phenomenon (utilization of the phenomenon that microorganisms etc. are digested to zero overnight when the rest of food is thrown away in a nearby river with almost zero change in air) 2a: Acceleration of natural phenomenon Equipment (equipment of cold power 28a into seawater by power generation, supply seawater with natural speed reduction to the seabed, supply nutrients such as nitrogen, oxygen and CO2 to greatly increase fish, kombu, etc.) 2a: Speed up natural phenomena (ship ) Supply nutrients such as nitrogen, oxygen and CO2 into the sea, aiming for the digestive ability of microorganisms tens of thousands of times in the forest, increasing phytoplankton, seaweed, etc. to increase human food such as fish and kombu through food chain etc.) 2b: Water resistance Slightly (for speeding gliding 2c: heat insulating material, 2d: long lens, 2e: water surface, 2A: heat-resistant material, 2B: heat-absorbing material, 2C: one-stage compression heat recovery device (cooling production method is 2X2Y2Z as a first-stage compression high temperature with a heat pump 2C: 2 to 2 stage compression heat recovery device (cooling production method aims to infinitely increase the cold pressure in the heat recovery container with 2X2Y2Z as a high temperature compression 2 to 2 times with heat pump) 2E : Specific critical substances (metal, platinum sphere, coated platinum sphere, gold sphere, coated gold sphere, platinum alloy sphere, alloyed metal sphere, coated metal sphere, water, etc. 2E: Specific critical substance (Manufacturing method reduces the impact energy as the diameter decreases. For example, molten steel is injected into the atmosphere at high speed and air cooled water is cooled to produce ultra-small diameter steel balls, etc.) Coated metal ball impact 2F: Specific critical substance raising device (gravity energy is increased and stored) 2H: Cold seawater mixer (mixing cold water into seawater, cooling the superheated steam vaporization heat in the process of speeding up the natural phenomenon) 2X: Air heat exchanger (Air is compressed with a heat pump to increase the heat recovery compressed air mass infinitely or the pressure is infinitely increased) 2Y: Water heat exchanger (High-temperature air or combustion gas is used to produce superheated steam) 2Z : Specific critical material heat exchanger (used for temperature control of liquid metal below 500 degrees) 3E: Specific critical material and impact reducing material (turbine protection with mercury, liquid metal and water below 500 degrees) 4X: Turbine blade 6A: Superheated steam injection nozzle, 6W: Specific material accelerator 6X: Fuel injection nozzle, 6X: Afterburner (fuel injection cold heat 28a combustion in suction air flow) 6Y: Combustion gas injection nozzle (cooling heat 28a combustion flow) 7A: Propeller, 7B: Rotor blade, 7C: Screw, 8c: Turbine blade, 8G: All blade turbine ( Vertical all-blade turbine opposed series all-blade flywheel turbine series all-blade flywheel turbine bite-in series all-blade flywheel turbine) 8G: All-blade ratio critical material gravity solar thermal turbine Since the damming output is close to zero with the stationary blades, all rotor blades are essential, and the work rate is 1 / 360,000, which is as small as that of platinum spheres. Near-heat + cold-producing turbine drive) 8G: Gravity turbine with all blade ratio critical material (use of hot-drive + cold-drive because the head is limited, so no head use is limited) 8G: turbine (light Quantification required Large area required Turbine blades, silicon-coated turbine blades, etc. when using ultra-small diameter steel balls, silicon carbide-coated turbine blades, etc. when using silicon-coated ultra-small diameter steel balls, etc.) 10: Hull, 10A: Ship cabin, 10b: Cockpit, 10c: Control room, 10d: Guest room, 10e: Cargo compartment, 24: Combustion gas control valve, 24A: Compressed air control valve, 25: Superheated steam control valve, 25b: Fuel control valve, 28a: Air, 28a: Cold (solar heat) And the geothermal heat is recovered multiple times with air 28a, and compressed heat is recovered multiple times and divided and stored in the form of 50 heat of superheated steam + cold air of compressed air 28a) 28b: heat of compressed air, 28A: intake air path, 28B: air path inlet, 38a: flight trunk, 38b: flying wing, 38c: flying tail, 38d: vertical wing, 38e: wing leading edge, 38g: surface wing, 38h: levitation boat, 38B: air suction jet Ship (with 79S79T79Y79Z) 38C: Water suction jet ship (with 79U79X) 39A: Solar thermal gravity plane, 39B: Solar thermal gravity rotating plane, 39C: Solar thermal gravity helicopter, 39D: Screw ship, 39G: Solar thermal gravity flying ship, 40A: Rudder, 49: Combustion gas, 50: Superheated steam, 50: Warmth (solar heat and geothermal are recovered by air 28a and compressed heat is recovered and divided into 50 heats of superheated steam + compressed air 28a cold) 51: Air extractor, 51: Combined extractor (extractor for joining) 52a: Water, 52b: Hot water, 52d: Hot heat (changed from 50) 52e: Cold heat (changed from 28a) 55B: Transmission, 60A: Inner shaft device (equipped with turbine blades) Device) 60B: Outer shaft device (equipment with turbine blades) 60C: Inner blade group ( 60D: Outer