JP2001012209A - Steam gas turbine united engine device - Google Patents

Abstract

PROBLEM TO BE SOLVED: To improve the heat efficiency and the specific output by providing a water cooled external wall with a spiral structure, comprising a combustor/heat exchanger minimized into the shape of a number of honeycombs of small diameter, supplying the compressed air to the same from a total rotor blade compressor, and driving the total rotor blade gas turbine by the obtained combustion gas. SOLUTION: Air is sucked from an external compressor rotor blade group 1 level 16 of a total rotor blade compressor, and compressed by the co-operation of an internal compressor rotor blade group 17 of even level and the external compressor rotor blade group 15 of odd level, and compressed air 15 is guided to an annular outlet 21, an annular receiving port 22 and an annular compressed air reservoir 8. Then compressed air is supplied to a combustor/heat exchanger 4 minimized into the shape of a number of honeycombs of small diameter, and stirred and mixed with the fuel including the steam supplied from a fuel supply means 27 to be combusted, whereby the combustion gas of high temperature and high pressure is produced. The combustion gas is supplied to the external turbine rotor blade group 19 of a total inlet blade gas turbine through an annular combustion gas reservoir 9, an annular nozzle hole group and an annular receiving port 23 to generate the motive power.

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 multi-combustor of a gas turbine, wherein a substantially spiral welded water cooling outer wall heat exchanger or a spiral water cooling outer wall unit is used. As a heat exchanger with an assembled structure or a spirally welded water-cooled outer wall unit as a unitary structure heat exchanger, it is possible to make a reasonable cylindrical shape by shortening it into a large number of small diameter honeycombs, and it is possible to greatly increase the pressure and greatly improve efficiency. In addition to increasing the heat exchange heat transfer area by reducing the size of the combustor / heat exchanger into a large number of small-diameter honeycombs according to the application, the conventional fuel supply means is used as a short and high pressure vessel. Around three times the technology, it is easy to add to the uppermost stream side, and a steam superheater is provided in the combustor / heat exchanger, including one that is nearly linear in a spiral shape. Including rockets that spray By using a steam turbine that obtains output from the superheated steam and a gas turbine that obtains output from the combustion gas, it can be used in various applications such as various aircraft, various ships, various vehicles, and various types of power generation equipment. The present invention also relates to a new technology of various types of steam gas turbine united engines, which also includes a suitable engine.

[0002]

2. Description of the Related Art Japanese Patent Application Laid-Open No. 50-97737 discloses a prior art in which a heat exchanger is provided inside a gas turbine combustor in a combined steam turbine / gas turbine 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 by performing evaporation by heat exchange with combustion gas between gas turbines, the temperature of waste gas at the outlet of the waste heat recovery boiler is reduced, and the boiler efficiency is improved. However, none of these aims to improve the thermal efficiency of the supercharging boiler cycle, and does not aim to simultaneously increase the pressure ratio and the specific output of the gas turbine, 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, Japanese Patent Application No. 11-69406, and Japanese Patent Application No. 11-77189. The priority claim application based on the above-mentioned prior application generally includes a heat exchanger including a whole rotor blade and / or a plurality of combustors of a gas turbine being lengthened, and a water-cooled outer wall spirally provided as 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 supply heat quantity (fuel combustion mass) to the maximum without exceeding the heat-resistant limit temperature of the turbine is to convert most of the supply heat quantity (fuel heat quantity) into superheated steam and to use a steam turbine or the like. The thermal efficiency x specific output = pressure ratio x combustion gas mass = velocity x mass greatly increases (in Tanikawa Mechanics, mass x velocity works, high temperature decreases unit volume mass = decrease factor of work At the same time, when the combustion gas temperature falls below the turbine inlet heat resistant limit temperature,
Including a rocket that injects a superheated steam containing supercritical fluid, which is obtained by infinitely exchanging heat so as to be around 00 ° C. and injects the pressure by greatly increasing the pressure to about 10 times the pressure ratio,
It is intended to be used for transporting people or luggage, or for supplying heat, electricity or cold, including reducing the exhaust temperature to 0 ° C. or lower.

[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. When the fuel calorific value is converted into superheated steam or steam, various steam turbines are used. In the previous application, the length of the gas turbine combustor was increased to accommodate the infinite number of applications, but in addition to the complicated shape, there were many applications where it was difficult to increase the length. It is provided in the form of a large number of small-diameter honeycombs to reduce the length and pressure, supply combustion gas from the inside of the inner diameter to the gas turbine, and form a rational cylindrical shape, and also serve as a heat exchanger with a greatly increased heat transfer area. By the large number of fuel supply means on the most upstream side, the calorific value of the fuel is greatly converted to superheated steam, and heat exchange is performed without exceeding the heat-resistant limit temperature of the gas turbine or as much as possible up to around 400 ° C. Specific output An engine capable of increasing the fuel combustion mass, for example, up to a stoichiometric air-fuel ratio, about four times that of the prior art, and increasing the pressure ratio and the fuel combustion mass to increase the amount of heat supplied. In addition to providing a device that reduces the amount of heat used by the gas turbine and raises the thermal efficiency and specific output of the gas turbine, it also converts outside air heat energy into superheated steam, so that the combustion gas and the combustion gas temperature become the turbine heat resistant limit temperature. As described below, the superheated steam obtained by heat exchange drives the steam turbine compressor, the steam turbine, and the gas turbine, for example, drives various vehicles, or drives various aircraft, or drives various ships. The purpose is to drive.

[0006] Combustion gas as a working gas of a gas turbine generally has a very high air ratio, and includes air that is about four times the stoichiometric air-fuel ratio. Is not limited to numerical values). That is, in the conventional technology, nearly 80% of the compressed air that consumes a large amount of heat energy is wastefully discharged, and in addition, it is used to reduce the combustion temperature, resulting in a large loss. Compressed air can be effectively used up to nearly 100%, and other applications requiring compressed air can be provided with a bypass. By heat exchange and temperature reduction, the pressure ratio and fuel combustion mass can be greatly increased. Of the supplied heat including the outside air temperature, the amount of heat used by the gas turbine is greatly reduced, the amount of gas used is greatly increased, the thermal efficiency of the gas turbine is increased by about three times, and the specific output is greatly increased, and the combustion is increased. Gas and
The steam turbine and gas turbine were driven by superheated steam obtained by heat exchange so that the combustion gas temperature was lower than the heat-resistant limit temperature of the gas turbine, and the pressure was greatly increased to about 10 times that of air compression. The purpose of the present invention is to greatly increase the total thermal efficiency by about 2 to 3 times and greatly increase the specific power by using superheated steam including critical steam conditions.

When the gas turbine combustor is shortened in a honeycomb shape with a large number of small diameters and has a large heat transfer area, and is also used as a heat exchanger, the higher the pressure ratio, the higher the thermal efficiency of the gas turbine and the same heat generation. In the fuel combustion of a large amount, the higher the pressure ratio, the higher the temperature can be obtained, and the higher the gas temperature at the gas turbine inlet is 400 C to 1000 C, the easier the heat exchange becomes. For this reason, including the increase in fuel supply, the advanced steam gas turbine combined cycle power generation facilities
Waste heat recovery More than 10 times more heat energy recovery than with a heat exchanger. Furthermore, since the heat transfer area of the heat exchanger can be reduced and shortened, fuel supply means can be provided only on the most upstream side. For difficult NOx reduction combustion in a high temperature and high pressure atmosphere, at 400 ° C. of combustion gas at the heat exchange turbine inlet,
Since the combustion gas volume is reduced to approximately one half of that of the prior art, in addition to increasing the fuel combustion mass by 4 times, supercritical steam or water injection agitation combustion is used to achieve a large increase in the combustion gas volume mass. It also enables reduced combustion. In addition, a steam gas turbine with ultra-high performance and ultra-high thermal efficiency that enables the exhaust heat to be used to the utmost, enabling a significant reduction in exhaust loss by increasing the pressure ratio and lowering the heat exchange gas turbine exhaust temperature. It is an object of the present invention to provide a combined engine and minimize the power transmission loss by maximizing the use of a magnetic friction power transmission device.

