JP2000038927A - Various kinds of steam gas turbine integrated engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To improve a ratio output as well as heat efficiency of a gas turbine effectively utilizing compressed air by driving a steam turbine and the like by superheated steam obtained by carrying out heat exchange so as to set a combustion gas temperature to a turbine heat resistance limit temperature or less. SOLUTION: Compressed air 15 is supplied to a device which serves as both a combustor and a heat exchanger, fuel is burnt together with stoichiometric air-fuel ratio fuel, and all superheated steam 5 generated by carrying out heat exchange without exceeding a heat resistance limit temperature of a turbine in a temperature of combustion gas 10, is individually used through respective steam regulating valve 7, and it is used for various kinds of steam turbine including all moving blades for necessitating superheated steam 5. All combustion gas is supplied to the most upstream part of various kinds of gas turbines so as to generate rotating force. An electric power generator and/or an electric motor are/is arranged as various kinds of gas turbine and various kinds of steam turbine having output shafts 12 respectively, a steam gas turbine integrated engine is arranged as a large power generation facility and/or a start device so as to utilize rotational force.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combined steam and gas turbine engine, and more particularly, to an outer wall of a plurality of combustors of a gas turbine, which is formed by a substantially spiral welded water cooling outer wall heat exchanger or a spiral water cooling outer wall unit. By providing an annular compressed air receiving portion and an annular combustion gas sending portion as an assembling structure heat exchanger or a spiral welding structure water-cooled outer wall unit assembling structure heat exchanger, a reasonable cylindrical shape is enabled, A large pressure increase and a highly efficient heat exchange are enabled, and the combustor / heat exchanger is provided in a honeycomb shape according to the application to increase a heat exchange heat transfer area and to provide a fuel supply means as a high pressure vessel. About three times that of the prior art, it is easy to add it to the most upstream side, and a steam superheater is provided in the combustor / heat exchanger, including one that is nearly linear in a spiral shape. Rocket that injects superheated steam Including such a steam turbine for obtaining an output by superheated steam, a gas turbine for obtaining an output by combustion gas, the steam gas turbine for obtaining an output by superheated steam and combustion gases, various aircraft, various vessels,
The present invention relates to a new technology of various types of steam gas turbine combined engines that can be used in various applications such as various vehicles and various power generation facilities and appropriately include a magnetic friction power transmission device.

[0002]

2. Description of the Related Art Japanese Patent Laid-Open Publication No. Sho 50-89737 discloses a prior art in which a heat exchanger is provided inside a gas turbine combustor in a steam turbine / gas turbine combined engine. The present invention provides a steam turbine cycle superheater or reheater in a high temperature region of a gas turbine combustor, thereby eliminating the need for a special auxiliary combustor.
The purpose is to increase the superheated steam temperature of the steam turbine cycle and improve the efficiency of the entire combined plant. Also, Japanese Patent Laid-Open No. 52
No. 156248 discloses that evaporation is performed by heat exchange with combustion gas between gas turbines, thereby reducing the temperature of waste gas at a waste heat recovery boiler outlet and improving boiler efficiency. However, none of these aims to improve the thermal efficiency of the supercharging boiler cycle, and does not aim to increase the pressure ratio and the specific output of the gas turbine at the same time, nor to increase the thermal efficiency of the gas turbine.

[0003] Further, as a prior application, a gas turbine combustor is improved.
No. 5074, Japanese Patent Application No. 7-335595, Japanese Patent Application No. 8-4
1998, Japanese Patent Application No. 8-80407, Japanese Patent Application No. 8-14
No. 3391, Japanese Patent Application No. 8-204049, Japanese Patent Application No. 8-2
No. 72806, Japanese Patent Application No. 9-106925, Japanese Patent Application No. 9-106
There are 181944, Japanese Patent Application No. 10-134720, Japanese Patent Application No. 10-134721, and Japanese Patent Application No. 11-69406. The priority application based on the above-mentioned prior application generally includes a heat exchanger in which a plurality of combustors including a whole rotor blade and / or a gas turbine are lengthened and a water-cooled outer wall is spirally provided to form a high-pressure vessel. An apparatus and method that can simultaneously increase the pressure ratio and the specific output to the maximum without exceeding the turbine heat-resistant limit temperature by being able to convert most of the supplied heat into superheated steam, also serving as an exchanger. Thing.

[0004]

What is important as the performance of a gas turbine cycle is thermal efficiency and specific power.
The higher the pressure ratio, the higher the thermal efficiency is obtained. If the thermal efficiency (pressure ratio) is constant, the larger the amount of heat supplied to the cycle, the higher the specific output. That is, the increase in the pressure ratio and the specific output is greatly restricted by the heat-resistant limit temperature of the turbine. For this reason, the method of increasing the pressure ratio and the supplied heat (fuel combustion mass) to the maximum without exceeding the heat-resistant limit temperature of the turbine is to convert most of the supplied heat (fuel calorific value) into superheated steam, It is used for gas turbines, heat efficiency x specific power = pressure ratio x combustion gas mass = speed x mass and greatly increases, and the supercritical gas obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature is obtained. It is intended to be used for transporting people and luggage, and for supplying heat and electricity, including a rocket that injects a jet by increasing the pressure ratio to about 10 times by using superheated steam.

[0005] That is, the obstacle to increase the pressure ratio and the specific output of the gas turbine is the fuel calorific value of the supplied calorific value.
In the previous application, the steam gas turbine and the combustor and heat exchanger of the gas turbine were lengthened or shortened by installing them in a small-diameter many-honeycomb shape in the earlier application because there were an unlimited number of types including various steam gas turbines. In order to support an infinite number of applications, it is designed to have a reasonable cylindrical shape, including intermediate ones. In addition, the fuel exothermic material supplied from the plurality of fuel supply means on the most upstream side, which is also used as a heat exchanger having a greatly increased heat transfer area, is largely converted into superheated steam, without exceeding the heat-resistant limit temperature of the turbine. To provide an engine capable of increasing the pressure ratio and the specific power to the limit, for example, by increasing the fuel combustion mass up to the stoichiometric air-fuel ratio by about four times that of the prior art, thereby increasing the pressure ratio and the fuel combustion mass. By providing a device that significantly reduces the amount of heat used by the gas turbine in the amount of heat supplied and increases the thermal efficiency and specific output of the gas turbine, the combustion gas and the combustion gas temperature are below the turbine heat-resistant limit temperature. Driving a steam turbine compressor or a steam turbine and a steam gas turbine with superheated steam obtained by heat exchange, for example, driving various vehicles and machines,
Another object is to drive various aircraft, drive various ships, or use it for heat or electricity supply equipment.

[0006] Combustion gas as a working gas for a gas turbine generally has a very high air ratio, and includes air that is about four times the stoichiometric air-fuel ratio (hereinafter, it is assumed that the air contains about four times the stoichiometric air). Is not limited to a numerical value), that is, in the prior art, a large amount of heat energy is consumed to wastefully discharge nearly 80% of the compressed air, and additionally used to reduce the combustion temperature (heat energy reduction). Heat and superheated steam conversion by a combustor and heat exchanger to enable the compressed air for combustion to be effectively used up to nearly 100%, and to use a bypass for other uses requiring compressed air. In response to this, the pressure ratio due to heat exchange and temperature decrease and the fuel combustion mass greatly increase, so that the amount of heat used by the gas turbine or the steam gas turbine out of the supplied heat is greatly reduced, and the thermal efficiency of the gas turbine is increased by 2%. The steam turbine and the steam gas turbine are driven by superheated steam obtained by heat-exchanging so that the specific power greatly increases or the combustion gas and the combustion gas temperature become equal to or lower than the heat-resistant limit temperature of the turbine. Then, the use of superheated steam including supercritical steam conditions in which the pressure ratio has been greatly increased to about 10 times that of air compression reduces the total thermal efficiency by 2%.
It is an object of the present invention to greatly increase the specific output as well as to approximately three times.

If the combustor / heat exchanger of the gas turbine is provided in a honeycomb shape and used also as a heat exchanger having a greatly increased heat transfer area, the combustion temperature can be reduced and the pressure ratio can be increased without limit. You. The higher the pressure ratio, the higher the thermal efficiency of the gas turbine. In the case of fuel combustion of the same calorific value, the higher the pressure ratio, the higher the temperature. In addition, the higher the gas temperature at the turbine inlet is 700 C to 1000 C, the higher the heat exchange. Also becomes easier. For this reason, by reducing and shortening the heat transfer area of the heat exchanger, fuel supply means can be provided only on the most upstream side,
Also enables NOx reduction combustion by cooling. In addition, exhaust pressure loss can be significantly reduced by increasing the pressure ratio and lowering the heat exchange exhaust heat temperature. That is, the present invention provides an ultra-high-performance and ultra-high-efficiency steam-gas-turbine combined engine capable of effectively utilizing the calorific value to the utmost limit, and makes the most of the magnetic friction power transmission device of the earlier application to reduce the power transmission loss. It aims to reduce to the limit.

[0008]

SUMMARY OF THE INVENTION The combustion gas as the working gas of the prior art gas turbine generally has a very high proportion of air and contains about four times the theoretical mixing ratio. That is, a large amount of heat energy is consumed, and about 80% of the compressed air is wasted, and the combustion temperature is reduced (heat energy is reduced).
In order to make it possible to effectively use approximately 100% of the compressed air for combustion by superheated steam conversion by heat exchange, a combustor / heat exchanger is used depending on the application. In the gas turbine, the combustion gas is supplied from the most upstream side, and the steam gas turbine is supplied to the intermediate stage from the inside according to the pressure to directly reheat the superheated steam. An air receiving portion (61) and an annular combustion gas sending portion (58) are provided to enable easy and rational cylindrical shape installation of a combustor / heat exchanger, as well as high pressure and the most upstream flow of fuel supply means. In addition to making it possible to increase the fuel supply amount to about four times that of the conventional technology, the heat transfer area is greatly increased as a combustor and heat exchanger, and the outer wall of the combustor is guided. Spiral welded structure including water pipe Spiral welding structure Water-cooled outer wall unit assembly structure or spiral water-cooled outer wall unit assembly structure, a relatively large pressure ratio is set, and superheated superheated steam obtained by heat exchange is injected and used. We provide water jet propulsion devices and rockets as devices and machines.

The design items of the combustor / heat exchanger include:
In the case of the smallest diameter, the part near the end of the water-cooled outer wall water pipe is used as a superheated steam as a steam pipe, and the steam pipe is sequentially provided in the water-cooled outer wall in a spiral from a nearly linear spiral in accordance with the inner diameter. It is also used as a very high-pressure, high-performance heat exchanger. When the heat exchange amount is small and the diameter is the largest, it becomes a honeycomb shape with a single row on the outer circumference. In addition, since a cylindrical combustor / heat exchanger is provided in a honeycomb shape, an empty space can be created. However, the empty space may be an unillustrated empty combustor / heat exchanger. In that case, FIG. d) Use a water-cooled external wall combustor / heat exchanger. By this heat exchange, the turbine inlet temperature is lowered below the turbine heat-resistant limit temperature, the total compressed air compressed for combustion is brought close to the stoichiometric air-fuel ratio combustion, and the fuel combustion mass can be increased to about four times that of the prior art. The use of fuel calorific value is greatly converted to superheated steam, and the pressure rises nearly 10 times that of air compression, including supercritical steam conditions, greatly increasing thermal efficiency and specific power, saving fuel and burning. The superheated steam obtained by exchanging heat so that the gas and combustion gas temperatures are equal to or lower than the turbine heat resistance limit temperature drives the steam gas turbine or the gas turbine and the steam turbine or the steam gas turbine and the steam turbine, and By rotating propellers, wheels, generators, machines, etc. to drive various aircraft, cars, ships, machines, etc., depending on the application, various types of superheated steam exhaust and combustion gas exhaust are injected. A device or the like buoyant exhaust injection promote the sky machines and ships, and the like, to provide, including a control device for controlling the severally.

Further, when comparing the case of compressing air with the case of compressing water, it is much more advantageous to compress water in which water vapor is condensed to about 1/700. In addition to being able to increase the amount of heat (the amount of retained heat energy), if it is released as superheated steam with a pressure of about 10 times that of air compression, it becomes 1700 times in the atmosphere and has a much larger volume of ultra-high speed in a vacuum such as space. Can be obtained. In either case, a large increase in thermal efficiency is obtained, so the best way to effectively utilize substantially all of the compressed air for combustion is to convert it to superheated steam with the highest efficiency, including substantially all of the increased supply fuel. is there. Therefore, in order to obtain a super-high performance combustor / heat exchanger, combustion and heat exchange are performed in an atmosphere of high temperature and high pressure as much as possible, and heat exchange is performed most efficiently, and N
Enables Ox reduction combustion. In addition, the amount of heat (superheated steam) extracted from the fuel having the same calorific value is maximized to obtain the superheated steam most efficiently, the steam gas turbine or the combustion gas mass for driving the gas turbine is maximized, and the heat combustion drives Minimizes the amount of heat and drives the steam gas turbine or gas turbine with the highest thermal efficiency. In addition, the exhaust heat is injected as a very low-temperature, very low-temperature exhaust heat to significantly reduce the exhaust loss as a very low-temperature exhaust. In addition, a bypass is provided for other uses that require compressed air. In addition, instead of a gear device for normal use, by appropriately or entirely using the magnetic friction power transmission device of the previous application, including any auxiliary equipment, as a drive device for transmitting power most efficiently, The maximum thermal efficiency of the steam gas turbine cycle including all rotor blades is greatly increased by about 2 to 3 times.