rotor blade group (inner side and outer side oppositely rotated) 77B: Semi-cylindrical outer box, 77F: Injection section outer box, 77G: Cylindrical rotating section, 77a: Turbine outer box, 78A: Combined engine injection part (super high pressure superheated steam is heated and injected at least once from the inner periphery and inner periphery and outer periphery with super high pressure combustion gas) 78B: Combined engine injection part (super high pressure superheated steam is applied to the inner periphery and inner periphery with ultra high pressure combustion gas) 78V: Combined engine injection part (super high pressure superheated steam with super high pressure combustion gas, additional heating afterburner injection from the inner periphery, outer periphery and inner periphery outer periphery) 78W: Combined engine injection part (ultra high pressure) 79S: Water jet (super high pressure superheated steam is heated and jetted from the inner circumference, outer circumference and inner circumference outer circumference with ultrahigh pressure combustion gas) 79T: Water jet (Addition of afterburner heating with super-high pressure superheated steam from the inner circumference, outer circumference and inner circumference outer circumference with super-high-pressure combustion gas) 79U: Water jet (Inner circumference, outer circumference and inner circumference outer circumference with super-high pressure superheated steam with ultra-high pressure combustion gas) 79X: Water jet (Super high pressure superheated steam is injected with super high pressure combustion gas at least once from the inner circumference and inner circumference outer circumference and heated jet water suction jet) 79Y: Water jet (Ultra high pressure superheated steam is super high pressure) 79Z: Water jet (super high pressure superheated steam is heated and injected once more from the inner circumference and inner circumference outer circumference at least once from the inner circumference and inner circumference outer circumference) 80: Bearing, 80a: Thrust bearing (equipped with multiple finely inclined or metal O-rings on the inner and outer surfaces so that it can be finely floated by hydraulic pressure) 80A: Joint, 80B: Tightening 84: Counter-rotating device (apparatus that makes the inner rotor blade group and the outer rotor blade group having the fixed portion rotate at substantially the same speed in the previous application) 84Y: Counter-rotating gear device (same for existing technology) 95a : Combustion gas reservoir, 95b: compressed air reservoir, 95c: superheated steam reservoir, 103: cold energy recovery device,

Claims (32)

  Combined with various energy storage cycles to generate electricity with unlimited hydraulic fluid thrust thrust bearing (80a) and 1 to 120 stage equivalent material (2E) with unlimited constant gravity material (8G) of all rotor blade specific material gravity turbine (8G) organ.   Increase the amount of cold (28a) and increase the cold pressure by using 1 to multi-stage heat pump (1G) to 1-stage multi-stage compression heat recovery unit (2C) with gravity blade (8G) drive Various energy conservation cycle coalescence engine.   Increase the production amount of cold heat (28a) with 1 to multi-stage heat pump (1G) 1 to multi-stage compression heat recovery unit (2C) by generating electricity and driving with all blade ratio critical material gravity turbine (8G). Various energy conservation cycle coalescence engine used for ascending use.   Total moving blade ratio material Gravity solar power turbine (8G) power generation electric drive or (8G) drive and heat production (50) + cold heat (28a) increased by 1 stage heat pump (1G) 2 to multiple stage heat Various energy storage cycle coalescing engines that use the pump (1G) with further increased cold pressure.   Various energy storage cycle coalescing engines with various rotor blade ratio critical material gravity solar heat turbine (8G) 1 to multi-stage compression heat recovery device (2C) and propeller (7A) drive.   Various energy storage cycle coalescing engines with various moving blade ratios, such as gravitational solar thermal turbine (8G) 1 to multistage compression heat recovery unit (2C) and various types of airplanes driven by rotor blades (7B).   Various energy storage cycle coalescing engines as various vessels driven by screw (7C) equipped with all-blade ratio critical material gravity turbine (8G) 1 to multistage compression heat recovery unit (2C).   Variety of various airplanes driven by the combined engine injection part (78A) with hot (50) + cold (28a) produced by the total moving blade ratio critical material gravity solar heat turbine (8G) and 1 to multistage heat pump (1G) Energy conservation cycle coalescence engine.   Variety of various airplanes driven by the combined engine injection part (78B) with hot (50) + cold (28a) produced by a gravity-solar turbine (8G) and 1 to multi-stage heat pump (1G) Energy conservation cycle coalescence engine. Variety of various airplanes driven by a combined engine injection unit (78V) with hot (50) + cold (28a) manufactured by a gravity solar thermal turbine (8G) and 1 to multi-stage heat pump (1G) Energy conservation cycle coalescence engine.