[0008]

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 stoichiometric mixture. That is, since about 80% of the compressed air which consumes a large amount of heat energy is wasted, and in addition, it is used for lowering the combustion temperature, resulting in a large loss. By increasing the heat exchange heat transfer area of the combustor and heat exchanger, the superheated steam conversion by heat exchange enables approximately 100% of the compressed air for combustion to participate in combustion and make it available for use.
The combustor and heat exchanger are arranged in a short, large number of honeycombs according to the application, and the combustion gas is supplied from the most upstream side of the gas turbine, enabling a reasonable cylindrical shape, as well as high pressure and fuel. It is easy to add only the most upstream side of the supply means,
The maximum fuel supply is about four times that of the conventional technology to increase the volume of combustion gas. The heat transfer area of the combustor / heat exchanger is greatly increased, and the combustion gas temperature is converted into superheated steam without limit.
The unit volume of the supplied combustion gas will be increased up to around 0 ° C, including reducing the exhaust gas temperature to around 0 ° C, reducing the unit volume to approximately half that of the conventional technology. The combustor outer wall is formed as a spiral welded water cooling outer wall including a water pipe or a spiral welded structure water cooled outer wall unit assembly structure, or a spiral water cooled outer wall unit assembly structure, including setting of a large pressure ratio. High temperature NO
x Combustion in atmospheres that are difficult to reduce, including supercritical steam or water-jet agitated combustion, ensures an increase in the volume of combustion gas including superheated steam and a reduction in NOx. Used for a variety of applications, including rockets that inject superheated steam such as supercritical fluid obtained by heat exchange.

The design items of the combustor / heat exchanger include:
In the case of the smallest diameter, the end portion of the water-cooled outer wall water conduit is used as a superheated steam as a steam pipe, and the steam pipe is provided in a substantially spiral shape or a nearly linear spiral shape according to the inner diameter of the water-cooled outer wall, It is also used as an ultra-high-performance heat exchanger with significantly higher pressure,
When the heat exchange amount is small, the combustor and heat exchanger in the outer row of the water-cooled outer water conduit are arranged in a honeycomb structure. 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 this case, FIG. d) Use a water-cooled external wall combustor / heat exchanger. By this heat exchange, the gas turbine inlet temperature is lowered below the turbine heat-resistant limit temperature as much as possible according to the application, and the total compressed air compressed for combustion is brought close to the stoichiometric air-fuel ratio combustion to reduce the fuel combustion mass by 4%.
And convert most of the fuel calorific value to superheated steam, including supercritical steam conditions, a pressure increase of nearly 10 times that of air compression, and in an atmosphere with a high pressure ratio. By using heat exchange including outside air heat energy recovery, the heat energy recovery in a boiler is about twice that of heat exchange,
By greatly increasing thermal efficiency and specific power, saving fuel, combustion gas and combustion gas temperature from below the turbine heat resistance limit temperature,
A superheated steam obtained by heat exchange drives a gas turbine, a steam turbine, or a steam turbine compressor so that the temperature becomes about 400 ° C., and propellers, wheels, a generator, a machine, and the like are driven by the rotational power and thrust. A variety of devices that rotate and drive various aircraft, automobiles, ships, machines, etc., and also levitate and propell various aircraft, ships, etc. by the thrust of superheated steam exhaust, combustion gas exhaust, or compressed air depending on the application. Provide a control unit that controls the

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 at a pressure about 10 times that of air compression, a large increase in thermal efficiency can be obtained as a large volume and a large speed far exceeding 1700 times. The best way to effectively utilize substantially all of the compressed air for combustion is to convert and use superheated steam with the highest efficiency, including substantially all of the increased fuel supply. Therefore, in order to obtain an ultra-high-performance combustor / heat exchanger, combustion and heat exchange are performed at as low a temperature as possible in a high-temperature and high-pressure atmosphere to achieve the most efficient heat exchange and reduce NOx combustion by cooling. It is possible to maximize the amount of heat (superheated steam) extracted from the fuel with the same calorific value, including external air heat energy, to obtain a huge amount of superheated steam most efficiently and to maximize the mass of combustion gas driving the gas turbine. The heat exchange minimizes the driving combustion gas calorific value, drives the gas turbine with the highest thermal efficiency, and significantly lowers the exhaust calorific value including exhaust gas temperature around 0 ° C, greatly reducing exhaust loss. It is also used as heat, electricity and cold heat supply equipment, and is provided with a bypass for applications requiring compressed air. By using the friction power transmission device appropriately or entirely, the maximum thermal efficiency of the steam gas turbine cycle including all the rotor blades as the drive device that transmits the power most efficiently, including all the auxiliary machines, is 2 We aim for a large rise around 2 to 3 times.

[0011]

DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiments and embodiments of the present invention will be described with reference to the drawings. The reference numerals are used to omit duplicate explanations, and the characteristic parts and the parts that are not explained are added and explained sequentially. 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, which has been enlarged in the previous application, is conversely shortened and arranged in a small-diameter multiple-honeycomb shape to increase the heat exchanger heat transfer area, The combustion gas is supplied to the uppermost stream side of the turbine cascade, and has a reasonable shape. As shown in FIGS. 1 to 4, 13, and 14, 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, and a small-diameter multiple honeycomb. A relatively large pressure ratio is set as the combustor / heat exchanger 4 arranged in a short shape, and the steam pipe 6 is provided inside in a substantially spiral shape or in a nearly linear spiral shape. As a combustor / heat exchanger 4, which is provided with no generator / motor, etc., is also used as a heat / electricity / cold heat supply facility or a starting device, and is arranged in a short shape in a honeycomb structure with many small diameters. 27 is provided on the most upstream side of each husband and the like, and the number of fuel supply means 2 is increased.
7 can be easily added and the heat exchange rate can be 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 in a state of being 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 occur.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. In addition to the double inversion driving, the peripheral speed is shared by approximately half, the outer diameter is approximately doubled and the fluid passage is approximately quadrupled, and the specific output is greatly increased, and the thermal efficiency is greatly increased. The relative speed between the moving blades is approximately 2
Doubling the specific power and thermal efficiency, or reducing the peripheral speed by approximately half of that of the prior art to reduce the allowable stress to approximately one-fourth.
It allows for a variety of designs (combined use of heat, electricity and cold for business or home use), such as low-cost, quiet, etc., while greatly increasing thermal efficiency.

A first embodiment of the core portion of the combined steam gas turbine engine shown in FIG. 1, an embodiment of the steam turbine compressor shown in FIGS. 5 to 8, and an embodiment of the combined steam gas turbine engine shown in FIGS. See and explain. As shown in FIG. 1, air is sucked in as usual from the first stage 16 of the replaced outer compressor blade group at the right end of the full blade compressor, and the inner compressor blade group 17 of the even-numbered stage is sucked.
And the odd-numbered stages of outer compressor blade groups 16 cooperate to efficiently compress air by all the blades, including known air cooling (not shown), and convert the compressed air 15 to the outer compressor blade group. From the final stage 16, through the annular outlet 21, the annular receptacle 2
2. A combustor / heat exchanger 4 having a small diameter and a large number of honeycombs arranged in a short shape from the annular compressed air reservoir 8 to increase the heat transfer area.
The high-compressed air 15 supplied is supplied from a fuel supply means 27 containing steam at the upstream side of each of them according to a command from a known control device (not shown). Around four times as much fuel and agitated mixed combustion / supercritical steam injection agitation NOx reduction combustion and combustion including near stoichiometric air-fuel ratio combustion, from combustion gas temperature below the turbine heat resistant limit temperature to around 400 ° C While performing combustion control in the combustor / heat exchanger 4, combustion and heat exchange according to the application are performed so that the water cooling outer wall 26 and the steam
As a result, the combustion gas 10 is cooled and heat-exchanged, and 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 and the annular nozzle group 24, It is supplied to the outer turbine blade group 1 stage 19 of the all-blade gas turbine having an annular receiving port 23, and generates rotational power sequentially downstream, and exhausts the exhaust gas including the exhaust temperature around 0 ° C depending on the application. .

Most of the supplied heat energy is converted into superheated steam 5 and is passed through a steam control valve 7 including a steam pipe 6 and a control device of each of the combustor / heat exchanger 4, as shown in FIG. Pool 3
Injection from the most upstream side of the steam turbine of the steam turbine compressor including all the moving blades of FIGS. 5 to 8 to the outer turbine moving blade group one stage 19, the inner turbine stationary blade, or the prior art stationary blade. Then, by sequentially driving the downstream side as usual, a large rotation output is sequentially generated, and the various compressors in the figure are strongly driven. The superheated steam which has been supplied to the downstream side and turned into wet steam or water droplets is injected from the outer turbine blade group 19 to the outer peripheral side by centrifugal force except for those using the conventional stationary blade. That is, the gas turbine and the steam turbine are driven to obtain a rotational force, and the respective exhausts are ejected, and the right front air is strongly ejected to the left rear to require the rotational force and the levitation propulsion force. Various applications, such as helicopters and jet aircraft, and various types of ships used for propulsion,
Or, an intermediate between an aircraft and a ship, or the like, is used for levitation injection propulsion, or is used as a rocket that injects superheated steam by providing a superheated steam reservoir 30 and an injection port 29 in FIG. 9, or A variety of well-known types that are used for rotating driving propellers, wheels, generators, machines, etc., and greatly increase thermal efficiency, propulsion efficiency and levitation propulsion efficiency by superheated steam whose pressure is nearly 10 times that of conventional air compressors. It is the core of an all-blade / steam gas turbine combined engine that has a control unit.