[0011]

DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiments and examples of the present invention will be described with reference to the drawings. The reference numerals are given and the overlapping description is omitted, and the characteristic portions and the portions that are insufficiently described will be sequentially described. In addition, some parts are described with numbers in order to specifically and clearly explain the intended and expected aspects of the invention, but are not limited to numbers.
Further, the combustor / heat exchanger 4 used in the present invention has an annular compressed air receiving portion 61, which has been increased in length in the earlier application or conversely, has been shortened in the shape of a large number of small diameter honeycombs.
In addition, the heat transfer area of the heat exchanger will be expanded according to the application, such as honeycomb, by the annular combustion gas delivery section 58. In the gas turbine, the combustion gas is supplied to the most upstream side of the turbine cascade,
In the steam gas turbine, a rational configuration was adopted to supply the gas to the middle stage from the inside according to the pressure. As shown in FIGS. 1 to 6 and FIGS. 17 to 20, the water-cooled outer wall 26 is formed as a spiral welded structure including a plurality of water pipes 1 or a water-cooled outer wall unit 52 assembly structure including a spiral welded structure. A relatively large pressure ratio is set as the combustor / heat exchanger 4, and the steam pipe 6 is provided inside in a substantially spiral shape or a nearly linear spiral shape. For example, a combustor / heat exchanger 4 in the form of a beehive, for example, is provided with a generator / motor (not shown) to serve also as a heat and electricity co-supply facility or as a starting device.
As a result, it is easy to increase the number of fuel supply means, for example, by providing the fuel supply means 27 at the most upstream side of each husband and the heat exchange rate is greatly increased.

Referring to FIG. 1 and FIG. 2, an embodiment of a core portion of a combined blade / steam gas turbine engine will be described. The idea of a fixed blade is that when a vehicle is pushed by hand and the vehicle is moved, a brake is applied. Pushing it while it is very tired, but the workload is 0, and you can move easily by releasing the brake and pushing.
Therefore, if a compressor or a turbine has a stationary blade, a large loss of energy will result in a large loss of energy. Therefore, the stationary blade is replaced with a moving blade as a whole moving blade, and the replaced moving blade is connected to an outer shaft device. The inner shaft device and the outer shaft device, which are connected to the inner shaft device and rotate in opposite directions to each other, are connected by a magnetic friction power transmission device 14 having a cooling device such as the water pipe 1 so that the two shafts are most efficiently connected. Double inversion drive. By doing so, the peripheral speed is shared approximately by half, the outer diameter is approximately doubled, and the fluid passage is approximately 4
As a result, the specific output is greatly increased, and the thermal efficiency is greatly increased. Alternatively, the peripheral speed is made substantially the same as that of the prior art, and the relative speed between the moving blades is made about twice, so that the specific output and the thermal efficiency are greatly increased. Alternatively, by making the peripheral speed approximately half that of the conventional technology, it is possible to make various designs (commercial or household combined use of heat and electricity, etc.) such as inexpensive and quiet with an allowable stress of about 1/4. , To greatly increase the thermal efficiency.

Referring to a first embodiment of the core portion of the combined steam and gas turbine engine shown in FIG. 1 and FIGS. 25 to 28, another description will be given. Air is normally sucked from the stage 16, and the even-numbered inner compressor blade group 17 and the odd-numbered outer compressor blade group 16 cooperate with each other to efficiently compress air by all the blades, and to perform the compression. The air 15 is formed into a honeycomb shape from the outer compressor rotor blade group final stage 16 through the annular outlet 21 through the annular outlet 22 and the annular compressed air reservoir 8 of the annular compressed air receiving portion 61A to increase the heat transfer area. To the burner / heat exchanger 4. The supplied high-compression air is stirred and mixed with up to about four times the fuel of the prior art, which is supplied from the fuel supply means 27 on the upstream side of each of them according to a command from a known control device not shown. The combustion and heat exchange are performed while controlling the combustion in the combustor / heat exchanger 4 in a honeycomb shape so that the combustion gas temperature is equal to or lower than the turbine heat-resisting limit temperature by performing the combustion including the substantially stoichiometric air-fuel ratio combustion. Then, the combustion gas 10 is cooled by the water-cooled outer wall 26 and the steam pipe 6 of each of the water guide pipes 1 to perform NOx reduction combustion. The combustion gas 10 obtained by the NOx reduction combustion is supplied from the respective combustor / heat exchanger 4 through the annular combustion gas reservoir 9 of the annular combustion gas delivery section 58A to the outside where the compressor-like compression blades are provided. According to the pressure from the annular delivery portion 18B of the inner shaft device via the annular delivery portion 18A on the shaft device side, all the rotor blades /
It is supplied from the inner diameter side to the optimal intermediate blade stage of the steam gas turbine, mixed with superheated steam, and directly reheats the superheated steam.
Also, for the upstream inner shaft device slightly higher than the combustion gas pressure,
A reheat cascade 60 is provided to increase the rotational power as reheat of superheated steam using the principle of spraying.

Most of the supplied heat energy is converted into superheated steam 5 for use in another application such as a steam turbine, and the steam containing the steam pipe 6 and the control device of the respective combustor / heat exchanger 4 is provided. Through the control valve 7, the outermost turbine blade group 1 stage 19 of the annular receiving port 23 downstream of the annular nozzle group 24 on the most upstream side of all the rotating blade / steam gas turbines of the annular combustion gas delivery portion 58 </ b> A. Injects and sequentially drives the downstream side as usual to generate a large rotation output. The superheated steam that has been supplied to the downstream side and has become wet steam is not limited to a combustion gas passage (a hole that applies the principle of atomization) provided in a suitable turbine blade of the inner turbine bucket group 20 as a cooling blade. Therefore, the combustion gas 10 is superheated by the combustion gas 10 by joining the combustion gas 10 at the optimum intermediate stage according to the combustion gas pressure, including the upstream reheating due to the reheating of the reheating cascade 60 that injects the combustion gas 10. Reheat steam directly. In addition, the combustion gas drives the rotor blades / steam gas turbine to obtain a rotational force without exceeding the heat-resistant limit temperature of the turbine, and at the same time, squirts the exhaust gas to inject the air in the right front to the left rear intensely. When the thrust is obtained, the rotational force is taken out using the inner shaft device as the output shaft 12. Therefore, various applications that require rotational force and levitation propulsion, such as for driving various machines and wheels, and various aircraft and ships such as helicopters and jets,
Various known control devices that are used for levitation and propulsion of something intermediate between an aircraft and a ship and that greatly increase thermal efficiency and propulsion efficiency with superheated steam whose pressure ratio is nearly 10 times that of conventional air compressors The core of a steam gas turbine united engine.

Referring to FIG. 1, another description will be given. The annular combustion gas delivery portion 58 and the annular compressed air receiving portion 61 are provided.
And the combustor / heat exchanger 4 is provided in a honeycomb shape so that the heat transfer area can be easily increased, and the lightweight high-pressure vessel can be easily provided with the fuel supply means 2.
7 is installed at the most upstream side, up to about four times that of the conventional technology. A magnetic friction power transmission device 14 is provided on each of the left and right sides of the center, an inner shaft device is fixedly mounted, and an outer compressor blade group final stage 16 and an outer turbine blade group 1 stage 19 provided annularly are provided on the outer circumference. The fixed outer shaft devices are rotatably fitted to the outer shaft devices, respectively, and are respectively rotated in opposite directions.
The shafts are connected at an optimum rotation ratio by a magnetic friction power transmission device 14, and the inner compressor blade group final stage 17 and the inner turbine blade group 2 stage 20 are fixed to the inner shaft device. The outer compressor blade group odd-numbered stage 16 is fixed to the outer compressor blade group odd-numbered stage 16, and the inner compressor blade group even-numbered stage 17 is fixed to the inner compressor blade group last stage 17. Then, the drive unit including the magnetic friction power transmission device, which transmits power most efficiently, constitutes a complete moving blade / compressor. Then, the outer turbine blade group odd-numbered stage 19 is fixed to the outer turbine blade group first stage 19 of the outer shaft device, and the inner turbine blade group even-numbered stage 20 is fixed to the inner turbine blade group second stage 20. The inner turbine blade group even-numbered final stage 20 is alternately fixed to the inner shaft device, and the outer turbine rotor blade group odd-numbered final stage 19 is fixed to the outer shaft device and rotatably fitted to the inner shaft device. Pivot, all blades
Configure a steam gas turbine.

Referring to FIG. 2, another description of the second embodiment of the core portion of the combined steam and gas turbine engine will be described. In the prior art, a large amount of heat energy is consumed and 80% of air compressed for combustion is used. %, The heat energy is wastefully reduced (by lowering the combustion temperature) and discharged, resulting in a large loss.
By making 00% effective use, the specific output is increased to the utmost and the thermal efficiency is greatly increased. That is, since the combustion gas as the working gas of the prior art gas turbine generally has a very high air ratio and contains air of about four times the stoichiometric air-fuel ratio, compressed air without exceeding the heat-resistant limit temperature of the turbine is obtained. In order to use 100% combustion, it is necessary to convert most of the supplied heat into superheated steam. Therefore, the present invention provides the combustor / heat exchanger 4 with an annular compressed air receiving portion 61 and an annular combustion gas sending portion 58.
Thus, the heat transfer heat exchange area is increased by providing a honeycomb structure, and it is easy to increase the pressure and fuel supply. As a result, most of the supplied heat can be converted to superheated steam, and at least one or more water cooling outer walls 26 are provided. A spiral welded structure including a plurality of water pipes 1 or an assembled structure of a spiral water-cooled outer wall unit 52 including a welded structure, enabling a large increase in pressure ratio and injection of superheated steam including supercritical, While greatly increasing the output,
Approximately all of the compressed air for combustion can be used effectively for combustion, and a bypass is provided for other uses that require compressed air, so that it is used separately.

Referring again to FIG. 2 and with reference to FIGS. 25-28, the outermost compressor blade group one stage 16 with the rightmost full blade compressor including the bypass 28 replaced, as usual. The air is sucked in, the even-numbered inner compressor blade group 17 and the odd-numbered outer compressor blade group 16 cooperate to efficiently compress the air by all the blades, and to use the compressed air for another purpose. Is supplied optimally from the bypass 28 passage provided appropriately according to the application. Compressed air for combustion is arranged in a honeycomb form from a rotatable and confidential annular outlet 21 of the all-blade compressor via an annular receiving port 22 of an annular compressed air receiving portion 61A. Is supplied to the combustor / heat exchanger 4. The supplied high compressed air is supplied from the fuel supply means 27 on the most upstream side of each of them, and is capable of performing agitated mixed combustion with the supplied fuel up to about four times that of the prior art. Thus, the combustion gas is heat-exchanged by performing combustion control combustion in the combustor / heat exchanger 4 in which the pressure of the combustion gas is increased and the heat exchange heat transfer area is expanded so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. The water-cooled outer wall 26 and the steam pipe 6 of each of the water pipes 1 make NOx reduction combustion as heat exchange cooling combustion gas. The superheated steam 5 obtained by exchanging heat so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature is passed through the steam control valve 7 of the respective combustor / heat exchanger 4 for another use such as a steam turbine. When used, the outer turbine blades replaced by the annular nozzle group 24 of the annular combustion gas delivery portion 58A rotatably inserted and rotatably inserted into the annular receiving port 23 of the full blade / steam gas turbine. Injects sequentially to the downstream side including the first stage 19 to generate large rotating power as usual.

The combustion gas 10 obtained by heat exchange so as to be lower than the heat-resistant limit temperature of the turbine is supplied from the respective combustor / heat exchanger 4 to the annular combustion gas reservoir 9 of the annular combustion gas delivery section 58. , Which is rotatably inserted and secured to an annular delivery portion 18A of the outer shaft device, and which is further rotatably secured to the annular delivery portion, and is provided with an annular delivery portion 18B of the inner shaft device. Will be supplied to The annular sending section 18
B, the rotational force is increased while reheating the superheated steam 5 and supplied to the inner diameter side optimal stage of the inner turbine bucket group 20 of the all buckets / steam gas turbine in accordance with the combustion gas pressure. The reheating cascade 60 of the inner turbine cascade that injects the combustion gas 10 by using the principle of spraying is provided on the side, and the reheating cascade 60 that directly reheats the superheated steam 5 is provided. The gas 10 is brought into direct contact with the superheated steam 5 to increase the rotational force and reheat, and the exhaust is strongly ejected to the left rear, and the air at the right front is ejected and moved strongly to the left rear to generate thrust, or The shaft unit is used as the output shaft 12 to take out the rotational force. It is the core of a combined rotor / steam gas turbine combined engine having various known control devices, and is used for many purposes in addition to the first embodiment.

Referring to FIG. 2, another description will be given. An annular combustion gas delivery portion 58 and an annular compressed air receiving portion 61 are provided, and the combustor / heat exchanger 4 arranged in a honeycomb shape is provided.
The respective inner shaft devices are connected to the inner left and right magnetic friction power transmission devices 14 at the center of the inner shaft device, and the outer compressor rotor blade group final stage 16 provided annularly on the left and right inner shaft devices. And the outer shaft device to which the outer turbine blade group 1 stage 19 is fixed is rotatably fitted on the outer shaft device so that the two shafts rotating in opposite directions to each other are rotated by the magnetic friction power transmission device 14 at an optimum rotation ratio. Husband and wife join. The final stage 17 of the inner compressor blade group and the second stage 20 of the inner turbine blade group are fixed to the respective inner shaft devices, and thereafter, the odd stage 16 of the outer compressor blade group and the even stage 17 of the inner compressor blade group are alternated thereafter. However, as a bypass for compressed air used for purposes other than combustion, it is fixed alternately, including the one with an enlarged outer diameter, to the outer compressor rotor blade group 1 stage 16
An outer shaft device is fixed to the inner shaft device, and the outer shaft device is rotatably fitted to the inner shaft device so as to be rotatably fitted to the outer shaft device, and is coupled at an optimum rotation ratio by the magnetic friction power transmission device 14 to drive the two blades most efficiently. Configure the machine. The odd numbered stages 19 of the outer turbine blade group are fixed to the first stage 19 of the outer turbine blade group, and the even number stages 20 of the inner turbine blade group are fixed to the second stage 20 of the inner turbine blade group. Then, the even-numbered final stage 20 of the inner turbine blade group is fixed to the inner shaft device, and the odd-numbered final stage 19 of the outer turbine blade group is fixed to the outer shaft device. , All buckets with bypass
Make up steam gas turbine

Referring to FIG. 3, a description will be given of a third embodiment of the core portion of the combined steam and gas turbine engine. The difference from the first embodiment of FIG. As the core of a steam gas turbine combined engine, the replacement rotor blades are reduced to conventional vanes, enabling the conventional compressor and the steam gas turbine of the present invention to be driven. That is, some changes are required, such as the annular combustion gas delivery section 58A being 58B and the annular compressed air receiving section 61A being 61B. Therefore, the elements from the first embodiment to the third embodiment in FIG. 1 are appropriately replaced with each other to be used for various purposes like the first embodiment, for example, for moving a vehicle and propelling a ship or an aircraft. To do.