Body engine.   Variety of airplanes driven by a combined engine injection unit (78W) with hot (50) + cold (28a) manufactured by a gravity bladed thermal turbine (8G) and 1 to multi-stage heat pump (1G) Energy conservation cycle coalescence engine.   All kinds of energy conservation as various vessels driven by water jet (79S) with hot (50) + cold (28a) manufactured by gravity solar thermal turbine (8G) and 1 to multi-stage heat pump (1G) Cycle coalescence engine.   All kinds of energy conservation as various ships driven by water jet (79T) with hot (50) + cold (28a) produced by gravity turbine (8G) and 1 to multi-stage heat pump (1G) Cycle coalescence engine.   All kinds of energy conservation as various ships driven by water jet (79U) with hot (50) + cold (28a) manufactured by gravity turbine (8G) and 1 to multi-stage heat pump (1G) Cycle coalescence engine.   All kinds of energy preservation as various ships driven by water jet (79X) with hot (50) + cold (28a) manufactured by gravity turbine (8G) and 1 to multi-stage heat pump (1G) Cycle coalescence engine.   All kinds of energy conservation as various vessels driven by water jet (79Y) with hot (50) + cold (28a) manufactured by gravity solar thermal turbine (8G) and 1 to multi-stage heat pump (1G) Cycle coalescence engine.   Energy saving as various ships driven by water jet (79Z) with hot (50) + cold (28a) manufactured by gravity turbine (8G) and 1 to multistage heat pump (1G) Cycle coalescence engine.   Various energy storage cycle coalescing engines that drive vehicles with electricity generated by all-blade ratio critical material gravity turbine (8G) to multistage compression heat recovery unit (2C).   Various energy storage cycle coalescence engine that drives vehicles with electricity generated by all-blade ratio critical material gravity solar turbine (8G) 1 to multistage compression heat recovery unit (2C).   Various energy storage cycle coalescing engines that drive automobiles with electricity generated and stored in a full-blade specific material gravity turbine (8G) 1 to multistage compression heat recovery unit (2C).   Various energy storage cycle coalescing engines that drive automobiles with electricity generated and stored in all-blade ratio critical material gravity solar turbine (8G) 1 to multistage compression heat recovery unit (2C).   Various energy storage cycle coalescing engines that drive ships with electricity generated and stored in all-blade ratio critical material gravity turbine (8G) 1 to multistage compression heat recovery unit (2C).   Various energy storage cycle coalescing engines that drive ships with electricity generated and stored in a full-blade ratio critical material gravity solar turbine (8G) 1 to multistage compression heat recovery unit (2C).   All kinds of space return airplanes driven by a combined engine injection unit (78A) with hot (50) + cold (28a) manufactured by a gravity solar thermal turbine (8G) and a multistage heat pump (1G). Various energy conservation cycle coalescing engines.   For various space return airplanes driven by a combined engine injection unit (78B) with hot (50) + cold (28a) produced by a gravity bladed thermal turbine (8G) and 1 to multi-stage heat pump (1G) Various energy conservation cycle coalescing engines.   All kinds of space return airplanes driven by a combined engine injection unit (78V) with hot (50) + cold (28a) manufactured by a gravity-solar turbine (8G) and a multistage heat pump (1G). Various energy conservation cycle coalescing engines.   All kinds of space return airplanes driven by a combined engine injection unit (78W) with hot (50) + cold (28a) manufactured with a gravity-severe solar thermal turbine (8G) and 1-stage heat pump (1G). Various energy conservation cycle coalescing engines.   Various energy storage cycle coalescence engine which makes home electrification prime, such as driving a refrigerator with electricity generated by the total power blade ratio critical material gravity solar heat turbine (8G) 1 to multistage compression heat recovery device (2C).   Various energy storage cycle coalescence engine that makes the best use of cold energy, such as mass production of ice with cold (28a) manufactured by a gravity solar thermal turbine (8G) 1 to multiple stage heat pump (1G).   Various energy conservation cycle coalescence engine that makes the best use of isothermal heat by injecting the heat (50) produced in the whole blade ratio critical material gravity solar turbine (8G) 1-multistage heat pump (1G) into methane hydrate and recovering methane .   Various energy storage cycle coalescence engines that make the factory electrification prime, such as driving machine tools with electricity generated by the gravity of the moving blade ratio critical material gravity solar heat turbine (8G) 1-multistage compression heat recovery device (2C).   Various energy storage cycle coalescence engines that make the factory electrification prime, such as driving machine tools with electricity generated by gravity turbine (8G) 1 to multistage compression heat recovery unit (2C) equipped with full blade ratio material.