Referring to FIG. 1, another description will be given. The heat transfer area of the combustor / heat exchanger 4 can be easily increased and the small-diameter multi-honeycomb arrangement can be easily shortened, so that the lightweight high-pressure vessel can be easily provided with fuel supply means. 27 is about 4 times as large as the conventional technology, and is installed on the most upstream side. A magnetic friction power transmission device 14 is provided on each of the left and right sides of the center, and each is fixed to the inner shaft device and is provided annularly on the outer periphery. The outer shaft device to which the fixing shaft 19 is fixed is externally rotatably fitted to each other, and the two shafts rotating in opposite directions to each other are connected to each other by the magnetic friction power transmission device 14 at an optimum rotation ratio. The inner compressor rotor blade group final stage 17 and the inner turbine rotor blade group 2
The stage 20 is fixed, and the outer compressor blade group odd-numbered stage 16 is fixed to the outer compressor blade group odd-numbered final stage 16 of the outer shaft device. The even stages 17 are fixed alternately.
In order to transmit power most efficiently, a drive unit including a magnetic friction power transmission unit is used to configure the entire moving blade and compressor. And an outer turbine rotor blade group 1 stage 1 of the outer shaft device.
9, the outer turbine blade group odd-numbered stage 19 is fixed, and the inner turbine blade group second stage 20 is fixed to the inner turbine blade group even-numbered stage 2.
0, the inner turbine blade group even-numbered final stage 20 is fixed to the inner shaft device, and the outer turbine blade group odd-numbered final stage 19 is fixed to the outer shaft device. And rotatably fitted on the inner shaft device to form the core of the combined blade and steam gas turbine engine.

Referring to FIG. 2, a description will be given of a second embodiment of the core portion of the combined engine with all the blades and the steam gas turbine combined with the bypass. In the prior art, a large amount of heat energy is consumed and wasteful (reversely lowering the combustion temperature) is discharged without using nearly 80% of the compressed air for combustion, resulting in a large loss. Air compressed for combustion is used for combustion.
The compressed air 15 used for purposes other than combustion is provided with a bypass 28 and used separately to increase the specific output to the utmost limit and greatly increase the thermal efficiency. 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 at about four times the stoichiometric air-fuel ratio, the combustion gas does not exceed the heat-resistant limit temperature of the turbine. 1 compressed air
In order to use it for 00% combustion, it is essential to convert most of the supplied heat to superheated steam. In view of this, the present invention arranges the combustor / heat exchanger 4 in the form of a honeycomb having a small diameter and a large number of honeycombs, thereby increasing the heat transfer heat exchange area, making it easy to increase the pressure and increasing the fuel supply. The water-cooling outer wall unit 52 of the helical water pipe 1 includes a helical welded structure or a welded structure including at least one or more water pipes 1 and a water-cooled outer wall 26 of the water-cooled outer wall unit 52. With an assembled structure, enabling a large increase in pressure ratio and injection of superheated steam including supercritical, greatly increasing the specific output, and making almost all of the air compressed for combustion available for combustion, For applications requiring compressed air, a bypass is provided for separate use. For applications requiring rotational force, an output shaft 12 is provided to extract rotational power, eliminating waste of air compression and greatly increasing thermal efficiency. Try to rise.

Another explanation will be given with reference to FIGS. 2 and 5 to 12. Air is sucked in as usual from the replaced outer compressor blade group 1 stage 16 of the rightmost full blade compressor including the bypass 28, and the even-numbered inner compressor blade group 17 and the odd-numbered outer compressor The moving blade group 16 cooperates to efficiently compress the air by all the moving blades, and for other applications requiring compressed air, optimally supplies compressed air from a bypass 28 passage provided appropriately according to the application. Compressed air 15 is arranged in a high pressure manner in the form of a large number of small-diameter honeycombs from an annular outlet 21 of the full-blade compressor.
It is supplied to the annular receiving port 22 of both the combustor and heat exchanger 4. The supplied high compressed air 15 is stored in the annular compressed air reservoir 8, and is supplied from the fuel supply means 27 at the most upstream side of the combustor / heat exchanger 4. The fuel mixture before and after and the agitated mixed combustion including the substantially stoichiometric air-fuel ratio combustion are performed, and in the combustor / heat exchanger 4 having an enlarged heat exchange heat transfer area, combustion controlled combustion is performed to exchange heat.
Heat exchange cooling is performed by the water cooling outer wall 26 and the steam pipe 6 of each of the water guide pipes 1 to achieve NOx reduction combustion. The combustion gas 10 obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature or around 400 ° C. is supplied from the respective combustor / heat exchanger 4 to the annular combustion gas reservoir 9. Through the ring-shaped receiving port 23, rotatably inserted and airtightly held,
Outer turbine blade group 1 replaced from annular nozzle group 24
Injects sequentially to the downstream side, including stage 19 and the second stage 20 of the inner turbine blade group, to generate large rotating power as usual.

Below the heat-resistant limit temperature of the turbine or 400 ° C.
The superheated steam 5 obtained by heat exchange so as to be before and after is passed through the steam control valve 7 of each of the combustor / heat exchanger 4 as shown in FIG.
As shown in FIGS. 10 and 11, the steam is supplied from the steam pipe 6 of FIG. 8 to the most upstream side of the steam turbine of the steam turbine compressor including all the moving blades, and sequentially drives the downstream side to generate a large torque. The steam turbine including all the moving blades drives a compressor including all the moving blades to generate a thrust or a rotating force, thereby generating a turboshaft engine, a turboprop engine, a turbojet engine, and a turbofan engine. And as a levitation propulsion device for ships, it is used for various aircraft, various ships, etc. together with various core parts. Similarly, in FIG. 9, the core portion of the combined engine of the steam gas turbine including all the rotor blades,
The rocket is constructed by allowing the superheated steam reservoir 30 and the injection port 29, in which the water pipes 1 are densely arranged in a spiral cylindrical shape, to be separable between the stop valves 13 and 13. Similarly, in FIG. 12, the steam turbine including all the moving blades is driven, and the propeller, the wheel, the generator, the machine, and the like are mainly used for driving the propeller, the wheel, the generator, the machine, and the like by the torque and the core section torque. The power may be used at the same time, the heat of the exhaust gas is used, etc., it is also used as a combined supply of heat, electricity and cold, and it has a well-known various control device. Used for many applications as in the first embodiment.

Another explanation will be given with reference to FIG. A combustor / heat exchanger 4 is provided, which is shortened and arranged in the shape of a large number of small-diameter honeycombs, and the respective inner shaft devices are connected to a magnetic friction power transmission device 14 on the inner left and right sides of the inner shaft device at the inside thereof. The outer shaft device, in which the outer compressor blade group final stage 16 and the outer turbine blade group 1 stage 19 provided annularly are fixed to the left and right inner shaft devices, is rotatably fitted to the outer shaft device. The two shafts rotating in mutually opposite directions are respectively connected by the magnetic friction power transmission device 14 at an optimum rotation ratio, and the inner compressor rotor blade group final stage 17 and the inner shaft are connected to the respective inner shaft devices. The turbine rotor blade group 2 stage 20 is fixed, and the outer compressor rotor blade group odd stage 1
6, and even-numbered stages 17 of the inner compressor rotor group are alternately fixed, but alternately fixed, including the one with an enlarged outer diameter, as a bypass for compressed air used for purposes other than combustion. The outer shaft device is fixed to the first stage 16 and is rotatably fitted to the inner shaft device so as to be rotatably fitted to the outer shaft device.
4, it is coupled at the optimal rotation ratio, and the most efficient
The whole blade compressor that drives the shaft is configured. Also, the outer turbine bucket group 1 stage 19 has an outer turbine bucket group odd number stage 19 fixed thereto, and the inner turbine bucket group 2 even stage 20 has an inner turbine bucket group even number stage 20 fixed thereto. And the inner turbine blade group even-numbered final stage 20 is fixed to the inner shaft device, and the outer turbine blade group odd-numbered final stage 19 is fixed to the inner shaft device.
Is fixed to the outer shaft device, and is rotatably fitted to the inner shaft device so as to form a core part of the combined engine with all blades and steam gas turbine with bypass.