Referring to FIG. 4, a fourth embodiment of the core portion of the combined steam and gas turbine engine will be described. The difference from the second embodiment of FIG. As the core of a steam gas turbine combined engine, the replacement rotor blades are reduced to conventional vanes, enabling the conventional compressor and the steam gas turbine of the present invention to be driven. That is, some changes are required, such as the annular combustion gas delivery section 58A being 58B and the annular compressed air receiving section 61A being 61B. Therefore, the elements from the first embodiment to the fourth embodiment in FIG. 1 are appropriately replaced with each other to be used for various purposes like the first embodiment, for example, for moving a vehicle and propelling a ship or an aircraft. To do.

Referring to FIG. 5, the welding structure of the means for increasing the heat exchange heat transfer area in which the combustor / heat exchanger 4 is arranged in a honeycomb shape will be described. (A), (b), (c), (d) ), The water-cooling outer wall 26 including at least one or more spiral water pipes 1 has a spiral welding structure, so that a large pressure ratio can be set and the heat exchange rate can be increased by increasing the heat transfer area. It facilitates acceleration and increases the most upstream side of the fuel supply means 27, and supplies combustion gas from the inside of the turbine cascade of the inner turbine bucket group 20 to make the entire steam gas turbine a reasonable cylindrical shape. . That is, as in the embodiments shown in (a) and (b), the combustor outer box part 25 is provided a little outward in the radial direction of the spirally provided water guide pipe 1, and one or more water guide pipes 1 are pivoted. Spiral welding, such as a T-shape, enables the combustor to be used in a high-pressure vessel, and also allows the heat transfer area of the combustor / heat exchanger 4 to be increased. Further, as in the embodiment shown in (c), a combustor outer box 25 is provided radially outward of the spirally provided water guide tube 1, and one or more water guide tubes 1 are welded in an axial spiral manner. This enables a large increase in the heat transfer area of the combustor / heat exchanger 4, which is significantly higher than the supercritical steam condition. or,
As in the embodiment shown in (d), a combustor outer box part 25 is provided at substantially the center in the radial direction of the spirally-arranged water guide tube 1, and one or more water guide tubes 1 are welded in an axial spiral manner. It enables a large increase in the heat transfer area of the combustor / heat exchanger 4 at a pressure ratio below the supercritical steam conditions and at a relatively high pressure.

Referring to FIGS. 5 and 6, the water-cooled outer wall unit 52 of the means for increasing the heat transfer area in which the combustor / heat exchanger 4 is arranged in a honeycomb shape will be described. FIGS. 6 (a) and 6 (b) As shown in (c), the water-cooled outer wall unit 52 including at least one or more spiral water pipes 1 is connected to a plurality of water-cooled outer wall units 52 as one unit that can be assembled by providing flanges 53 at both ends. It is the main part of the combustor / heat exchanger 4 that can greatly increase the pressure. That is, as in the embodiment shown in FIGS. 5A and 6B, the at least one or more spirally provided water pipes 1 are slightly separated outward in the radial direction, and the outside of the combustor including the welding structure is provided. A box 25 is provided, and flanges 53 are provided at both ends thereof.
The water pipes 1 are respectively opened in 3 so that the water-cooled outer wall unit 52 including the water pipe 1 can be connected. (C) (d)
As in the embodiment shown in (c), a combustor outer box part 25 including a welding structure is provided radially outward or at substantially the center in the radial direction of at least one or more water guide tubes 1 provided in a spiral shape. A flange 53 is provided at each end, and the water pipe 1 is opened at the flange 53 so that the water-cooled outer wall unit 52 including the water pipe 1 can be connected. Enables a large increase in the heat transfer area of the combustor / heat exchanger 4 with a relatively high pressure ratio.

Referring to FIG. 7 and FIG. 8, the magnetic friction power transmission device 14 will be described. Various power transmission devices including normal speed change and reverse rotation mainly use a gear device. For this reason, since a sliding tooth surface including a large load is essential for the tooth surface, in addition to requiring lubricating oil, friction heat loss is extremely large, and it is used for transmission of large power including high speed rotation. There is a problem of impossibility. For this reason, in order to commercialize an all-blade / steam gas turbine combined engine, an ultra-high-speed large power transmission device by rolling contact is indispensable. In order to
A power transmission device by rolling contact, which has almost no sliding tooth surface of the gear device, is required. For this reason, the meshing height of the gears is reduced as much as possible to provide a low unevenness 40, and a bar magnet 33 or an electromagnet 34 is provided as shown in FIG. For example, various magnetic friction power transmission devices 14 including various combinations of various magnetized friction wheels 37, 37 and various magnetic friction wheels 39, 39 of FIGS. 7 and 8 using the strong attraction force of the magnet. It is preferable to use it entirely. In other words, by bringing rolling contact closer, friction heat loss can be reduced to almost zero, and ultra-high-speed large-power transmission equipment and water-free cooling can be achieved in place of lubricating oil.

Referring to FIGS. 7, 8, and 9, the magnetic friction power transmission device 14 will be described. Instead of various gears, various types of magnetized friction wheels 37, 37 and various types of magnetic friction wheels 39, 39, etc. The power transmission surface 31 has a low unevenness 40, for example, a flat unevenness 41 car instead of a spur gear, a helical unevenness 42 car instead of a helical gear, and a Yamaha unevenness 4 instead of a yamaba gear.
Three cars will be provided. As a result, various magnetic friction power transmission devices 14 are configured and used as the magnetic friction power transmission device 14 in the same manner as known various gear type power transmission devices. As the special magnetic friction power transmission device 14, as shown in the embodiment of FIG. 9, the power transmission surfaces 31 of the main magnetized friction wheel 54, the forward magnetized friction wheel 55, and the reverse magnetized friction wheel 56 have low irregularities 40. Is established,
There is a forward / reverse switching device configuration in which electromagnets 34 are provided on the upstream and downstream sides in the rotation direction. In this embodiment, by reversing the current of the electromagnet 34, in addition to being able to switch between the forward rotation side and the reverse rotation side connection with a small amount of axial movement, the low unevenness 40 aims to significantly reduce the weight. A large diameter is possible, and a forward / reverse switching device with a simple structure and light weight and large specific output can be obtained. That is, since this technology can be applied in a wide variety of applications, it is significantly simpler in structure than conventional power transmission devices, and has a light weight and a large output. For practical use.

Referring to FIG. 10, a first embodiment of the combined steam gas turbine engine will be described. In the combined steam gas turbine engine for obtaining rotational power, the combustor / heat exchanger 4 is formed in a honeycomb shape depending on the application. The use of various means, such as an increase in the fuel supply means 27 and an increase in the heat transfer area, are added. That is, air is sucked and compressed as usual from the leftmost compressor,
The high-pressure compressed air 15 is supplied to the combustor / heat exchanger 4, and the high-pressure air and a fuel containing up to about four times that of the conventional technology are mixed and agitated so that the stoichiometric air-fuel ratio combustion can be performed. The superheated steam 5 obtained by heat exchange is injected through the steam control valve 7 from the most upstream side of the steam gas turbine to the downstream side so that the temperature is equal to or lower than the turbine heat-resistant limit temperature, thereby generating a rotational output. The combustion gas 10 obtained by the heat exchange is supplied to an optimal intermediate stage of a steam gas turbine to increase the output, and directly contact the superheated steam 5 to reheat the superheated steam to increase the output. Further, the exhaust gas is heat-exchanged and cooled by the exhaust heat recovery heat exchanger 49 and exhausted. The hot-water supply water and the water supply 3 obtained by the heat exchange are used as appropriate, but the exhaust itself is 100 ° C.
Since the low temperature is close to the above, a refuse incinerator 50 and a refuse incinerator heat exchanger 51 are provided to raise the temperature of the feed water 3 so that the water can be supplied to the combustor / heat exchanger 4 by the feed water pump 2 so that heat and electricity can be supplied. Various steam gas turbine combined engines used for co-supply facilities.

Referring to FIG. 11 and FIGS. 25 to 32, a first embodiment of a steam gas turbine combined engine having a control device will be described.
In various steam gas turbine combined engines, air is strongly sucked, combustion gas 10 and superheated steam 5 are strongly jetted to obtain a propulsive force or a levitation force, and various propellers are driven by a rotational force to levitate. Get power or propulsion, or superheated steam 5
1 to 4 and FIGS. 17 to 20 because it is necessary to obtain a propulsive force or a levitation force by injecting the combustion gas 10 strongly.
Up to the core of the combined steam gas turbine engine and the steam turbine compressor or steam turbine shown in Figs. 21 to 24. Various power transmission devices not shown in the figure will switch from the use of normal various power transmission devices, including auxiliary equipment, to the development and use of various magnetic friction power transmission devices 14 sequentially. Therefore, it is common practice to use various steam gas turbine combined engines using various known control devices.

Referring to FIG. 12 and FIGS. 25 to 32, a second embodiment of a steam gas turbine combined engine having a control device will be described. In the engine, the combustion gas 10 and the superheated steam 5 are strongly injected by strongly sucking the air, and the hull is levitated to obtain the propulsion, and at the same time, the various propellers are driven by the rotational force to obtain the propulsion. 1 or 4 and FIGS. 17 and 2 because it is necessary to inject the superheated steam 5 and the combustion gas 10 strongly to obtain the propulsion force while floating the hull.
0 and the core of the steam gas turbine combined engine up to 0
Use the steam turbine compressor or steam turbine shown in Fig.24. Various power transmission devices not shown in the figure will switch from the use of normal various power transmission devices, including auxiliary equipment, to the development and use of various magnetic friction power transmission devices 14 sequentially. Therefore, it is common practice to use various steam gas turbine combined engines using various known control devices.

Referring to FIG. 13 and FIGS. 25 to 32, a third embodiment of a combined steam gas turbine engine having a control device will be described. In any of the combined steam gas turbine combined engines, it is necessary to inject superheated steam and combustion gas to obtain rotational power. Therefore, the core of the combined steam gas turbine combined engine shown in FIGS. 1 to 4 and FIGS. Then, the rotational power is taken out from the output shaft 12 by using the steam turbine shown in FIGS. Various power transmission devices not shown include various types of magnetic friction power transmission devices 14 starting from the use of normal various power transmission devices, including reverse rotation and shifting, including auxiliary equipment.
Although it is common practice to use a control device when using any of these, a combined steam gas turbine engine using various known control devices will be used.

Referring to FIG. 14 and FIGS. 25 to 32, a fourth embodiment of a combined steam and gas turbine engine having a control device will be described. In the various steam gas turbine combined engines used for various aircraft and ships to obtain power, it is necessary to inject superheated steam 5 and combustion gas 10 to obtain rotational power and propulsion or levitation. Rotation power is taken out from the output shaft 12 by using the core of the combined steam gas turbine engine shown in FIGS. 1 to 4 and FIGS. 17 to 20 and the steam turbine shown in FIGS. Various power transmission devices not shown in the figure will switch from the use of normal various power transmission devices, including reversing and shifting including auxiliary equipment, to the development and use of various magnetic friction power transmission devices 14 in sequence. In this case, it is common sense to use a control device. Therefore, a combined steam gas turbine engine using various known control devices will be used.

Referring to FIG. 15 and FIGS. 25 to 32, a fifth embodiment of the combined steam / gas turbine engine having a control device will be described. In any of the combined steam gas turbine combined engines used, it is necessary to inject the superheated steam 5 and the combustion gas 10 to obtain rotational power, so that the combined steam gas turbine combination shown in FIGS. 1 to 4 and FIGS. Rotation power is taken out from the output shaft 12 using the engine core and the steam turbine shown in FIGS. Various power transmission devices not shown in the figure will switch from the use of normal various power transmission devices, including reversing and shifting including auxiliary equipment, to the development and use of various magnetic friction power transmission devices 14 in sequence. In this case, it is common sense to use a control device. Therefore, a combined steam gas turbine engine using various known control devices will be used.

Referring to FIG. 16, FIGS. 10, 28 and 3
The steam-gas-turbine combined engine having a control device according to a sixth embodiment will be described with reference to FIG. In all types of steam gas turbine combined engines, while injecting superheated steam and combustion gas to obtain rotational power,
Since it is necessary to use exhaust heat, FIGS. 1 to 4 and FIG.
7 to 20 and the steam turbine of FIG. 21 to FIG. 24 are used to drive a generator from each output shaft 12 to supply electricity.
Using the one with the waste heat recovery heat exchanger 49 like
Used to supply both heat and electricity for hot water supply. Various power transmission devices not shown in the figure will switch from the use of normal various power transmission devices, including auxiliary equipment, to the development and use of various magnetic friction power transmission devices 14 sequentially. Therefore, it is common practice to use various steam gas turbine combined engines using various known control devices.

Referring to FIGS. 17 to 20, FIGS. 29 to 32, and FIG.
The fifth to eighth embodiments of FIGS. 7 to 20 will be described.
4 to FIG. 4 are different from the first to fourth embodiments.
In the combustor / heat exchanger using a steam gas turbine as a gas turbine, by using all of the superheated steam 5 obtained by exchanging heat without exceeding the heat-resistant limit temperature of the turbine in a portion other than the core portion such as a steam turbine, At the core of the steam gas turbine combined engine, the output is obtained using only the combustion gas 10. Accordingly, in the first to fourth embodiments and the fifth to eighth embodiments, the respective annular combustion gas delivery sections 58 are also changed to those for the gas turbine. 1 to 4 and FIG.
The elements from the first embodiment to the eighth embodiment shown in FIGS. 7 to 20 are appropriately replaced with each other to provide various applications, such as moving various vehicles, various ships, various aircraft, and various rockets. Used for propulsion and driving various machines.