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. 1 is that the core of the combined rotor / steam gas turbine engine is the core of the steam gas turbine combined engine.
The replacement rotor blades are reduced to conventional stator vanes, and the conventional compressor and gas turbine are provided with a combustor / heat exchanger, which is arranged in a short shape in a small-diameter multi-honeycomb configuration, and is drivable. Thing. 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 FIGS. 3 and 12, which are close to the prior art steam / gas turbine combined cycle thermal power plant, the case of using it as a state-of-the-art thermal power plant will be described in comparison with the prior art. In the third embodiment using the conventional gas turbine shown in FIG. 3, when the generator is driven, the combustor / heat exchanger 4 is arranged in a short shape in the form of a large number of small-diameter honeycombs, and various heat exchanges according to the application are performed. It is possible to obtain an air temperature of 600 ° C at a pressure ratio of 60, a compression ratio of around 18, and an outside air temperature of 0 ° C. Therefore, if the turbine inlet temperature is set at around 400 ° C, the heat energy that can be recovered from the outside air temperature is very large. Become. Furthermore, with the same amount of compressed air for combustion, fuel combustion becomes up to about four times that of the conventional technology, and heat exchange is performed in a high-temperature, high-pressure atmosphere with the pressure ratio increased to the limit, so that the heat energy recovery efficiency is also high.
Compared to the waste heat recovery heat exchanger of the advanced steam / gas turbine combined cycle thermal power generation equipment of the prior art, the heat energy recovery is more than 10 times. Furthermore, as a greatly increased combustion gas mass including superheated steam, in addition to obtaining a small and large-output gas turbine,
Exhaust gas at an exhaust temperature of around 0 ° C enables the supply of cold heat. As for the comparison of pressure ratios, the use of large amounts of water makes it easier to lower the compressed air temperature, so the pressure ratio can be raised to the limit and thermal efficiency can be increased. That is, the more heat exchanged in an atmosphere with a large pressure ratio, the higher the thermal efficiency of the steam gas turbine united cycle, the larger the combustion gas mass, the smaller and larger the output of the gas turbine, and the smaller the exhaust heat, the smaller the thermal efficiency of the gas turbine. As the amount of thermal energy extracted from the same amount of fuel increases, the output of the steam turbine increases and the overall thermal efficiency increases to around 80%.

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. 2 is that the core part of the combined rotor / steam gas turbine engine is the core part of the combined steam gas turbine engine.
The replacement rotor blade is reduced to a conventional stator blade, and the combustor and heat exchanger of the compressor and gas turbine of the conventional technology are reduced in size and arranged in a honeycomb with small diameters to enable driving. .
Accordingly, the elements from the first embodiment to the fourth embodiment in FIG. 1 are appropriately replaced with each other, and are used for various purposes like the first embodiment, for example, for moving a vehicle and propelling a ship or an aircraft. Used for

Referring to FIG. 5, a first embodiment of a full blade / steam turbine compressor will be described. Superheated steam 5 obtained by heat exchange at the core of various steam gas turbine combined engines
The rotor blade steam turbine is driven to generate rotational force, which is used as rotational power by the output shaft 12 at the left end.
Also used as a steam turbine. In addition, the rotating blade is equipped with the full-blade compressor shown in FIG. 5 and rotated to obtain a high compressed air or a high-speed airflow. The rotating force, the thrust and the levitation force are obtained. Therefore, the superheated steam 5 obtained by heat exchange in the core portion is conveyed to the most upstream side of all the rotor blade steam turbines by the steam control valve 7 and the steam pipe 6 to drive the most upstream side and sequentially downstream. The outer turbine blade group 19 and the outer shaft device, and the inner turbine blade group 20 and the outer turbine device, which drive the sides to generate large rotational power and rotate in opposite directions by the magnetic friction power transmission device 14 at the left end. Combines the inner shaft device with the optimal rotation ratio. 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 the all-blade steam turbine compressor is constructed by combining the all-blade compressors by ratio.

Referring to FIG. 6, a description will be given of a second embodiment of the all blade / steam turbine compressor. Superheated steam 5 obtained by heat exchange in the core portion of various steam gas turbine combined engines is supplied from a center of the right end of the inner shaft device to an upstream side of all the blade steam turbines by a steam pipe 6, and the entire blade steam The turbine is driven to generate rotational force, and is used as rotational power by the output shaft 12 at the left end, and is also used as a full-rotor blade / steam turbine. Also, by using the rotational force, the full-blade compressor shown in FIG. 6 is provided and rotated to obtain high compressed air or high-speed airflow, and obtain rotational force, thrust, levitation, and the like. Therefore, the superheated steam 5 obtained by the heat exchange is conveyed from the steam control valve 7 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. The outer turbine blade group 19 and the outer shaft device, and the inner turbine blade group 20 and the inner shaft device, which generate large rotational power and rotate in the opposite directions by the magnetic frictional power transmission device 14 at the left end. , Combined with the optimal rotation ratio to form an all-blade steam turbine. Further, the right side compressor-side magnetic friction power transmission device 14 allows the inner compressor rotor blade group 17 and the inner shaft device, and the outer compressor rotor blade group 16
By combining the outer shaft device and the optimum contra-rotating rotation ratio to form a full blade compressor, a second embodiment of the full blade steam turbine compressor is provided.

A third embodiment of the steam turbine compressor will be described with reference to FIG. At the core of various steam gas turbine combined engines, the superheated steam 5 obtained by heat exchange drives the steam turbine to generate torque, which is used by the output shaft 12 and used as a steam turbine. In addition, the compressor shown in Fig. 7 is rotated by the rotational force to obtain high compressed air or high-speed airflow, and to obtain rotational force, thrust, levitation, and the like. Therefore, the superheated steam 5 obtained by heat exchange is conveyed from the center of the right end of the inner fixed shaft device to the most upstream side of the steam turbine by the steam pipe 6 through the steam control valve 7 to drive the most upstream side. And the downstream side is sequentially driven to generate a large rotating power, and by rotating the outer turbine blade group 19 and the outer shaft device, which are opposite to the usual, the superheated steam 5 which has become wet steam or water droplets
Can be ejected outward by centrifugal force, the propulsion force is increased as the mass of the compressed air flow is increased, and the outer shaft device is pivotally fitted to the left inner fixed shaft device, and the left end of the outer shaft device is used as the output shaft 12. Make up, steam turbine. The right end of the inner turbine stationary blade shaft and inner fixed shaft device is fixed by a horizontal joint of a casing, and the casing is externally fitted to the inner shaft device also serving as the turbine outer shaft device and the inner compressor blade group 17. Then, the compressor is constituted, and the third of the steam turbine compressor is
An example.

Referring to FIG. 8, a fourth embodiment of the steam turbine compressor will be described. The steam turbine is driven by superheated steam 5 obtained by heat exchange in the core part of various steam gas turbine combined engines to generate torque, and it is used by the output shaft 12 and used as a steam turbine. . In addition, a compressor is provided on the right side and rotated by the rotational force to obtain high compressed air or high-speed airflow, and to obtain rotational force, thrust and levitation force. Therefore, the superheated steam 5 obtained by the heat exchange is conveyed to the most upstream side of the known steam turbine by the steam pipe 6 from the steam control valve 7 to drive the most upstream side as usual, and sequentially. By driving the downstream side, a large rotational power is generated, and the left end of the inner shaft device is connected to the output shaft 1.
As 2, configure a steam turbine that extracts rotational power. That is, a stationary turbine is fixed to a casing that can be disassembled and assembled with a horizontal joint on the outer side of the inner turbine moving blade group 20 and the inner shaft device, and is externally fitted and pivoted to constitute a steam turbine. Similarly, outside the inner compressor rotor blade group 17 and the inner shaft device, a casing to which the stationary vane is fixed is externally fitted and pivoted to form a compressor, which is a fourth embodiment of the steam turbine compressor. .

Referring to FIG. 13, a description will be given of 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 plurality of small-diameter honeycombs and shortened. )
(C) As shown in (d), the water cooling outer wall 26 including at least one or more spiral water pipes 1 is formed into a spiral welding structure with a small number of diameters, thereby setting a large pressure ratio and increasing heat transfer. Acceleration of the heat exchange rate due to the increase in the area and easy addition of the fuel supply means 27 on the most upstream side are facilitated, and the core of the entire steam gas turbine engine has a reasonable cylindrical shape. That is, as in the embodiments shown in (a) and (b), a combustor outer box part 25 is provided slightly outward in the radial direction of the spirally provided water guide pipe 1, and one or more water guide pipes 1 are axially connected. Spiral welding, such as a T-shape, enables the combustor and heat exchanger 4 of the high-pressure vessel to be greatly increased, and also allows the heat transfer area of the combustor and heat exchanger 4 to be increased. Further, as in the embodiment shown in (c), a combustor outer box part 25 to a water-cooled outer wall 26 are provided radially outward of the spirally-provided water guide tube 1 so that one or more water guide tubes 1 are provided.
Is axially spirally welded, enabling the heat transfer area of the combustor / heat exchanger 4 to be increased at a significantly higher pressure than the supercritical steam condition. Further, as in the embodiment shown in (d), a combustor outer box part 25 is provided substantially at the center in the radial direction of the water guide pipe 1 provided in a spiral shape, and one or more water guide pipes 1 are axially spiraled. It enables the heat exchange heat transfer area of the combustor / heat exchanger 4 to be increased below the supercritical steam condition and at a relatively high pressure ratio.