Referring to FIG. 17, a fifth embodiment of the core portion of the combined steam and gas turbine engine will be described with reference to FIGS. 29 to 32. The difference from the first embodiment of FIG. The superheated steam 5 obtained by exchanging heat without exceeding the heat-resistant limit temperature of the turbine in the combustor / heat exchanger 4 using the steam gas turbine as an all-blade gas turbine is used in a portion other than the core such as the steam turbine. By doing so, in the core of the combined steam gas turbine engine, the output is obtained using only the combustion gas 10. Accordingly, in the fifth embodiment, the annular combustion gas delivery section 58A of the first embodiment is also an annular combustion gas delivery section 58C for an all-blade gas turbine, and is changed to an all-blade gas turbine. That is, the elements from the first embodiment to the eighth embodiment are appropriately replaced with each other, and are used for various purposes such as moving various vehicles and propelling various ships, various aircrafts and various rockets. Also used for driving various machines.

Referring to FIG. 18 and FIGS. 29 to 32, the sixth embodiment of the core portion of the combined steam and gas turbine engine will be described. The difference from the fifth embodiment of FIG. Because a large amount of heat energy is consumed and the air compressed for combustion is exhausted without using nearly 80% of the air, it is wasted and a large loss occurs, so 100% of the compressed air for combustion can be used effectively for combustion. In addition, the compressed air 15 used for purposes other than the combustion is provided with a bypass 28 and used separately. By using a bypass-added all-blade compressor, the specific output is increased to the utmost and the thermal efficiency is greatly increased. is. Therefore, except for the bypass 28, the fifth and sixth embodiments are the same. That is, the elements from the first embodiment to the eighth embodiment are appropriately replaced with each other, and are used for various purposes such as moving various vehicles and propelling various ships, various aircrafts and various rockets. Also used for driving various machines.

Another embodiment of the sixth embodiment will be described with reference to FIG. 18. The combustor / heat exchanger is provided with an annular combustion gas delivery section 58 and an annular compressed air receiving section 61 and arranged in a honeycomb shape. 4 and the inner shaft device is connected to the inner left and right magnetic friction power transmission devices 14 at the center of the inner shaft device, respectively.
An outer shaft device in which an outer compressor blade group final stage 16 and an outer turbine blade group 1 stage 19, which are provided in a ring shape, are fixed to the left and right inner shaft devices so as to be rotatably fitted on the outer shaft device. The two shafts rotating in opposite directions are connected to the magnetic friction power transmission device 1.
4, and the final stage 17 of the inner compressor blade group and the second stage 20 of the inner turbine blade group are fixed to the respective inner shaft devices, and thereafter the odd number stage of the outer compressor blade group is fixed. 16
And the even-numbered stage 17 of the inner compressor blade group are alternately fixed, but as a compressed air bypass used for purposes other than combustion,
The outer shaft device is fixed to the first stage 16 of the outer compressor rotor blades alternately, and the outer shaft device is rotatably fitted to the inner shaft device. By combining with the optimal rotation ratio, it makes up a full-blade compressor that drives the two shafts most efficiently. The odd numbered stages 19 of the outer turbine blade group are fixed to the first stage 19 of the outer turbine blade group, and the even number stages 20 of the inner turbine blade group are fixed to the second stage 20 of the inner turbine blade group. Then, the even-numbered final stage 20 of the inner turbine blade group is fixed to the inner shaft device, and the odd-numbered final stage 19 of the outer turbine blade group is fixed to the outer shaft device. The sixth embodiment of the core of the steam-gas-turbine combined engine with all blades with bypass added.

A seventh embodiment of the core portion of the combined steam and gas turbine engine will be described with reference to FIG. 19 and FIGS. 29 to 32. The difference from the fifth embodiment of FIG. 17 is that the replacement rotor blade is reduced to a stationary blade of the prior art by using the core portion of the combined blade and steam gas turbine combined engine as the core portion of the combined steam gas turbine engine, and As a combustor / heat exchanger 4 provided with a compressed air receiving portion 61D and an annular combustion gas sending portion 58D, a conventional compressor and gas turbine can be driven.
Therefore, the elements from the first embodiment to the eighth embodiment in FIG. 1 are appropriately replaced with each other, and for various purposes, for example, movement of various vehicles and various ships, various aircraft, and various rockets. Used for propulsion and driving various machines.

Referring to FIG. 19 and FIG. 32, which are close to a steam / gas turbine combined cycle thermal power generation facility, a case where it is used as a state-of-the-art thermal power generation facility will be described in comparison with the prior art. In the case where the generator is driven in the seventh embodiment using the conventional gas turbine of FIG. 19, an annular combustion gas sending section 58 and an annular compressed air receiving section 61 are provided, and the combustor / heat exchanger 4 is formed in a honeycomb shape. To enable various heat exchanges with a greatly increased pressure ratio according to the application, with the same amount of compressed air for combustion up to about four times the fuel combustion of the conventional technology and a greatly increased combustion gas mass. Enables a significant increase in output and significantly lower temperature exhaust. As for the comparison of pressure ratios, the temperature of the combustion gas 10 can be significantly reduced by heat exchange, so the pressure ratio can be increased to the utmost and the thermal efficiency can be increased. In addition, in order to perform heat exchange with the pressure ratio raised to the limit, the amount of superheated steam energy including supercritical steam conditions extracted from the combustion gas is also compared with the amount of heat energy in the conventional heat recovery heat exchange. It will be too much. Furthermore, since the gas turbine is driven by the combustion gas 10 that has undergone heat exchange with the pressure ratio raised to the limit, the amount of exhaust heat can be minimized. That is,
The greater the pressure ratio, the higher the thermal efficiency of the gas turbine, the greater the mass of the combustion gas, the greater the output of the gas turbine. The higher the output of the steam turbine, the greater the overall thermal efficiency.

Referring to FIG. 20, a description will be given of an eighth embodiment of the core portion of the combined engine of the steam and gas turbine. The difference from the sixth embodiment shown in FIG. 18 is that the core portion of the combined rotor / steam gas turbine engine is used as the core portion of the combined steam gas turbine engine, and the replacement rotor blades are reduced to the stationary blades of the prior art to reduce the combustor. As a combustor / heat exchanger 4 provided with an annular compressed air receiving portion 61D and an annular combustion gas sending portion 58D, a conventional compressor and gas turbine can be driven. Therefore, the first of FIG.
The elements from the embodiment to the eighth embodiment are appropriately replaced with each other, and for various purposes, for example, for the movement of various vehicles and for the propulsion of various ships, various aircraft and various rockets, and the various types of machinery. Used for driving etc.

Referring to FIG. 21, a first embodiment of a full blade / steam turbine compressor will be described. The superheated steam 5 obtained by exchanging heat in the core of various steam gas turbine combined engines drives the all-blade steam turbine to generate torque, which is used as rotational power by the output shaft 12 at the left end. Or
The rotating blade compressor is rotated by the rotating force to obtain high compressed air or high-speed airflow, and to obtain rotating force, thrust and levitation force. Accordingly, the superheated steam 5 obtained by exchanging heat in the core portion of the combined steam gas turbine engine is used to convert the superheated steam 5 to the steam control valve 7.
The steam is transferred to the most upstream side of the all-blade steam turbine by the steam pipe 6 to drive the most upstream side and sequentially drive the downstream side to generate a large rotational power and to transmit the magnetic friction power at the left end. The device 14 couples the outer turbine blade group 19 and the outer shaft device rotating in opposite directions to the inner turbine blade group 20 and the inner shaft device at an optimum rotation ratio, and is used for an application requiring a rotational force. You. Further, the right end compressor-side magnetic friction power transmission device 14 optimally reverses the inner compressor blade group 17 and the inner shaft device also serving as the turbine outer shaft device, and the outer compressor blade group 16 and the outer shaft device. The first embodiment of a full-blade steam turbine compressor is shown in FIG. 26, which is used for high pressure gas or high-speed gas.
It is used for various steam gas turbine united engines shown in FIG.

Referring to FIG. 22, a second embodiment of the all blade / steam turbine compressor will be described. The superheated steam 5 obtained by exchanging heat in the core of various steam gas turbine combined engines drives the all-blade steam turbine to generate torque, which is used as rotational power by the output shaft 12 at the left end. Or
By rotating the full blade compressor shown in Fig. 22 by the rotational force, high compressed air or high-speed airflow is obtained, and rotational force, thrust, levitation, etc. are obtained. Therefore, the superheated steam 5 obtained by heat exchange in the core part of the combined steam gas turbine engine is conveyed to the most upstream side of the all-blade steam turbine by the steam pipe 6 through the steam control valve 7 and the most upstream side is Driving and sequentially driving the downstream side to generate large rotational power,
The leftmost magnetic frictional power transmission device 14 connects the outer turbine rotor blade group 19 and the outer shaft device rotating in opposite directions to the inner turbine rotor blade group 20 and the inner shaft device at an optimum rotation ratio, and Used for applications that require rotational power by configuring a steam turbine. Furthermore, the rightmost compressor-side magnetic friction power transmission device 14 causes the inner compressor rotor blade group 1 to move.
7 and the inner shaft device, the outer compressor blade group 16 and the outer shaft device are combined at an optimum contra-rotating rotation ratio to form a full blade compressor, and a second embodiment of the full blade steam turbine compressor is constructed. The invention is used for applications utilizing high-pressure gas or high-speed gas. In the present invention, it is used for various steam gas turbine combined engines shown in FIGS.

Referring to FIG. 23, a third embodiment of the steam turbine compressor will be described. The superheated steam 5 obtained by exchanging heat at the core of various steam gas turbine combined engines drives the steam turbine to generate rotational force, which is used as rotational power by the output shaft 12. Alternatively, the compressor shown in FIG. 23 is rotated by the rotational force to obtain high compressed air or high-speed airflow, and obtains rotational force, thrust, levitation, and the like. Therefore, the superheated steam 5 obtained by exchanging heat in the core portion of the combined steam gas turbine engine is supplied from the steam control valve 7 to the steam pipe 6 through the steam control valve 7.
It is conveyed to the most upstream side of the steam turbine, drives the most upstream side and sequentially drives the downstream side to generate a large rotational power, and the outer turbine blade group 19 which is opposite to the normal one.
And by rotating the outer shaft device, the superheated steam 5 which has become wet steam or water droplets can be ejected outward by centrifugal force, and the propulsion force is increased as the mass of the compressed air flow is increased,
It is externally fitted to the inner fixed shaft device at the left end, and the left end of the outer shaft device is used as an output shaft 12 to constitute a steam turbine, which is used for applications requiring torque. The right end of the inner turbine vane and the inner fixed shaft device is fixed by a horizontal joint of a casing, and the casing is fixed to the inner compressor rotor group 1.
The third embodiment of the steam turbine compressor is used for applications utilizing high-pressure gas or high-speed gas. The present invention is used for the various steam gas turbine combined engines shown in FIGS.

Referring to FIG. 24, a fourth embodiment of the steam turbine compressor will be described. The superheated steam 5 obtained by exchanging heat at the core of various steam gas turbine combined engines drives the steam turbine to generate rotational force, which is used as rotational power by the output shaft 12. Alternatively, the compressor of the prior art shown in FIG. 24 is rotated by the rotational force to obtain high compressed air or high-speed airflow, and obtains rotational force, thrust, levitation, and the like. Therefore, the superheated steam 5 obtained by heat exchange in the core part of the combined steam gas turbine engine is conveyed to the most upstream side of the known steam turbine through the steam pipe 6 from the steam control valve 7 and the reheated steam is sent as usual. An application that drives the upstream side and sequentially drives the downstream side to generate a large rotational power, and configures a steam turbine that takes out the rotational force by using the left end of the inner shaft device as the output shaft 12 and uses the rotational force. Used for That is, the stationary blade is fixed to a casing that can be disassembled and assembled with a horizontal joint on the outer side of the inner turbine rotor blade group 20 and the inner shaft device, and a steam turbine is configured by externally fitting and pivoting. Similarly, outside the inner compressor rotor blade group 17 and the inner shaft device, a casing to which the stationary vanes are fixed is fitted and pivoted to form a compressor. As a fourth embodiment of the steam turbine compressor, a high pressure It is used for applications that use gas or high-speed gas. In the present invention, it is used for various steam gas turbine combined engines shown in FIGS.

Referring to FIG. 25, a second embodiment of the combined steam and gas turbine engine will be described. In the core part of the combined engine of various steam gas turbines, air is sucked and compressed by various compressors including all the moving blades, and the highly compressed air 15 is supplied to the combustor / heat exchanger 4 to at most the conventional art. A part of the superheated steam 5 obtained by burning the fuel including about 4 times the fuel and the stoichiometric air-fuel ratio combustion and exchanging heat without the combustion gas 10 temperature exceeding the heat-resistant limit temperature of the turbine, It is supplied to the most upstream side of the steam gas turbine to obtain output, and most of the heat energy is converted to superheated steam 5 and used for various devices and machines that require superheated steam 5. For example, when the rocket is used as a rocket, it is accelerated in the air as much as possible by the thrust of various steam gas turbines, and a supercritical steam reservoir 30 in which one or more water pipes 1 are provided in a spiral honeycomb shape is supercritical. Circulates and accumulates heat energy of the superheated steam 5 containing the steam, and the shutoff valves 13 provided for the shutoff and the cutoff.
・ Separate between 13 at the optimal time, and thereafter, open the shut-off valve 13 provided for thrust generation appropriately and inject superheated steam 5 from the injection port 29 to make the rocket capable of accelerated flight in vacuum.

Referring to FIG. 26, a third embodiment of the combined steam and gas turbine engine will be described. In the core part of the combined engine of various steam gas turbines, air is sucked and compressed by various compressors including all the moving blades, and the highly compressed air 15 is supplied to the combustor / heat exchanger 4 to at most the conventional art. A part of the superheated steam 5 obtained by performing the heat exchange with the fuel of about four times and the stoichiometric air-fuel ratio including the stoichiometric air-fuel ratio without exceeding the heat-resistant temperature of the turbine through the steam control valve 7 is obtained. The steam is supplied to the most upstream side of various steam gas turbines, including all the moving blades, to obtain an output. Most of the heat energy is converted to superheated steam 5 and is separately used through the steam control valve 7 of each of them. It is used for various steam turbines including all moving blades that require superheated steam 5 and various steam turbine compressors including all moving blades.
The combustion gas 10 obtained by heat exchange without the combustion gas temperature exceeding the heat-resistant limit temperature of the turbine is supplied to the optimum intermediate stage of various steam gas turbines including all the moving blades according to the pressure, and the output is reduced. As the output increases by directly reheating the superheated steam 5 to increase the output, and as a third embodiment of the combined steam and gas turbine engine, various applications utilizing the thrust of various steam gas turbines and various steam turbine compressors, such as various Used for levitation promotion of ships and various aircraft.

Referring to FIG. 27, a fourth embodiment of the combined steam and gas turbine engine will be described. In the core part of the combined engine of various steam gas turbines, air is sucked and compressed by various compressors including all the moving blades, and the highly compressed air 15 is supplied to the combustor / heat exchanger 4 to at most the conventional art. A part of the superheated steam 5 obtained by performing the heat exchange with the fuel of about four times and the stoichiometric air-fuel ratio including the stoichiometric air-fuel ratio without exceeding the heat-resistant temperature of the turbine through the steam control valve 7 is obtained. The steam is supplied to the most upstream side of various steam gas turbines, including all the moving blades, to obtain an output. Most of the heat energy is converted to superheated steam 5 and is separately used through the steam control valve 7 of each of them. It is used for various steam turbines including all moving blades that require superheated steam 5 and various steam turbine compressors including all moving blades.
The combustion gas 10 obtained by heat exchange without the combustion gas temperature exceeding the heat-resistant limit temperature of the turbine is supplied to the optimum intermediate stage of various steam gas turbines including all the moving blades according to the pressure, and the output is reduced. As the output increases, the superheated steam 5 is directly reheated to increase the output. Various steam gas turbines each having an output shaft 12 and various steam turbine compressors are used as a fourth embodiment of a steam gas turbine united engine. It is used for various purposes that use the rotational and thrust forces of gas turbines and various steam turbine compressors, for example, for moving various vehicles and driving various machines, and for floating propulsion of various ships and various aircraft.

Referring to FIG. 28, a fifth embodiment of the combined steam and gas turbine engine will be described. In the core part of the combined engine of various steam gas turbines, air is sucked and compressed by various compressors including all the moving blades, and the highly compressed air 15 is supplied to the combustor / heat exchanger 4 to at most the conventional art. A part of the superheated steam 5 obtained by performing the heat exchange with the fuel of about four times and the stoichiometric air-fuel ratio including the stoichiometric air-fuel ratio without exceeding the heat-resistant temperature of the turbine through the steam control valve 7 is obtained. The steam is supplied to the most upstream side of various steam gas turbines, including all the moving blades, to obtain an output. Most of the heat energy is converted to superheated steam 5 and is separately used through the steam control valve 7 of each of them. It is used for various steam turbines, including all moving blades that require superheated steam 5. The combustion gas 10 obtained by heat exchange without the combustion gas temperature exceeding the heat-resistant limit temperature of the turbine is supplied to the optimum intermediate stage of various steam gas turbines including all the moving blades according to the pressure, and the output is reduced. Superheated steam 5
Are directly reheated to increase the output, and a steam generator and an electric motor are provided as various steam gas turbines and steam turbines each having the output shaft 12, respectively. The fifth embodiment of the present invention is used for various purposes utilizing the rotational force of various steam gas turbines and various steam turbines, for example, for moving various vehicles, driving various machines, various power generation, and propulsion of various ships and various aircraft. Used for etc.

Referring to FIG. 29, a sixth embodiment of the combined steam and gas turbine engine will be described. In the core part of the combined engine of various steam gas turbines, air is sucked and compressed by various compressors including all the moving blades, and the highly compressed air 15 is supplied to the combustor / heat exchanger 4 to at most the conventional art. Combustion including about four times the fuel and stoichiometric air-fuel ratio combustion, and all of the combustion gas 10 obtained by heat exchange without causing the combustion gas 10 temperature to exceed the heat-resistant limit temperature of the turbine are converted to various gases including all rotor blades. It is supplied to the most upstream side of the turbine to obtain output, and most of the heat energy is converted to superheated steam 5 and used for various devices and machines that require superheated steam 5. For example, when the rocket is used as a rocket, it is accelerated in the air as much as possible by the thrust of various gas turbines, and the superheated steam reservoir 30 in which one or more water guide tubes 1 are provided in a spiral honeycomb shape is provided.
Circulating and storing the thermal energy of the superheated steam 5 including the supercritical fluid so that the valve can be closed and separated.
3 at an optimum time, and thereafter, the closing valve 13 provided for generating thrust is opened appropriately, and the superheated steam 5
To make a rocket capable of accelerating flight in a vacuum.

Referring to FIG. 30, a seventh embodiment of the combined steam and gas turbine engine will be described. In the core part of the combined engine of various steam gas turbines, air is sucked and compressed by various compressors including all the moving blades, and the highly compressed air 15 is supplied to the combustor / heat exchanger 4 to at most the conventional art. All of the superheated steam 5 obtained by performing the heat exchange with the fuel of about 4 times and the stoichiometric air-fuel ratio combustion and the combustion gas 10 not exceeding the heat-resistant limit temperature of the turbine through the steam control valve 7 is obtained. To obtain thrust by supplying to the most upstream side of various steam turbines including all rotor blades,
Or use it for various steam turbine compressors including all rotors and use the thrust of each husband and wife. Combustion gas 10 obtained by heat exchange without the combustion gas temperature exceeding the heat-resistant limit temperature of the turbine
Are supplied to the most upstream side of various gas turbines including all the moving blades to generate and increase the output, and also to inject the exhaust gas to generate and increase the thrust or the levitation force. As an example, it is used for various purposes utilizing the thrust of various gas turbines and various types of steam turbine compressors, for example, for levitation propulsion of various ships and various aircraft.

Referring to FIG. 31, an eighth embodiment of the combined steam and gas turbine engine will be described. In the core part of the combined engine of various steam gas turbines, air is sucked and compressed by various compressors including all the moving blades, and the highly compressed air 15 is supplied to the combustor / heat exchanger 4 to at most the conventional art. All of the superheated steam 5 which is burned including about four times the fuel and the stoichiometric air-fuel ratio combustion and heat-exchanged without the temperature of the combustion gas 10 exceeding the heat-resistant limit temperature of the turbine is transferred to the respective steam control valves 7 and 7. It is used for various steam turbine compressors including all the moving blades that require superheated steam 5 to generate and increase the thrust and torque of each of them. All of the combustion gas 10 obtained by heat exchange without causing the combustion gas temperature to exceed the heat-resistant limit temperature of the turbine is supplied to the most upstream side of various gas turbines including all the moving blades, and the rotational force and thrust are generated and increased. In addition, as the various gas turbines and the various steam turbine compressors each having the output shaft 12, the eighth embodiment of the combined steam and gas turbine engine is adopted, and the rotational force and thrust of the various steam gas turbines and the various steam turbine compressors are adjusted. It is used for various purposes such as moving various vehicles and driving various machines, and for levitation propulsion of various ships and various aircraft.

Referring to FIG. 32, a ninth embodiment of the combined steam and gas turbine engine will be described. In the core part of the combined engine of various steam gas turbines, air is sucked and compressed by various compressors including all the moving blades, and the highly compressed air 15 is supplied to the combustor / heat exchanger 4 to attain the conventional technology. All of the superheated steam 5 which is burned including about four times the fuel and the stoichiometric air-fuel ratio combustion and heat-exchanged without the temperature of the combustion gas 10 exceeding the heat-resistant limit temperature of the turbine is transferred to the respective steam control valves 7 and 7. It is used for various steam turbines including all the moving blades that require superheated steam 5 as a separate use. All of the combustion gas 10 obtained by heat exchange without the combustion gas temperature exceeding the heat-resistant limit temperature of the turbine is supplied to the most upstream side of various gas turbines including all the moving blades to generate and increase the rotational force. A generator or an electric motor is provided as each of the various gas turbines and the various steam turbines having the output shaft 12, and a ninth of the steam gas turbine combined engine is provided as a large power generation facility or a starting device.
As an example, it is used for various purposes utilizing the rotational force of various gas turbines and various steam turbines, for example, for moving various vehicles, driving various machines, various power generation, propulsion of various ships and aircraft, etc. .

[0052]

According to the present invention, the outer wall of a combustor / heat exchanger is formed as a core portion of a combined steam and gas turbine engine including all rotor blades, and a spiral welding structure including a water pipe or a spiral structure including a welding structure. Since the water-cooled outer wall unit assembly structure is arranged in a honeycomb shape, the outer shape of the core of the combined steam and gas turbine engine can be easily expanded as an ideal cylindrical shape, and it has a great effect of being compact. In addition, as a combustor / heat exchanger for a high-pressure vessel with a greatly increased heat transfer area, the fuel supply means can be easily added to the most upstream side up to four times that of the conventional technology, and the majority of the supplied heat can be converted to superheated steam. It has an effect. When the rotating power is obtained by the combustion gas and the superheated steam obtained by exchanging heat without exceeding the heat-resistant limit temperature of the turbine, and the amount of compressed air for combustion is the same as that of the conventional technology, the maximum of the conventional gas turbine is 4%. It has the effect that the heat output can be greatly increased and the specific output greatly increased up to stoichiometric air-fuel ratio combustion with about twice the fuel. 100% compressed air for combustion
It can be used for combustion and can inject superheated steam at a pressure close to 10 times the normal pressure ratio and less than the supercritical pressure. As a result, the combined cycle of various steam gas turbines with the highest thermal efficiency has a great effect on greatly increasing the thermal efficiency.

The most important feature of the present invention is that the gas turbine, the steam turbine, and the steam gas turbine can be optimally used, so that the thermal efficiency of the most advanced thermal power generation equipment most commonly used in the world is maximized. It is a place that can be used in a wide variety. In other words, the gas turbine pressure ratio of the steam / gas turbine combined cycle can be raised to the limit by heat exchange combustion gas cooling, and the thermal efficiency of the gas turbine can be raised to the limit. In addition, since heat is exchanged with the pressure ratio raised to the limit, the amount of superheated steam energy including supercritical steam conditions can be increased to increase the total specific output and thermal efficiency to the limit. Furthermore, since heat is exchanged with the pressure ratio raised to the limit, the heat consumption of the gas turbine is minimized, the combustion gas mass is maximized, and the thermal efficiency can be increased to the limit. Furthermore, the use of combustion gas that has undergone heat exchange while the pressure ratio has been raised to the maximum has the effect of minimizing the exhaust heat of the gas turbine and making the most of thermal energy. In addition, the development and use of various magnetic friction power transmission devices has the effect of greatly reducing the frictional heat loss caused by the various power transmission devices of the prior art and further increasing the thermal efficiency. Therefore, it is very effective to reduce CO2 on a global scale by using it variously as various transportation equipment and co-supply equipment of heat and electricity.

[Brief description of the drawings]

FIG. 1 is a partial cross-sectional view showing a first embodiment of a core portion of a combined steam gas turbine engine.

FIG. 2 is a partial cross-sectional view showing a second embodiment of the core part of the steam gas turbine combined engine.

FIG. 3 is a partial cross-sectional view showing a third embodiment of a core portion of a combined steam gas turbine engine.

FIG. 4 is a partial cross-sectional view showing a fourth embodiment of the core portion of the combined steam gas turbine engine.

FIG. 5 is a cross-sectional view showing a spiral welding structure of a water-cooled outer wall of the combustor / heat exchanger.

FIG. 6 is a sectional view for explaining a spiral water cooling wall tube unit of the combustor / heat exchanger.

FIG. 7 is a conceptual diagram of a magnetic friction power transmission device for a steam gas turbine combined engine.

FIG. 8 is a diagram for explaining friction increasing means such as a magnetic friction wheel and a magnetic friction wheel.

FIG. 9 is a view for explaining a special embodiment of the magnetic friction power transmission device.

FIG. 10 is an overall configuration diagram showing a first embodiment of the combined steam gas turbine engine.

FIG. 11 is an overall configuration diagram showing a first embodiment of the steam gas turbine combined engine.

FIG. 12 is an overall configuration diagram showing a second embodiment of the combined steam gas turbine engine.

FIG. 13 is an overall configuration diagram showing a third embodiment of the steam gas turbine combined engine.

FIG. 14 is an overall configuration diagram showing a fourth embodiment of the combined steam gas turbine engine.

FIG. 15 is an overall configuration diagram showing a fifth embodiment of the combined steam gas turbine engine.

FIG. 16 is an overall configuration diagram showing a sixth embodiment of the combined steam gas turbine engine.

FIG. 17 is a partial cross-sectional view showing a fifth embodiment of the core part of the combined steam gas turbine engine.

FIG. 18 is a partial cross-sectional view showing a sixth embodiment of the core portion of the combined steam gas turbine engine.

FIG. 19 is a partial cross-sectional view showing a seventh embodiment of the core of the steam gas turbine combined engine.

FIG. 20 is a partial cross-sectional view showing an eighth embodiment of the core portion of the combined steam gas turbine engine.

FIG. 21 is a partial sectional view showing a first embodiment of the steam turbine compressor.

FIG. 22 is a partial sectional view showing a second embodiment of the steam turbine compressor.

FIG. 23 is a partial sectional view showing a third embodiment of the steam turbine compressor.

FIG. 24 is a partial sectional view showing a fourth embodiment of the steam turbine compressor.

FIG. 25 is an overall configuration diagram showing a second embodiment of the combined steam gas turbine engine.

FIG. 26 is an overall configuration diagram showing a third embodiment of the steam gas turbine combined engine.

FIG. 27 is an overall configuration diagram showing a fourth embodiment of the combined steam gas turbine engine.

FIG. 28 is an overall configuration diagram showing a fifth embodiment of the combined steam gas turbine engine.