Referring to FIGS. 13 and 14, the water-cooled outer wall unit 52 of the means for increasing the heat transfer area, which has a plurality of small diameter combustor / heat exchangers 4 and is arranged in a honeycomb shape to reduce the size, will be described. . As shown in FIGS. 14A, 14B and 14C, a water-cooled outer wall unit 52 including at least one or more spiral water pipes 1
Is provided with flanges 53 at both ends, and as a unit that can be assembled, a plurality of water-cooled outer wall units 52 are connected to form a main part of the combustor / heat exchanger 4 that can be significantly increased in pressure and shortened. . That is, as in the embodiments shown in FIGS. 13 and 14 (a), (b), (a), and (b), at least one or more spirally provided water pipes 1 are slightly separated radially outward, A combustor outer box part 25 including a welding structure is provided, and flanges 53 are provided at both ends of the combustor outer box part 25. The water pipe 1 is opened in the flange 53, and a water-cooled outer wall unit 52 including the water pipe 1 is provided. To be connectable.
Further, as in the embodiments shown in (c), (d), and (c), at least one or more spirally provided water pipes 1 includes a welding structure at a position radially outward or substantially at the center in the radial direction. An outer box part 25 is provided, and flanges 53 are provided at both ends thereof.
3 and a water-cooled outer wall unit 52 including the water pipe 1 is configured to be connectable, and a combustor / heat unit having a supercritical steam condition or lower and a relatively high pressure ratio is used. Exchanger 4
The heat exchange heat transfer area can be increased.

The magnetic friction power transmission device 14 will be described with reference to FIGS. Various power transmission devices including normal speed change and reverse rotation mainly use a gear device. For this reason, in order to require a sliding tooth surface including a large load on the tooth surface, in addition to requiring lubricating oil, friction heat loss is also very large, and transmission equipment for large power including high speed rotation is required. ,
There is a problem that it cannot be used. For this reason, in order to commercialize an all-blade / steam gas turbine combined engine, an ultra-high-speed and large-power transmission device by rolling contact is indispensable. In order to do so, a power transmission device by rolling contact is required, in which the sliding tooth surfaces of the gear device are almost zero. For this reason,
As shown in FIG. 15, a bar magnet 33 or an electromagnet 34 is provided on the upstream and downstream sides, or on the upstream or downstream side, in the rotation direction 35, as shown in FIG. Using the strong attractive force of the magnet, for example, FIG.
It is preferable to use the entire magnetic friction power transmission device 14 including various combinations of the magnetized friction wheels 37, 37 and the magnetic friction wheels 39, 39 shown in FIG. That is, by approaching rolling contact,
This is an ultra-high-speed large-power transmission device that reduces frictional heat loss to almost zero, and enables pollution-free water cooling in place of lubricating oil.

Referring to FIG. 16, the magnetic friction power transmission device 14 will be described. In place of various gears, various types of magnetic friction wheels 37, 37 and various magnetic friction wheels 39, 39 are used.
The power transmission surface 31 is provided with low unevenness 40 as, for example, 41 flat unevennesses instead of spur gears, 42 helical unevennesses instead of helical gears, and 43 Yamaha unevennesses instead of yamaba gears. As a result, various types of 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.

[0031]

According to the present invention, the outer wall of a combustor / heat exchanger is provided with a spiral welding structure or a welding structure including a water pipe as a core part of various steam gas turbine combined engines including all blades. The spiral water-cooled outer wall unit assembly structure includes a small number of small-diameter, honeycomb-like arrangements, so the outer shape of the core of the steam-gas-turbine combined engine can be easily expanded as an ideal cylindrical type, and it has a great effect of being compact. .
In addition, as a combustor and heat exchanger for the high-pressure vessel with an increased heat transfer area, the fuel supply means is also easily added to the most upstream side up to four times that of the conventional technology, and the majority of the supplied heat is converted to superheated steam. There is an effect that can be converted. The heat exchange raises the inlet temperature of the gas turbine from below the heat-resistant limit temperature of the turbine to 400
The effect is that the exhaust temperature is around 0 ° C and the exhaust loss is around 0%. When rotational power is obtained by the combustion gas and superheated steam obtained by heat exchange, and the amount of compressed air for combustion is the same as that of the conventional technology, the stoichiometric air-fuel ratio is at most about four times that of the conventional gas turbine. It has the effect of greatly increasing the amount of heat to be supplied to the combustion and the mass of the combustion gas due to the heat exchange, thereby greatly increasing the specific output.
By utilizing the amount of air compressed for combustion for 100% combustion, superheated steam at a pressure close to 10 times the normal pressure ratio and below the supercritical pressure can be injected, and as a steam gas turbine united cycle with the highest thermal efficiency, It has a great effect on a large increase in thermal efficiency.

The gas turbine pressure ratio can be increased to the limit by the infinite cooling of the heat exchange combustion gas, and the heat efficiency of the gas turbine can be increased 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, is maximized, and the overall specific output and thermal efficiency can be increased to the limit. Furthermore, since heat is exchanged with the pressure ratio raised to the limit, the gas turbine inlet temperature is set to around 400 ° C, which has the effect of minimizing the amount of heat consumed, maximizing the combustion gas mass, and increasing the thermal efficiency to the limit. . Furthermore, since the combustion gas that has undergone infinite heat exchange is used with the pressure ratio raised to the limit, the exhaust temperature of the gas turbine can be reduced to around 0 ° C, and the heat energy can be effectively used to the limit. Also, by developing and using various magnetic friction power transmission devices, friction loss by various power transmission devices of the prior art is greatly reduced, and there is an effect of further increasing thermal efficiency. Therefore, it can be used as a variety of transportation equipment and co-supply equipment of heat, electricity and cold, etc., and has a great effect to reduce CO2 on a global scale.

The most significant feature of the present invention is that the gas turbine and the steam turbine are separated, so that the thermal efficiency of the most advanced thermal power generation equipment, which is most commonly spread around the world, can be maximized. In other words, in a state-of-the-art steam and gas turbine combined cycle power generation facility, the amount of heat supplied to the steam turbine cycle is small because the waste heat of the gas turbine is recovered and the steam turbine cycle is driven. Therefore, the present invention
As a combustor / heat exchanger, for example, an outside air temperature of 0 ° C. and a pressure ratio of 6
At 0, the air temperature is 600 ° C, which is almost the same as the waste heat recovery temperature. In addition to being able to recover a large amount of outside air heat energy, the heat energy supplied by fuel combustion is also greatly increased. Heat energy to be supplied,
It has the effect of increasing the overall thermal efficiency to about 80% by increasing it by about 10 times.

[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 a core portion of a combined steam gas turbine engine.

FIG. 5 is a partial sectional view showing a first embodiment of the steam turbine compressor.

FIG. 6 is a partial sectional view showing a second embodiment of the steam turbine compressor.

FIG. 7 is a partial sectional view showing a third embodiment of the steam turbine compressor.

FIG. 8 is a partial sectional view showing a fourth embodiment of the steam turbine compressor.

FIG. 9 is an overall configuration diagram showing a first embodiment of the combined steam gas turbine engine.

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

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

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

FIG. 13 is a sectional view showing a spiral welding structure of a water-cooled outer wall of the combustor / heat exchanger.

FIG. 14 is a cross-sectional view for explaining a spiral water cooling wall tube unit of the combustor / heat exchanger.

FIG. 15 is a conceptual diagram of a magnetic friction power transmission device for a steam gas turbine combined engine.

FIG. 16 is a view for explaining friction increasing means such as a magnetic friction wheel and a magnetic friction wheel.

[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 blade group 17: Inner compressor blade group 19: Outer turbine blade group 20: Inner turbine blade group 21: Annular outlet
22: Annular receptacle 23: Annular receptacle 24: Annular nozzle group 25: Combustor outer box 26:
Water cooling outer wall 27: Fuel supply means 28: Bypass
29: Injector 30: Superheated steam reservoir 31: Power transmission surface 33: Bar magnet 34: Electromagnet 35: Rotation direction 36: Magnetic pole 37: Magnetized friction wheel 38: Inner magnetized friction wheel 39: Magnetically bonded friction wheel 40: Low unevenness 4
1: flat unevenness 42: boss unevenness 43: yamaba unevenness 44: inner magnetized friction wheel 45: friction increasing durability means
46: Magnet part 47: Yoke (for magnetized friction wheel)
48: Insulating material 52: Water-cooled outer wall unit 53: Tsuba

Claims (119)