FIG. 29 is an overall configuration diagram showing a sixth embodiment of the combined steam gas turbine engine.

FIG. 30 is an overall configuration diagram showing a seventh embodiment of the combined steam and gas turbine engine.

FIG. 31 is an overall configuration diagram showing an eighth embodiment of the steam gas turbine combined engine.

FIG. 32 is an overall configuration diagram showing a ninth embodiment of the combined steam gas turbine engine.

[Explanation of symbols]

1: water pipe 2: water supply pump 3: water supply 4: combustor and heat exchanger 5: superheated steam 6: steam pipe
7: Steam control valve 8: Annular compressed air reservoir 9: Annular combustion gas reservoir 10 Combustion gas 12: Output shaft 1
3: Stop valve 14: Magnetic friction power transmission device 15:
Compressed air 16: Outer compressor rotor blade group 17: Inner compressor rotor blade group 18: Annular sending section 1
9: Outer turbine bucket group 20: Inner turbine bucket group 21: Annular outlet 2
2: Annular socket 23: Annular socket 24: Annular nozzle group 25:
Combustor outer box 26: Water-cooled outer wall 27: Fuel supply means 28: Bypass 29: Injector 30: Superheated steam reservoir 31: Power transmission surface 33: Bar magnet 34:
Electromagnet 35: Direction of rotation 36: Magnetic pole 37: Magnetized friction wheel 38: Inner magnetized friction wheel 39: Magnetically attached friction wheel 40: Low irregularity 41: Flat irregularity 42: Husuba irregularity 43: Yamaba irregularity 44: Internal magnetized friction wheel 4
5: friction increasing durability means 46: magnet part 47: yoke (for magnetized friction wheel) 48: insulating material 49: waste heat recovery heat exchanger 50: refuse incinerator 51: refuse incinerator heat exchanger 52: water cooling outer wall unit 53: Tsuba 54:
Main magnetized friction wheel 55: Forward magnetized friction wheel 56: Reverse magnetized friction wheel 58: Annular combustion gas delivery section 6
0: Reheat cascade 61: Annular compressed air receiving section

Claims (162)