[Claims] 1. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure, and is arranged in a short shape with a large number of small diameter honeycombs.
An all-blade compressor that supplies compressed air to the combustor / heat exchanger, an all-blade gas turbine that obtains output with combustion gas, and heat-exchanges 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 nozzle (29) for obtaining an output with the obtained superheated steam and a superheated steam reservoir (30) for supplying superheated steam to the nozzle. 2. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure with a small diameter and a large number of honeycombs, and a full-movement supplying compressed air to the combustor / heat exchanger. A blade compressor, an all-blade gas turbine that obtains output with combustion gas, and an injection port (29) 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. A combined steam gas turbine engine having a superheated steam reservoir (30) for supplying superheated steam to an injection port. 3. A spiral water-cooled outer wall unit assembling structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
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;
A superheated steam reservoir (30) for supplying superheated steam to the injection port. 4. A combustor / heat exchanger in which a water-cooled outer wall is formed in a spiral welding structure, and is arranged in a short shape in the form of a large number of small diameter honeycombs.
A compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output using combustion gas, and an output that uses 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 a superheated steam reservoir (30) for supplying superheated steam to the nozzle. 5. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and has a small diameter and many honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. A gas turbine that obtains output with combustion gas, an injection port (29) 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 supplies superheated steam to the injection port. A combined steam and gas turbine having a superheated steam reservoir (30). 6. A spiral water-cooled outer wall unit assembly structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a large number of small diameters, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains an output from combustion gas, A combined steam and gas turbine engine having an injection port (29) for obtaining an output with superheated steam obtained by heat exchange so as to be below the limit temperature, and a superheated steam reservoir (30) for supplying superheated steam to the injection port. 7. The combined steam and gas turbine engine according to claim 4, wherein one of the compressor and the gas turbine is a full moving blade. 8. The method according to claim 1, wherein the compressor, gas turbine, combustor and heat exchanger and the superheated steam reservoir (30) are separated between the stop valve (13). A combined steam gas turbine engine. 9. A steam gas turbine combined engine, wherein the superheated steam reservoir (30) has a water pipe (1) densely packed in a cylindrical spiral shape with a honeycomb shape in cross section. 10. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
A combined steam gas turbine engine comprising: a full-rotor 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 a turbine heat-resistant limit temperature. 11. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welding unit unit assembling structure, and is compactly arranged in a small-diameter multi-honey structure. A blade compressor, an all-blade gas turbine that obtains output with combustion gas, and a full-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 resistance limit temperature. Steam gas turbine combined engine having. 12. A combustor / heat exchanger which is arranged in a spiral shape in a water-cooled outer wall unit assembling structure and has a small diameter and a large number of honeycombs, and an all-blade compressor which supplies compressed air to the combustor / heat exchanger. And a full-blade steam turbine that obtains output with combustion gas, and a full-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 resistance limit temperature. Turbine united engine. 13. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a large number of small diameters, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains an output with combustion gas, and a combustion gas temperature that is turbine heat resistant. A combined steam gas turbine engine having a steam turbine that obtains output with superheated steam obtained by heat exchange so as to be lower than a limit temperature. 14. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembling structure in which the outer wall is shortened and arranged in a plurality of small diameter honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine that obtains output with combustion gas,
A steam gas turbine combined engine comprising: a steam turbine that obtains an output using superheated steam obtained by performing heat exchange so that a combustion gas temperature is equal to or lower than a turbine heat resistance limit temperature. 15. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and A combined steam gas turbine engine having a gas turbine that obtains output with gas, and a 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. 16. The method according to claim 13, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 17. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
A device for levitating and moving an aircraft body by the thrust of a full-blade steam turbine compressor 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. Turbine united engine. 18. A combustor / heat exchanger in which a water-cooled outer wall is formed as a helical welding unit as a unitary structure, and a combustor / heat exchanger which is arranged in a short shape in the form of a large number of small-diameter honeycombs. A blade compressor, an all-blade gas turbine that obtains output with combustion gas, and an all-blade steam turbine compressor that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature And a device for levitating and moving the aircraft body by the thrust force. 19. A combustor / heat exchanger which is arranged as a spiral-shaped water-cooled outer wall unit assembling structure in the form of a plurality of small diameter honeycombs, and an all-blade compressor which supplies compressed air to the combustor / heat exchanger. And the thrust of a full-blade steam turbine compressor that obtains output with combustion gas and a full-blade steam turbine compressor that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat-resistant limit temperature And a device for levitating and moving the aircraft body. 20. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a large number of small diameters, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains an output from combustion gas, A combined steam gas turbine engine having a device for levitating and moving an aircraft body by a thrust of a steam turbine compressor that obtains an output with superheated steam obtained by heat exchange so as to be equal to or lower than a limit temperature. 21. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembling structure and has a small diameter and a large number of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine that obtains output with combustion gas,
An apparatus for lifting and moving an aircraft body by means of a thrust of a steam turbine compressor 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. . 22. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger which is arranged in a short shape in the form of a plurality of small-diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and A gas turbine that obtains output with gas and a steam turbine compressor 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 are used to lift and move the aircraft body. A combined steam and gas turbine engine having a device. 23. The combined steam and gas turbine engine according to claim 20, wherein at least two of the compressor, the steam turbine compressor, and the gas turbine are all blades. 24. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
A device for levitating and moving a ship by the power of a full-blade steam turbine compressor that obtains 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. Coalition organization. 25. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welding structure unit assembling structure in a small-diameter multi-honey structure, and a full-movement supplying compressed air to the combustor / heat exchanger. A blade compressor, an all-blade gas turbine that obtains output with combustion gas, and an all-blade steam turbine compressor that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature And a device for levitating and moving a ship by the force of (1). 26. A combustor / heat exchanger which is arranged as a spiral water-cooled outer wall unit assembling structure in the form of a plurality of small diameter honeycombs, and a full blade compressor which supplies compressed air to the combustor / heat exchanger. With the power of the full-blade gas turbine, which obtains output with combustion gas, and the full-blade steam turbine compressor, which 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. And a device for levitating and moving a ship. 27. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a large number of small diameters, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains an output with combustion gas, and a combustion gas temperature that is turbine heat resistant. A combined steam gas turbine engine having a device for levitating and moving a ship by the power of a steam turbine compressor that obtains output with superheated steam obtained by exchanging heat so that the temperature becomes equal to or lower than a limit temperature. 28. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and has a small diameter and a large number of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine that obtains output with combustion gas,
A steam turbine combined engine having a device for levitating and moving a ship by the power of a steam turbine compressor that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than a turbine heat-resistant limit temperature. 29. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger which is arranged in a short shape in the form of a small number of honeycombs; a compressor for supplying compressed air to the combustor / heat exchanger; A device that lifts and moves a ship by the power of a gas turbine that obtains output with gas and a steam turbine compressor that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. And a combined steam and gas turbine engine. 30. The combined steam / gas turbine engine according to claim 27, wherein at least two of the compressor, the steam turbine compressor, and the gas turbine are all blades. 31. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
A device for lifting the airframe by rotating the propeller and rotating the propeller using the output and thrust of a full-blade steam turbine that obtains output using superheated steam obtained by heat exchange so that the combustion gas temperature is below the turbine heat-resistant limit temperature And a combined steam and gas turbine engine. 32. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and is arranged in a short shape in the form of a large number of small diameter honeycombs, and a full motion for supplying compressed air to the combustor / heat exchanger. A blade compressor, 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. A combined steam gas turbine engine having a device for lifting and moving an airframe by rotating a propeller using output and thrust. 33. A combustor / heat exchanger which is arranged as a spiral-shaped water-cooled outer wall unit assembling structure in the form of a plurality of small diameter honeycombs, and a full blade compressor which supplies compressed air to the combustor / heat exchanger. Power and thrust of a full-rotor blade gas turbine that obtains output with combustion gas, and a full-rotor blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat-resistant limit temperature And a device for rotating the propeller to levitate and move the airframe. 34. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a large number of small diameters, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains an output with combustion gas, and a combustion gas temperature that is turbine heat resistant. A combined steam and gas turbine engine having a device for rotating a propeller to levitate and move an airframe by using an output and a thrust of a steam turbine that obtains an output with superheated steam obtained by heat exchange so as to be equal to or lower than a limit temperature. 35. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and is arranged in a short shape with a large number of small diameter honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine that obtains output with combustion gas,
A device for rotating the propeller to levitate the airframe by using the output and thrust of a 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. Steam gas turbine combined engine. 36. As a spiral water-cooled outer wall unit assembling structure, a combustor / heat exchanger which is arranged in a short form in a small number of honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and The propeller is rotated by the output and thrust of the gas turbine that obtains output with gas and the 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. And a device for levitation movement. 37. The method according to claim 34, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 38. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