[Claims] An annular compressed air receiving portion (61) and an annular combustion gas sending portion (5) having a water-cooled outer wall having a spiral welding structure.
8) a plurality of combustors / heat exchangers having compressed air; a full-blade compressor for supplying compressed air to the combustors / heat exchangers; A combined steam gas turbine engine having a full-blade steam gas turbine that obtains output with superheated steam obtained by heat exchange. 2. An annular compressed air receiving portion (61) and an annular combustion gas sending portion (5) with a water-cooled outer wall having a spiral welding structure.
(8) a plurality of combustor / heat exchangers, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas and a combustion gas temperature of not more than the turbine heat resistant limit temperature. Steam having an all-blade steam gas turbine that obtains output with superheated steam obtained by heat exchange, and a device that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature Gas turbine combined engine. 3. An annular compressed air receiving portion (61) and an annular combustion gas sending portion (5) with a water-cooled outer wall having a spiral welding structure.
(8) a plurality of combustor / heat exchangers, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas and a combustion gas temperature of not more than the turbine heat resistant limit temperature. Steam having an all-rotor blade steam gas turbine that obtains output with superheated steam obtained by heat exchange, and a machine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. Gas turbine combined engine. 4. An annular compressed air receiving portion (61) and an annular combustion gas sending portion (5) with a water-cooled outer wall having a spiral welding structure.
(8) a plurality of combustor / heat exchangers, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas and a combustion gas temperature of not more than the turbine heat resistant limit temperature. An all-blade steam gas turbine that obtains output with superheated steam obtained by heat exchange, and an injection port (29) that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. And a superheated steam reservoir (30) for supplying superheated steam to the injection port. 5. An annular compressed air receiving portion (61) and an annular combustion gas sending portion (5) with a water-cooled outer wall having a spiral welding structure.
(8) a plurality of combustor / heat exchangers, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas and a combustion gas temperature of not more than the turbine heat resistant limit temperature. A combined steam gas turbine engine having an all-rotor steam turbine and an output shaft (12) for obtaining an output with superheated steam obtained by heat exchange. 6. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welding structure unit assembly structure, and compressed air. Rotor blade compressor that supplies heat to the combustor / heat exchanger, and a rotor blade steam that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine having a gas turbine. 7. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with the water-cooled outer wall being a helical welded structural unit assembly structure; Rotor blade compressor that supplies heat to the combustor / heat exchanger, and a rotor blade steam that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine having a gas turbine and a device for obtaining an output with superheated steam obtained by heat exchange so that a combustion gas temperature is equal to or lower than a turbine heat-resistant limit temperature. 8. A plurality of combustors / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with the water-cooled outer wall having a spiral welding structure unit assembly structure, and compressed air. Rotor blade compressor that supplies heat to the combustor / heat exchanger, and a rotor blade steam that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine having a gas turbine and a machine that obtains an output with superheated steam obtained by heat exchange so that a combustion gas temperature is equal to or lower than a turbine heat resistant limit temperature. 9. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welded structural unit assembly structure, and compressed air. Rotor blade compressor that supplies heat to the combustor / heat exchanger, and a rotor blade steam that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature. A gas turbine, an orifice (29) for obtaining an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature, and an overheated steam reservoir (30) for supplying the superheated steam to the orifice. A steam gas turbine combined engine having 10. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welding structure unit assembly structure, and compressed air. Rotor blade compressor that supplies heat to the combustor / heat exchanger, and a rotor blade steam that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature. A combined steam gas turbine engine having a gas turbine and the output shaft (12). 11. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure; Rotor blade compressor that supplies heat to the heat exchanger, and a rotor blade steam gas turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine allowable temperature limit. A steam gas turbine combined engine having 12. A plurality of combustors and heat exchangers having an annular compressed air receiving section (61) and an annular combustion gas sending section (58) as a spiral water cooling outer wall unit assembly structure, and the compressed air is burned. Rotor blade compressor that supplies heat to a heat exchanger and a combustor, and a rotor blade steam gas turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine allowable temperature limit. And a device for obtaining an output using superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. 13. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure; Rotor blade compressor that supplies heat to the heat exchanger, and a rotor blade steam gas turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine allowable temperature limit. And a machine for obtaining an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature. 14. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is subjected to the combustion. Rotor blade compressor that supplies heat to the heat exchanger, and a rotor blade steam gas turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine allowable temperature limit. Steam having an orifice (29) for obtaining an output with superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat resistant limit temperature, and a superheated steam reservoir (30) for supplying the superheated steam to the orifice; Gas turbine combined engine. 15. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is subjected to the combustion. Rotor blade compressor for supplying heat to a heat exchanger and a combustor, and a rotor blade steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature; and A combined steam gas turbine engine having the output shaft (12). 16. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welding structure, and the compressed air is subjected to the combustion. Gas turbine unit having a compressor that supplies heat to a heat exchanger and a steam gas turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature organ. 17. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welding structure, and the compressed air is subjected to the combustion. A compressor that supplies heat to the heat exchanger, a steam gas turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine heat-resistant limit temperature, and a turbine that outputs the combustion gas temperature. An apparatus for obtaining an output using superheated steam obtained by exchanging heat so that the temperature becomes equal to or lower than a heat-resistant limit temperature. 18. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welding structure, and the compressed air is subjected to the combustion. A compressor that supplies heat to the heat exchanger, a steam gas turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine heat-resistant limit temperature, and a turbine that outputs the combustion gas temperature. A combined steam and gas turbine engine having a machine that obtains output with superheated steam obtained by heat exchange so as to be below a heat-resistant limit temperature. 19. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welding structure, and the compressed air is subjected to the combustion. A compressor that supplies heat to the heat exchanger, a steam gas turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine heat-resistant limit temperature, and a turbine that outputs the combustion gas temperature. Injector (29) that obtains output with superheated steam obtained by exchanging heat to be below the heat-resistant limit temperature
And a superheated steam reservoir (30) for supplying superheated steam to the injection port. 20. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welding structure, and the compressed air is subjected to the combustion. A compressor for supplying heat to a heat exchanger and a combustion gas, a steam gas turbine for obtaining output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than a turbine heat resistant limit temperature, and the output shaft (12) And a combined steam gas turbine engine having 21. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with the water-cooled outer wall being a helical welded structural unit assembly structure; And a steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature. Gas turbine combined engine. 22. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welding structure unit assembly structure, and compressed air. A steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the temperature of the combustion gas and the combustion gas is equal to or lower than the turbine heat-resistant limit temperature; A device that obtains output with superheated steam obtained by heat exchange so that the temperature is equal to or lower than the turbine heat-resistant limit temperature. 23. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welding structure unit assembly structure, and compressed air. A steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the temperature of the combustion gas and the combustion gas is equal to or lower than the turbine heat-resistant limit temperature; A combined steam and gas turbine engine comprising: a machine that obtains output with superheated steam obtained by performing heat exchange so that the temperature is equal to or lower than a turbine heat-resistant limit temperature. 24. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with the water-cooled outer wall being a helical welding unit assembly structure, and compressed air. A steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the temperature of the combustion gas and the combustion gas is equal to or lower than the turbine heat-resistant limit temperature; A steam gas turbine combination having a nozzle (29) for obtaining an output with superheated steam obtained by heat exchange so that the temperature is equal to or lower than the turbine heat resistant limit temperature, and a superheated steam reservoir (30) for supplying superheated steam to the nozzle. organ. 25. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) with a water-cooled outer wall having a spiral welded unit construction structure, and compressed air. And a steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature, and the output shaft. (12) A combined steam gas turbine engine having: 26. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure; Gas turbine unit having a compressor that supplies heat to a heat exchanger and a steam gas turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature organ. 27. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure; A compressor that supplies heat to the heat exchanger, a steam gas turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine heat-resistant limit temperature, and a turbine that outputs the combustion gas temperature. An apparatus for obtaining an output using superheated steam obtained by performing heat exchange so as to be equal to or lower than a heat-resistant limit temperature. 28. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water cooling outer wall unit assembly structure, and the compressed air is burned. A compressor that supplies heat to the heat exchanger, a steam gas turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and a turbine that has a combustion gas temperature of A combined steam and gas turbine engine having a machine that obtains output with superheated steam obtained by heat exchange so as to be below a heat-resistant limit temperature. 29. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water cooling outer wall unit assembly structure, and the compressed air is burned. A compressor that supplies heat to the heat exchanger, a steam gas turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine heat-resistant limit temperature, and a turbine that outputs the combustion gas temperature. Injector (29) that obtains output with superheated steam obtained by exchanging heat to be below the heat-resistant limit temperature
And a superheated steam reservoir (30) for supplying superheated steam to the injection port. 30. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is subjected to the combustion. A compressor for supplying heat to a heat exchanger and a combustion gas, a steam gas turbine for obtaining output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than a turbine heat resistant limit temperature, and the output shaft (12) And a combined steam and gas turbine engine. 31. The combined steam gas turbine engine according to claim 16, wherein one of the compressor and the steam gas turbine is a full moving blade. 32. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; In order to obtain the output from superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are lower than the turbine heat resistance limit temperature, and so that the combustion gas temperature is lower than the turbine heat resistance limit temperature, An integrated steam gas turbine engine having an all-blade steam turbine that obtains an output with superheated steam obtained by heat exchange, and an all-blade compressor that rotates with the output. 33. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; A rotor blade steam gas turbine and an output shaft (12) for obtaining an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and A combined steam gas turbine engine having an all-blade steam turbine that obtains an output with superheated steam obtained by exchanging heat so that the temperature becomes equal to or lower than a limit temperature, an all-blade compressor that rotates by the output, and the output shaft (12) . 34. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. An all-blade compressor that supplies air to the combustor / heat exchanger, and a all-blade blade that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature. Steam having a steam gas turbine, an all-blade steam turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and an all-blade compressor that rotates with the output Gas turbine combined engine. 35. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. An all-blade compressor that supplies air to the combustor / heat exchanger, and a all-blade blade that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature. A steam gas turbine and the output shaft (12);
A full-blade steam turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, a full-blade compressor that rotates by the output, and the output shaft (12) Steam gas turbine combined engine having. 36. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air. An all-blade compressor that supplies the combustor and heat exchanger;
An all-blade steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are below the turbine heat resistance limit temperature, and heat so that the combustion gas temperature is below the turbine heat resistance limit temperature A combined steam gas turbine engine having an all-blade steam turbine that obtains an output with superheated steam obtained by exchange and an all-blade compressor that rotates with the output. 37. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air is provided. An all-blade compressor that supplies the combustor and heat exchanger;
All rotor blade steam gas turbines and output shafts (12) for obtaining output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and the combustion gas temperature being the turbine heat resistance limit A combined steam gas turbine engine having an all-blade steam turbine that obtains output with superheated steam obtained by heat exchange so as to be at or below a temperature, an all-blade compressor rotating by the output, and the output shaft (12). 38. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; And a steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature, and heat exchange is performed such that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam gas turbine engine having a steam turbine that obtains output with superheated steam and a compressor that rotates with the output. 39. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; And a steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature, and the output shaft (12). A combined steam and gas turbine having a steam turbine that obtains an output with superheated steam obtained by heat exchange with a compressor, a compressor that rotates by the output, and the output shaft (12). 40. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. A compressor for supplying air to the combustor / heat exchanger; a steam gas turbine for obtaining an output using superheated steam obtained by heat exchange between the combustion gas and the combustion gas so that the temperature of the combustion gas is equal to or lower than a turbine heat-resistant limit temperature; A combined steam and gas turbine engine having a steam turbine that obtains an output using superheated steam obtained by heat exchange so that a gas temperature is equal to or lower than a turbine heat-resistant limit temperature, and a compressor that rotates by the output. 41. A plurality of combustors / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. A compressor that supplies air to the combustor / heat exchanger; a steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that a combustion gas and a combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature; A shaft (12), a steam turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than a turbine heat-resistant limit temperature, a compressor that rotates by the output, and the output shaft (12). Steam gas turbine united engine. 42. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air. A compressor for supplying to the combustor / heat exchanger, a steam gas turbine for obtaining output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and a combustion gas temperature A combined steam gas turbine engine having a steam turbine that obtains an output with superheated steam obtained by heat exchange so as to be equal to or lower than a turbine heat resistant limit temperature, and a compressor that rotates by the output. 43. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air. A compressor for supplying to the combustor / heat exchanger; a steam gas turbine for obtaining output using superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature; ) And a steam turbine having a steam turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, a compressor that rotates by the output, and the output shaft (12). Turbine united engine. 44. The combined steam gas turbine engine according to claim 38, wherein at least three of the compressor, the steam gas turbine, the compressor, and the steam turbine are all blades. 45. The water-cooled outer wall has a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; In order to obtain an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature, A combined steam gas turbine engine having a full-rotor blade steam turbine that obtains output with superheated steam obtained by heat exchange. 46. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; A rotor blade steam gas turbine and an output shaft (12) for obtaining an output using superheated steam obtained by performing heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and A combined steam and gas turbine engine having an all-rotor blade steam turbine and an output shaft (12) for obtaining an output with superheated steam obtained by heat exchange so as to have a temperature lower than a limit temperature. 47. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; , A combustion blade and a full-blade steam gas turbine and a generator that obtain output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are lower than the turbine heat resistance limit temperature, and the combustion gas temperature is lower than the turbine heat resistance limit temperature A combined steam gas turbine engine having a full-blade steam turbine and a generator that obtains output with superheated steam obtained by heat exchange. 48. The water-cooled outer wall has a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; , A combustion blade and a full-blade steam gas turbine and a generator that obtain output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are lower than the turbine heat resistance limit temperature, and the combustion gas temperature is lower than the turbine heat resistance limit temperature A combined steam gas turbine engine having a full-blade steam turbine and a generator that obtains output with superheated steam obtained by heat exchange, a charger and an electric motor. 49. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding unit assembly structure. An all-blade compressor that supplies air to the combustor / heat exchanger, and a all-blade blade that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature. A combined steam gas turbine engine having a steam gas turbine and an all-blade steam turbine that obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature. 50. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. An all-blade compressor that supplies air to the combustor / heat exchanger, and a all-blade blade that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature. A steam gas turbine and the output shaft (12);
A combined steam gas turbine engine having an all-rotor blade steam turbine and an output shaft (12) for obtaining an output with superheated steam obtained by heat exchange so that a combustion gas temperature is equal to or lower than a turbine heat-resistant limit temperature. 51. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding unit assembly structure. An all-blade compressor that supplies air to the combustor / heat exchanger, and a all-blade blade that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature. A combined steam gas turbine engine comprising: a steam gas turbine and a generator; and an all-blade steam turbine and a generator that obtain output with superheated steam obtained by exchanging heat so that a combustion gas temperature is equal to or lower than a turbine heat resistance limit temperature. 52. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. An all-blade compressor that supplies air to the combustor / heat exchanger, and a all-blade blade that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature. A steam gas turbine and a generator, a full-blade steam turbine and a generator that obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and a charger and an electric motor Steam gas turbine combined engine. 53. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembly structure, and compressed air. An all-blade compressor that supplies the combustor and heat exchanger;
An all-blade steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are below the turbine heat resistance limit temperature, and heat so that the combustion gas temperature is below the turbine heat resistance limit temperature An integrated steam gas turbine engine having a full-rotor blade steam turbine that obtains output with superheated steam obtained by replacement. 54. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is provided. An all-blade compressor that supplies the combustor and heat exchanger;
All rotor blade steam gas turbines and output shafts (12) for obtaining output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and the combustion gas temperature being the turbine heat resistance limit A combined steam and gas turbine engine having an all-blade steam turbine and an output shaft (12) for obtaining an output using superheated steam obtained by performing heat exchange so as to be at or below a temperature. 55. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air. An all-blade compressor that supplies the combustor and heat exchanger;
Combustion gas and all-blade steam gas turbine and generator to obtain output with superheated steam obtained by heat exchange so that the combustion gas temperature is below the turbine heat resistance limit temperature, and the combustion gas temperature is below the turbine heat resistance limit temperature Steam turbine combined engine having a full-blade steam turbine and a generator that obtains output with superheated steam obtained by heat exchange as described above. 56. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembly structure, and compressed air. An all-blade compressor that supplies the combustor and heat exchanger;
Combustion gas and all-blade steam gas turbine and generator to obtain output with superheated steam obtained by heat exchange so that the combustion gas temperature is below the turbine heat resistance limit temperature, and the combustion gas temperature is below the turbine heat resistance limit temperature Steam turbine combined engine having a rotor blade steam turbine and a generator for obtaining an output with superheated steam obtained by heat exchange as described above, a charger and an electric motor. 57. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; And a steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature, and heat exchange is performed such that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A steam gas turbine combined engine having a steam turbine that obtains output with superheated steam. 58. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; And a steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is lower than the turbine heat resistance limit temperature, and the output shaft (12), and the combustion gas temperature is lower than the turbine heat resistance limit temperature. A steam gas turbine combined engine comprising: a steam turbine that obtains an output using superheated steam obtained by heat exchange with the steam turbine; and the output shaft (12). 59. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; Heat exchange between the steam gas turbine and the generator to obtain output with superheated steam obtained by heat exchange so that the combustion gas temperature is lower than the turbine heat resistance limit temperature, and heat exchange so that the combustion gas temperature is lower than the turbine heat resistance limit temperature A combined steam and gas turbine engine having a steam turbine and a generator for obtaining an output from the superheated steam obtained. 60. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; Heat exchange between the steam gas turbine and the generator to obtain output with superheated steam obtained by heat exchange so that the combustion gas temperature is lower than the turbine heat resistance limit temperature, and heat exchange so that the combustion gas temperature is lower than the turbine heat resistance limit temperature A combined steam and gas turbine engine having a steam turbine and a generator for obtaining an output from the superheated steam obtained as described above, a charger and an electric motor. 61. A plurality of combustors / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. A compressor that supplies air to the combustor / heat exchanger; a steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature; A combined steam gas turbine engine having a steam turbine that obtains output with superheated steam obtained by performing heat exchange so that the gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature. 62. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. A compressor for supplying air to the combustor / heat exchanger; a steam gas turbine for obtaining an output with superheated steam obtained by heat exchange between the combustion gas and the combustion gas so that the temperature of the combustion gas becomes equal to or lower than a turbine heat-resistant limit temperature; A shaft (12), a steam turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and the output shaft (1).
2) A combined steam gas turbine engine having: 63. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. A compressor for supplying air to the combustor / heat exchanger; a steam gas turbine and a generator for obtaining an output with superheated steam obtained by heat exchange between the combustion gas and the combustion gas so that the temperature of the combustion gas becomes equal to or lower than a turbine heat-resistant limit temperature A steam gas turbine combined engine comprising: a steam turbine and a power generator that obtain an output with superheated steam obtained by performing heat exchange so that a combustion gas temperature becomes equal to or lower than a turbine heat resistance limit temperature. 64. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. A compressor for supplying air to the combustor / heat exchanger; a steam gas turbine and a generator for obtaining an output with superheated steam obtained by heat exchange between the combustion gas and the combustion gas so that the temperature of the combustion gas becomes equal to or lower than a turbine heat-resistant limit temperature And a steam turbine and a generator, each of which obtains an output with superheated steam obtained by performing heat exchange so that a combustion gas temperature becomes equal to or lower than a turbine heat resistant limit temperature, and a charger and an electric motor. 65. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air. A compressor for supplying to the combustor / heat exchanger, a steam gas turbine for obtaining output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and a combustion gas temperature A combined steam gas turbine engine having a steam turbine that obtains an output with superheated steam obtained by heat exchange so as to be equal to or lower than a turbine heat resistant limit temperature. 66. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembly structure, and compressed air. A compressor for supplying to the combustor / heat exchanger; a steam gas turbine for obtaining output using superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature; ), A steam turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature, and a steam gas turbine combined engine having the output shaft (12). 67. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air. A compressor for supplying to the combustor / heat exchanger, a steam gas turbine and a generator for obtaining an output with superheated steam obtained by exchanging heat so that a combustion gas and a combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature, and combustion. A steam gas turbine combined engine having a steam turbine and a power generator that obtains output with superheated steam obtained by performing heat exchange so that a gas temperature is equal to or lower than a turbine heat-resistant limit temperature. 68. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembly structure, and the compressed air is provided. A compressor for supplying to the combustor / heat exchanger, a steam gas turbine and a generator for obtaining an output with superheated steam obtained by exchanging heat so that a combustion gas and a combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature, and combustion. A combined steam and gas turbine engine comprising: a steam turbine and a generator that output power with superheated steam obtained by performing heat exchange so that a gas temperature is equal to or lower than a turbine heat-resistant limit temperature; a charger and an electric motor. 69. The combined steam gas turbine engine according to claim 57, wherein at least two of the compressor, the steam gas turbine, and the steam turbine are all blades. 70. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; An integrated steam gas turbine engine comprising: an all-blade gas turbine that obtains output with combustion gas; and a device that obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. 71. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. An all-blade compressor that supplies air to the combustor / heat exchanger, a all-blade gas turbine that obtains output with combustion gas, and heat exchanged so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam gas turbine engine having a device that obtains output with superheated steam. 72. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is provided. An all-blade compressor that supplies the combustor and heat exchanger;
A combined steam gas turbine engine comprising: an all-blade gas turbine that obtains output with combustion gas; and a device that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. 73. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; An integrated steam gas turbine engine comprising: a gas turbine that obtains an output from a steam turbine; and a device that obtains output by using superheated steam obtained by performing heat exchange so that a combustion gas temperature is equal to or lower than a turbine heat-resistant limit temperature. 74. A plurality of combustors / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure, A compressor that supplies air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and an output is obtained with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine having a device. 75. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is provided. A compressor for supplying to the combustor / heat exchanger, a gas turbine for obtaining output with combustion gas, and a device for obtaining output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. Steam gas turbine combined engine having. 76. The combined steam and gas turbine engine according to any of claims 73 to 75, wherein any one of the compressor and the gas turbine is a full moving blade. 77. A water-cooled outer wall having a spiral welding structure,
A plurality of combustors / heat exchangers having an annular compressed air receiving portion (bi) 61 and an annular combustion gas sending portion (58); and a full blade compressor for supplying compressed air to the combustor / heat exchanger. An integrated steam gas turbine engine comprising: a full blade gas turbine that obtains output with combustion gas; and a machine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. 78. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure, An all-blade compressor that supplies air to the combustor / heat exchanger, a all-blade gas turbine that obtains output with combustion gas, and heat exchanged so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine having a machine that obtains output with superheated steam. 79. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is provided. An all-blade compressor that supplies the combustor and heat exchanger;
A combined steam gas turbine engine comprising: a full blade gas turbine that obtains output with combustion gas; and a machine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. 80. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; A combined steam and gas turbine engine comprising: a gas turbine that obtains an output from a steam turbine; and a machine that obtains output by using superheated steam obtained by performing heat exchange so that a combustion gas temperature is equal to or lower than a turbine heat-resistant limit temperature. 81. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. A compressor that supplies air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and an output is obtained with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam gas turbine engine having a machine. 82. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air. A compressor that supplies power to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and a machine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. Steam gas turbine combined engine having. 83. The combined steam and gas turbine engine according to claim 80, wherein one of the compressor and the gas turbine is a full blade. 84. The water-cooled outer wall has a spiral welding structure,
A plurality of combustors / heat exchangers having an annular compressed air receiving portion (bi) 61 and an annular combustion gas sending portion (58); and a full blade compressor for supplying compressed air to the combustor / heat exchanger. An all-blade gas turbine that obtains output with combustion gas, an orifice (29) that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and And a superheated steam reservoir (30) for supplying steam. 85. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure, An all-blade compressor that supplies air to the combustor / heat exchanger, a all-blade gas turbine that obtains output with combustion gas, and heat exchanged so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A nozzle (29) for obtaining output with superheated steam,
A superheated steam reservoir (30) for supplying superheated steam to the injection port. 86. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembly structure, and the compressed air. An all-blade compressor that supplies the combustor and heat exchanger;
An all-blade gas turbine that obtains output with combustion gas, an injection port (29) that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and supplies superheated steam to the injection port A combined steam and gas turbine having a superheated steam reservoir (30). 87. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; A gas turbine which obtains an output by means of a gas turbine, an injection port (29) which obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat resistant limit temperature, and a superheated steam reservoir which supplies superheated steam to the injection port 30). 88. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. A compressor that supplies air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and an output is obtained with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam gas turbine engine having an injection port (29) and a superheated steam reservoir (30) for supplying superheated steam to the injection port. 89. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air. A compressor for supplying to the combustor / heat exchanger, a gas turbine for obtaining an output from the combustion gas, and an injection port for obtaining an output from the superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature (29 ) And a superheated steam reservoir (30) for supplying superheated steam to the injection port. 90. The combined steam and gas turbine engine according to claim 87, wherein one of the compressor and the gas turbine is a full moving blade. 91. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; A full-rotor blade gas turbine that obtains output with combustion gas, a full-rotor blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and rotates with the output A combined steam gas turbine engine having a full blade compressor. 92. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. An all-blade compressor that supplies air to the combustor / heat exchanger, an all-blade gas turbine that obtains output with combustion gas, and a heat exchange performed so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam gas turbine engine having a full-blade steam turbine that obtains output with superheated steam and a full-blade compressor that rotates with the output. 93. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air. An all-blade compressor that supplies the combustor and heat exchanger;
A full-rotor blade gas turbine that obtains output with combustion gas, a full-rotor blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, and a total rotor that rotates by the output A combined steam gas turbine engine having a moving blade compressor. 94. The water-cooled outer wall has a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a compressor for supplying compressed air to the combustor / heat exchanger; Combined with a gas turbine that obtains an output with a steam turbine, a steam turbine that obtains an output with superheated steam obtained by exchanging heat so that the combustion gas temperature becomes equal to or lower than a turbine heat-resistant limit temperature, and a compressor that rotates by the output organ. 95. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure, A compressor that supplies air to the combustor / heat exchanger, a gas turbine that obtains output using combustion gas, and an output that uses superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature. A combined steam gas turbine engine having a steam turbine to be obtained and a compressor rotated by the output. 96. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is provided. A compressor that supplies a combustor and heat exchanger, a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. And a compressor rotating by the output. 97. The combined steam and gas turbine engine according to claim 94, wherein any three or less of the compressor, the compressor, the steam turbine, and the gas turbine are all blades. 98. The water-cooled outer wall has a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; Combined steam gas turbine having a full-blade gas turbine that obtains output with combustion gas and a full-blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature organ. 99. A water-cooled outer wall having a spiral welding structure,
A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58); a full blade compressor for supplying compressed air to the combustor / heat exchanger; Rotor blade gas turbine that obtains output from combustion gas and its output shaft (1)
2) a steam turbine combined engine having an all-rotor blade steam turbine and an output shaft (12) for obtaining an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature. 100. A water-cooled outer wall having a spiral welding structure, a plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), and compressed air. An all-blade compressor that supplies the combustor and heat exchanger;
A full-rotor blade gas turbine and a generator that obtains output with combustion gas, and a full-rotor steam turbine and a generator that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine allowable temperature limit. A steam gas turbine combined engine having 101. A water-cooled outer wall having a spiral welding structure, a plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), and compressed air. An all-blade compressor that supplies the combustor and heat exchanger;
A full-rotor blade gas turbine and a generator that obtains output with combustion gas, and a full-rotor steam turbine and a generator that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine allowable temperature limit. , A charger and an electric motor. 102. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. An all-blade compressor that supplies air to the combustor / heat exchanger, a all-blade gas turbine that obtains output with combustion gas, and heat exchanged so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam gas turbine engine having a full-blade steam turbine that obtains output with superheated steam. 103. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. The all-blade compressor for supplying air to the combustor / heat exchanger, the all-blade gas turbine for obtaining an output from the combustion gas, and the output shaft (12), the combustion gas temperature being equal to or lower than the turbine heat resistant limit temperature. Steam turbine combined engine having an entire rotating blade steam turbine and an output shaft (12) for obtaining an output with superheated steam obtained by heat exchange as described above. 104. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. Heat exchange with an all-blade compressor that supplies air to the combustor / heat exchanger, a full-blade gas turbine and a generator that obtains output with combustion gas, so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine having a full-blade steam turbine and a generator for obtaining an output with superheated steam obtained by the above method. 105. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. Heat exchange with an all-blade compressor that supplies air to the combustor / heat exchanger, a full-blade gas turbine and a generator that obtains output with combustion gas, so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine comprising: a full-blade steam turbine and a generator for obtaining an output with the superheated steam obtained as described above; a charger and an electric motor. 106. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is An all-blade compressor that supplies the combustor and heat exchanger;
Combined steam gas turbine engine having a full blade gas turbine that obtains output with combustion gas and a full blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine allowable temperature limit . 107. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure; An all-blade compressor that supplies the combustor and heat exchanger;
An all-blade gas turbine that obtains output with combustion gas and the output shaft (12), and an all-blade steam turbine that obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature becomes equal to or lower than a turbine heat-resistant limit temperature. And a combined steam gas turbine engine having the output shaft (12). 108. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembly structure, and the compressed air. An all-blade compressor that supplies the combustor and heat exchanger;
A full-rotor blade gas turbine and a generator that obtains output with combustion gas, and a full-rotor steam turbine and a generator that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine allowable temperature limit. A steam gas turbine combined engine having 109. A plurality of combustor / heat exchangers having an annular compressed air receiving section (61) and an annular combustion gas sending section (58) as a spiral water cooling outer wall unit assembly structure, An all-blade compressor that supplies the combustor and heat exchanger;
A full-rotor blade gas turbine and a generator that obtains output with combustion gas, and a full-rotor steam turbine and a generator that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine allowable temperature limit. , A charger and an electric motor. 110. A water-cooled outer wall having a spiral welding structure, a plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), and compressed air. A compressor that supplies the combustor and heat exchanger, a gas turbine that obtains output with combustion gas, and a steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. A steam gas turbine combined engine having 111. A water-cooled outer wall having a spiral welding structure, a plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) and A compressor for supplying to the combustor / heat exchanger, a gas turbine for obtaining output from combustion gas, and the output shaft (12);
A steam turbine combined engine having a steam turbine that obtains an output with superheated steam obtained by heat exchange so that a combustion gas temperature becomes equal to or lower than a turbine heat-resistant limit temperature, and the output shaft (12). 112. A water-cooled outer wall having a spiral welding structure, a plurality of combustors / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), and the compressed air being supplied to the water cooling outer wall. A compressor supplied to the combustor / heat exchanger, a gas turbine and a generator that obtains output using combustion gas, and an output using superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine having a steam turbine and a generator. 113. A water-cooled outer wall having a spiral welding structure, a plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas delivering portion (58), A compressor supplied to the combustor / heat exchanger, a gas turbine and a generator that obtains output using combustion gas, and an output using superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. Steam turbine and generator to obtain;
A combined steam gas turbine engine having a charger and an electric motor. 114. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. A compressor that supplies air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and an output is obtained with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam gas turbine engine having a steam turbine. 115. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembling structure. A compressor for supplying air to the combustor / heat exchanger, a gas turbine for obtaining an output from the combustion gas, and the output shaft (12) are heat-exchanged so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature. A combined steam gas turbine engine having a steam turbine that obtains output with the obtained superheated steam and the output shaft (12). 116. A plurality of combustors and heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. A compressor for supplying air to the combustor / heat exchanger; a gas turbine and a generator for obtaining an output from the combustion gas; and a superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine having a steam turbine and a generator for obtaining an output from the steam turbine. 117. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58), wherein the water-cooled outer wall has a spiral welding structure unit assembly structure. A compressor for supplying air to the combustor / heat exchanger; a gas turbine and a generator for obtaining an output from the combustion gas; and a superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine having a steam turbine and a generator for obtaining an output with a battery, a charger and an electric motor. 118. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a spiral water-cooled outer wall unit assembly structure, and the compressed air is provided. A compressor that supplies the combustor and heat exchanger, a gas turbine that obtains output with combustion gas, and a steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. A steam gas turbine combined engine having 119. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and the compressed air is provided. A compressor for supplying to the combustor / heat exchanger, a gas turbine for obtaining output from combustion gas, and the output shaft (12);
A steam turbine combined engine having a steam turbine that obtains an output with superheated steam obtained by heat exchange so that a combustion gas temperature becomes equal to or lower than a turbine heat-resistant limit temperature, and the output shaft (12). 120. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembling structure, and compressed air. A compressor supplied to the combustor / heat exchanger, a gas turbine and a generator that obtains output using combustion gas, and an output using superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine having a steam turbine and a generator. 121. A plurality of combustor / heat exchangers having an annular compressed air receiving portion (61) and an annular combustion gas sending portion (58) as a helical water-cooled outer wall unit assembly structure, and the compressed air. A compressor supplied to the combustor / heat exchanger, a gas turbine and a generator that obtains output using combustion gas, and an output using superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. Steam turbine and generator to obtain;
A combined steam gas turbine engine having a charger and an electric motor. 122. The claim 110 through claim 121.
Wherein the compressor, the steam turbine, and the gas turbine all have two or more moving blades. 123. A combined steam gas turbine engine, wherein the steam gas turbine uses superheated steam at or below supercritical steam conditions. 124. A combined steam gas turbine engine, wherein the all-blade steam gas turbine uses superheated steam under supercritical steam conditions. 125. A combined steam gas turbine engine, wherein the steam turbine uses superheated steam having a supercritical steam condition or less. 126. A steam gas turbine combined engine, wherein the all-blade steam turbine uses superheated steam under supercritical steam conditions. 127. A combined steam gas turbine engine comprising: a magnetic friction power transmission device (14) in which an inner shaft device and an outer shaft device of the full-blade steam gas turbine are connected at an optimum rotation ratio. 128. A combined steam gas turbine engine comprising a magnetic friction power transmission device (14) in which an inner shaft device and an outer shaft device of the full-blade steam turbine are connected at an optimum rotation ratio. 129. A combined steam gas turbine engine comprising: a magnetic friction power transmission device (14) in which an inner shaft device and an outer shaft device of the full blade compressor are connected at an optimum rotation ratio. 130. The magnetic friction power transmission device (14)
Is a steam gas turbine combined engine having a cooling device. 131. A combined steam gas turbine engine, wherein a bypass is provided in an all-blade compressor that supplies the compressed air to a combustor / heat exchanger. 132. A combined steam gas turbine engine, wherein a bypass is provided in a compressor that supplies the compressed air to a combustor / heat exchanger. 133. A combined steam gas turbine engine wherein the combustion gas supplied to the all-blade steam gas turbine is supplied to an intermediate stage according to the pressure, mixed with superheated steam, and directly reheated. . 134. A combined steam gas turbine engine wherein the combustion gas supplied to the steam gas turbine is supplied to an intermediate stage according to the pressure, mixed with superheated steam, and directly reheated. 135. A turbine blade of the inner blade moving blade group (20) of the full moving blade steam gas turbine includes a reheat cascade (60) provided with a hole for sucking and atomizing combustion gas. Steam gas turbine combined engine. 136. The steam turbine, wherein the turbine blades of the inner turbine blade group (20) of the steam gas turbine include a reheat cascade (60) provided with a hole for sucking and atomizing combustion gas. Gas turbine combined engine. 137. A part of the combustion gas supplied to the full-blade steam gas turbine is supplied from an upstream reheating cascade (60) having a pressure higher than the pressure and mixed with the superheated steam, and the superheated steam is directly converted to the superheated steam. A combined steam gas turbine engine characterized by reheating. 138. A part of the combustion gas supplied to the steam gas turbine is supplied to the upstream reheating cascade (6
0) mixed with superheated steam, and the superheated steam is directly reheated. 139. Combustion gas supplied to the full-blade steam gas turbine is supplied from the combustor / heat exchanger via an annular combustion gas delivery section (58) to the inner turbine bucket group (2).
0) The steam-gas-turbine united engine supplied from inside. 140. The combustion gas to be supplied to the steam gas turbine is supplied from the inside of the inner turbine blade group (20) from a combustor / heat exchanger via an annular combustion gas delivery section (58). A combined steam and gas turbine engine. 141. A combined steam gas turbine engine wherein the compressed air from the all-blade compressor is distributed and supplied in a honeycomb shape to a combustor / heat exchanger by an annular compressed air receiving portion (61). . 142. A combined steam gas turbine engine wherein the compressed air from the compressor is distributed and supplied to the combustor / heat exchanger in a honeycomb shape by an annular compressed air receiving portion (61). 143. The combined steam gas turbine engine according to claim 143, further comprising a device for levitating and moving the aircraft body by the thrust. 144. A combined steam gas turbine engine according to claim 144, further comprising a device for levitating and moving the ship by said thrust. 145. The combined steam gas turbine engine according to claim 145, further comprising a device for levitating and moving the aircraft body by the thrust and the rotating force. 146. The combined steam gas turbine engine as set forth in claim 1, further comprising a device for levitating and moving the ship by the thrust and the rotating force. 147. The combined steam gas turbine engine, wherein a device for rotating and moving wheels by the rotational force is provided in the combined steam gas turbine engine. 148. In the combined steam and gas turbine engine, a device for rotating and moving the wheels by the rotational force, and for generating and charging by the rotational force and rotating and moving the wheels by the electric motor. A combined steam gas turbine engine comprising: 149. The combined steam gas turbine engine according to claim 149, further comprising a device for generating and charging by the rotational force and rotating and moving wheels by an electric motor. 150. The combined steam gas turbine engine according to claim 150, further comprising a device for rotating the propeller by the rotational force to levitate and move the aircraft body. 151. The combined steam gas turbine engine according to claim 151, further comprising a device for rotating a propeller by the thrust and the rotating force to levitate and move the aircraft body. 152. The combined steam gas turbine engine according to claim 1, further comprising a device for rotating various propellers by the rotational force to levitate and move the aircraft body. 153. The combined steam gas turbine engine according to claim 153, further comprising an apparatus for rotating a propeller by the rotational force to move a ship. 154. The steam gas turbine united engine according to claim 1, further comprising a device for rotating the generator by the rotational force to supply electricity from the generator. 155. In the combined steam and gas turbine engine, when the generator is rotated by the rotational force to supply electricity from the generator, heat is supplied from the exhaust heat recovery heat exchanger (49). Steam turbine combined engine, characterized in that a combined device is provided. 156. In the combined steam and gas turbine engine, when the generator is rotated by the torque to supply electricity from the generator, the exhaust heat recovery heat exchanger (49) and the refuse incinerator heat exchange An integrated steam gas turbine engine provided with a device for supplying heat from a vessel (51). 157. The combined steam gas turbine engine as set forth in claim 1, further comprising a device for rotating the machine by the rotational force to perform work. 158. The combined steam gas turbine engine as set forth in claim 1, wherein a magnetic friction power transmission device is used as a device for rotating the machine with the rotational force to perform work. 159. A steam gas turbine combined engine, wherein the steam turbine compressor uses superheated steam having a supercritical steam condition or less. 160. A combined steam gas turbine engine comprising: a magnetic friction power transmission device (14) in which an inner shaft device and an outer shaft device of the full blade gas turbine are connected at an optimum rotation ratio. 161. The vehicle driven by the various steam turbines.
A combined steam gas turbine engine comprising: a magnetic friction power transmission device (14) in which an inner shaft device and an outer shaft device of an all-blade compressor are connected at an optimum rotation ratio. 162. The magnetic friction power transmission device (14)
To the main magnetized friction wheel (54) and the forward magnetized friction wheel (5).
5) A combined engine for a steam gas turbine, wherein a forward / reverse switching device is provided by a reverse rotation friction wheel (56) and an electromagnet (34).