A device for floating the hull by rotating a propeller by using the output and thrust of an all-blade steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. And a combined steam and gas turbine engine. 39. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembling structure and is arranged in a short shape in a plurality of small diameter honeycombs; A blade compressor, 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. A combined steam and gas turbine engine having a device for lifting and moving a hull by rotating a propeller with output and thrust. 40. A combustor / heat exchanger which is arranged in a spiral shape in a water-cooled outer wall unit assembling structure and has a small diameter and a large number of honeycombs, and an all-blade compressor for supplying compressed air to the combustor / heat exchanger. Power and thrust of a full-rotor blade gas turbine that obtains output with combustion gas, and a full-rotor blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat-resistant limit temperature And a device for rotating the propeller to levitate and move the hull. 41. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a large number of small diameters, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains an output with combustion gas, and a combustion gas temperature that is turbine heat resistant. An integrated steam gas turbine engine comprising: a device for rotating a propeller to levitate and move a hull by an output and a thrust of a steam turbine that obtains an output with superheated steam obtained by heat exchange so as to be below a limit temperature. 42. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure so as to be shortened in a plurality of small diameter honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine that obtains output with combustion gas,
A device for rotating a propeller to lift and move the hull by using the output and thrust of a 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 resistance limit temperature. Steam gas turbine combined engine. 43. As a spiral water-cooled outer wall unit assembling structure, a combustor / heat exchanger which is arranged in a short shape in a small-diameter multiple honeycomb structure, a compressor for supplying compressed air to the combustor / heat exchanger, The propeller is rotated and the hull is rotated by the output and thrust of the gas turbine that obtains output with gas and the steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature becomes lower than the turbine heat-resistant limit temperature. And a device for levitation movement. 44. The method according to claim 41, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 45. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a small diameter, a full blade compressor that supplies compressed air to the combustor / heat exchanger, and a full blade gas turbine that obtains output with combustion gas. ,
A power transmission device for rotating and moving wheels by means of output from a full-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. Steam gas turbine combined engine. 46. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
The output from superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature is output from the full-rotor blade steam turbine, so that the wheels can be rotated and moved, and the power is generated by the output. A steam gas turbine united engine having a power transmission device for charging and rotating wheels by an electric motor to be movable. 47. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling unit, and is compactly arranged in a small-diameter multi-honeycomb shape, and a full-movement supplying compressed air to the combustor / heat exchanger. A blade compressor, 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. A power transmission device for rotating and moving wheels according to output; 48. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welding structure unit assembling structure, and is compactly arranged in a small-diameter multi-honey structure. A blade compressor, 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 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 power transmission device for rotating wheels to enable movement by an output, and for generating and charging by the output and rotating the wheels by an electric motor to enable movement. 49. A combustor / heat exchanger, which is arranged as a spiral-shaped water-cooled outer wall unit assembling structure in a small-diameter multi-honey structure, and an all-blade compressor for supplying compressed air to the combustor / heat exchanger. With the output of the all-blade gas turbine that obtains output with combustion gas, and the output of the 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, A power transmission device for rotating wheels to move the steam turbine. 50. A combustor / heat exchanger which is arranged in a spiral shape in a water-cooled outer wall unit assembling structure and has a small diameter and a large number of honeycombs, and an all-blade compressor which supplies compressed air to the combustor / heat exchanger. With the output of the all-blade gas turbine that obtains output with combustion gas, and the output of the 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, A combined steam gas turbine engine having a power transmission device for rotating wheels to enable movement, and for generating and charging the output and rotating the wheels by an electric motor to enable movement. 51. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a large number of small diameters, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains an output with combustion gas, and a combustion gas temperature that is turbine heat resistant. A combined steam gas turbine engine having a power transmission device for rotating and moving wheels by using an output from a steam turbine that obtains an output using superheated steam obtained by performing heat exchange so as to be equal to or lower than a limit temperature. 52. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a large number of small diameters, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains an output with combustion gas, and a combustion gas temperature that is turbine heat resistant. With the output from the superheated steam obtained by heat exchange so as to be below the limit temperature, the output from the steam turbine is used to rotate the wheels to enable movement, and the output is used to generate and charge and rotate the wheels using the electric motor. And a power transmission device for making it movable. 53. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and has a small diameter and a large number of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine that obtains output with combustion gas,
A power transmission device for rotating and moving wheels by using an output from a steam turbine that obtains an output from 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. Coalition organization. 54. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure so as to be short and arranged in a small-diameter multi-honey structure, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine that obtains output with combustion gas,
With the output from the steam turbine that obtains the output from the superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, the wheels are rotated to enable movement,
A power transmission device for generating and charging the output and rotating the wheels by an electric motor so as to be movable. 55. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger which is arranged in a short shape in the form of a plurality of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and The output of a gas turbine that obtains output with gas and the output of a 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, for rotating and moving wheels. A combined steam gas turbine engine having a power transmission device. 56. A helical water-cooled outer wall unit assembling structure comprising a combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and The wheels are rotated to enable movement by the output of a gas turbine that obtains output with gas and a 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. And a power transmission device for generating and charging the output and rotating the wheels by an electric motor so as to be movable. 57. The method according to claim 51, wherein the compressor, the steam turbine, or the gas turbine is selected from the group consisting of:
The following is a combined steam gas turbine engine with all blades. 58. The power transmission surface (31) of the railway rail (54) and the wheel (55) is provided with low irregularities (40), respectively, so that the wheel A combined steam gas turbine engine wherein a bar magnet (33) or an electromagnet (34) is provided between the front and rear rails (54) in the traveling direction to apply a suction force. 59. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
A device for rotating a propeller and moving a hull by using an output from a full-blade steam turbine that obtains an output 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. Steam gas turbine combined engine. 60. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure and is shortened and arranged in a small-diameter multiple-honeycomb shape, and a full-motion supplying compressed air to the combustor / heat exchanger. A blade compressor, 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. And a device for rotating a propeller according to an output to move a hull. 61. A combustor / heat exchanger which is arranged in a spiral shape in a water-cooled outer wall unit assembly structure in the form of a plurality of small diameter honeycombs, and an all-blade compressor which supplies compressed air to the combustor / heat exchanger. With the output of the full blade gas turbine that obtains output with combustion gas, and the output of the full 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 a device for moving the hull by rotating the propeller. 62. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in a honeycomb shape with a large number of small diameters, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains an output with combustion gas, and a combustion gas temperature that is turbine heat resistant. A combined steam / gas turbine engine having a device for rotating a propeller to move a hull by using an output from a steam turbine that obtains an output using superheated steam obtained by exchanging heat so that the temperature becomes equal to or lower than a limit temperature. 63. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure so as to be shortened in a plurality of small diameter honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine that obtains output with combustion gas,
A device for rotating a propeller to move a hull by using an output from a steam turbine that obtains an output from 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. Coalition organization. 64. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and The propeller is rotated and the hull is moved by the output of the gas turbine that obtains output with gas and the 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 combined apparatus for a steam gas turbine. 65. The method according to claim 62, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 66. The combined steam and gas turbine engine according to claim 59, wherein an exhaust orifice containing the superheated steam is opened at the bottom of the ship. 67. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
A device for rotating a machine to perform work by using an output from an all-blade steam turbine that obtains an output from superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. Gas turbine combined engine. 68. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure and is shortened and arranged in a small-diameter multi-honey structure, and a full-movement supplying compressed air to the combustor / heat exchanger. A blade compressor, 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. An apparatus for rotating a machine to perform work according to output. 69. A combustor / heat exchanger which is arranged in a spiral shape in a water-cooled outer wall unit assembly structure and has a small diameter and a large number of honeycombs, and an all-blade compressor which supplies compressed air to the combustor / heat exchanger. With the output of the full blade gas turbine that obtains output with combustion gas, and the output of the full 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, An apparatus for rotating a machine to perform work. 70. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that is arranged in a short shape in the form of a large number of small-diameter honeycombs; a compressor that supplies compressed air to the combustor / heat exchanger; a gas turbine that obtains output using combustion gas; A combined steam gas turbine engine comprising: a device for rotating a machine to perform work by using an output from a steam turbine that obtains an output using superheated steam obtained by performing heat exchange so as to be equal to or lower than a limit temperature. 71. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure and is shortened and arranged in a small number of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine that obtains output with combustion gas,
A device for rotating a machine to perform work by an output from a steam turbine that obtains an output from 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. organ. 72. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs; a compressor for supplying compressed air to the combustor / heat exchanger; To rotate a machine to work by the output of a gas turbine that obtains output with 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-resistant limit temperature And a combined steam gas turbine engine having the apparatus. 73. The method according to claim 70, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 74. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger having a small diameter and arranged in a honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, and a full-blade gas turbine generator for obtaining output from combustion gas An all-blade steam turbine 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, heat supply from either of them, And a device for supplying electricity from the generator. 75. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger having a small diameter and arranged in a honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, and a full-blade gas turbine generator for obtaining output from combustion gas Supply of cold heat by the heat and exhaust gas, and an all-blade steam turbine generator 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 device for supplying electricity from the couple. 76. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger having a small diameter and arranged in a honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, and a full-blade gas turbine generator for obtaining output from combustion gas And a full-blade steam turbine generator 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 a device for supplying electricity from each of them. Steam gas turbine combined engine. 77. A combustor / heat exchanger in which the water-cooled outer wall is formed as a spiral welding unit assembly structure with a small diameter and a large number of honeycombs, and a full-movement supplying compressed air to the combustor / heat exchanger. Blade compressor, all-blade gas turbine generator that obtains output with combustion gas, and all-blade 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 combined steam and gas turbine engine having a generator, heat supply from either of the couple, and a device for supplying electricity from the couple's generator. 78. A combustor / heat exchanger in which the water-cooled outer wall is formed as a spiral welding unit unit assembling structure and is shortened and arranged in a small-diameter multi-honeycomb shape, and a full-movement supplying compressed air to the combustor / heat exchanger. A blade compressor, an all-blade gas turbine generator that obtains output with combustion gas, supply of cold heat by the heat and exhaust gas,
Steam having an all-blade steam turbine generator that obtains 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 device for supplying electricity from the respective turbines Gas turbine combined engine. 79. A combustor / heat exchanger in which the water-cooled outer wall is formed as a spiral welded unit assembling structure and is shortened and arranged in a small-diameter multi-honeycomb shape, and a full-movement supplying compressed air to the combustor / heat exchanger. A blade compressor, an all-blade gas turbine generator that obtains output with combustion gas, and an all-blade 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 combined steam gas turbine engine having a generator and a device for supplying electricity from the couple. 80. A combustor / heat exchanger, which is arranged in a spiral shape in a water-cooled outer wall unit assembly structure and has a small diameter and a large number of honeycombs, and a full blade compressor that supplies compressed air to the combustor / heat exchanger. And a full-blade steam turbine generator that obtains output with combustion gas, and a full-blade steam turbine generator 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. , Heat supply from either husband or husband,
And a device for supplying electricity from the couple. 81. A combustor / heat exchanger, which is arranged as a spiral-shaped water-cooled outer wall unit assembling structure in a small-diameter multi-honey structure, and an all-blade compressor for supplying compressed air to the combustor / heat exchanger. And an all-blade gas turbine generator that obtains output with combustion gas, supply of the heat and cold heat, and 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. A combined steam and gas turbine engine having an all-blade steam turbine generator and a device for supplying electricity from the couple. 82. A combustor / heat exchanger, which is arranged as a spiral-shaped water-cooled outer wall unit assembling structure and has a small diameter and a large number of honeycombs, and an all-blade compressor for supplying compressed air to the combustor / heat exchanger. And a full-blade steam turbine generator that obtains output with combustion gas, and a full-blade steam turbine generator 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 a device for supplying electricity from the couple. 83. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger, which is arranged in a short shape in the form of a large number of small diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine generator that obtains output using combustion gas, and A steam turbine generator that obtains output with superheated steam obtained by exchanging heat so as to be equal to or lower than the turbine heat resistant limit temperature, a device for supplying heat from any one of the two, and a device for supplying electricity from the couple And a combined steam and gas turbine engine. 84. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small-diameter honeycombs; a compressor for supplying compressed air to the combustor / heat exchanger; a gas turbine generator for obtaining an output from combustion gas; A steam having a supply, a steam turbine generator 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, and a device for supplying electricity from the steam turbine generator Gas turbine combined engine. 85. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger, which is arranged in a short shape in the form of a large number of small diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine generator that obtains output using combustion gas, and A combined steam gas turbine engine comprising: a steam turbine generator for obtaining an output with superheated steam obtained by heat exchange so as to be equal to or lower than a turbine heat resistance limit temperature; and a device for supplying electricity from the steam turbine generator. 86. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and is arranged in a short shape in a small number of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. A gas turbine generator that obtains output with combustion gas, and a steam turbine 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 heat-resistant limit temperature. A combined steam and gas turbine engine having heat supply from the steam generator and a device for supplying electricity from the couple. 87. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembling structure and is arranged in a short shape in a small number of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. A gas turbine generator that obtains output with combustion gas, and a steam turbine generator that obtains output with superheated steam obtained by supplying heat and cold heat and exchanging heat 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 power plant and a device for supplying electricity from the couple. 88. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and is arranged in a short shape in a small number of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. A gas turbine generator that obtains output with combustion gas, a steam turbine generator 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 device for supplying electricity. 89. As a spiral water-cooled outer wall unit assembling structure, a combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, A gas turbine generator that obtains output with gas, a steam turbine 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 heat-resistant limit temperature, and heat from either of them A combined steam gas turbine engine having a supply and a device for supplying electricity from the couple. 90. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger which is arranged in a short shape in a small-diameter multi-honey structure, a compressor for supplying compressed air to the combustor / heat exchanger, and A gas turbine generator that obtains output with gas, a supply of the heat and cold heat, and a steam turbine 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 heat resistance limit temperature, And a device for supplying electricity from the couple. 91. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and A gas turbine generator that obtains output with gas, a steam turbine generator 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 supplies electricity from each of them. Steam gas turbine combined engine having a device for performing 92. The method according to claim 83, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 93. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger, which is arranged in a short shape in a small number of honeycombs, an all-blade compressor for supplying compressed air to the combustor / heat exchanger, and a total exhaust gas temperature of about 0 ° C. which obtains an output with combustion gas. A rotor blade gas turbine generator, a full rotor blade steam turbine generator with a condenser 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 device for supplying electricity to the steam gas turbine. 94. A combustor / heat exchanger in which the water-cooled outer wall is formed as a helical welded structural unit as a unitary structure in a small-diameter multiple-honeycomb arrangement, and a full-movement supplying compressed air to the combustor / heat exchanger. Wing compressor and exhaust temperature 0 to obtain output from combustion gas
All rotor blade gas turbine generator with a condenser 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 a device for supplying electricity from the couple. 95. A combustor / heat exchanger, which is arranged in a spiral shape with a water-cooled outer wall unit and has a small diameter and a large number of honeycombs, and an all-blade compressor that supplies compressed air to the combustor / heat exchanger. And an all-blade gas turbine generator with an exhaust temperature of around 0 ° C, which obtains output from combustion gas, and a condensate, which obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. A combined steam and gas turbine engine having an all-bladed steam turbine generator and a device for supplying electricity from each of them. 96. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger which is arranged in a short form in a small-diameter multiple honeycomb structure, a compressor for supplying compressed air to the combustor / heat exchanger, and a gas turbine generator having an exhaust temperature of about 0 ° C. for obtaining an output from combustion gas And a steam turbine generator with a condenser 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 device for supplying electricity from each of them. A steam gas turbine combined engine having 97. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure and shortened in a small-diameter multi-honey structure, and a compressor for supplying compressed air to the combustor / heat exchanger. And a gas turbine generator with an exhaust temperature of around 0 ° C. that obtains output using combustion gas, and steam with a condenser that obtains output using superheated steam obtained by 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 turbine generator and a device for supplying electricity from the couple. 98. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and A gas turbine generator with an exhaust temperature of around 0 ° C that obtains output with gas, and a steam turbine generator with a condenser that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature And a device for supplying electricity from the couple. 99. The method according to claim 96, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 100. A combined steam gas turbine engine, wherein the combustor / heat exchanger of the all-blade gas turbine injects supercritical steam that is supercritical or lower to reduce NOx by agitated combustion. 101. A steam gas turbine combined engine, wherein a combustor / heat exchanger of the gas turbine injects superheated supercritical steam or less to reduce NOx by agitated combustion. 102. A combined steam gas turbine engine as set forth in claim 102, wherein the exhaust gas temperature of the all-blade gas turbine approaches 0 ° C. 103. The gas turbine, wherein the exhaust gas temperature is set to 0.
A steam gas turbine combined engine characterized by approaching the temperature of ℃. 104. The steam turbine uses superheated steam under supercritical steam conditions.
3. The steam gas turbine combined engine according to any one of 3. 105. 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. 106. 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. 107. The magnetic friction power transmission device (14)
Is a steam gas turbine combined engine having a cooling device. 108. 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. 109. A combined steam gas turbine engine, wherein a bypass is provided in a compressor for supplying the compressed air to a combustor / heat exchanger. 110. A combined steam gas turbine engine, wherein a cooling device is provided in a magnetic friction power transmission device 14 for reversing an inner shaft device and an outer shaft device of the full blade gas turbine. 111. A combined steam gas turbine engine, wherein a cooling device is provided in a magnetic friction power transmission device 14 for reversing an inner shaft device and an outer shaft device of the all-blade compressor. 112. The all-blade steam turbine compressor comprises:
The inner shaft device is provided with an inner turbine blade group (20), and the outer shaft device is provided with an outer turbine blade group (19) and an inner compressor blade group (17). The two shafts are connected by a magnetic friction power transmission device to form a full-blade steam turbine, and an outer shaft device and an outer compressor blade group (16) are provided outside the inner compressor blade group (17), and are mutually inverted. The outer shaft device and the inner shaft device are combined by a magnetic friction power transmission device to form a full blade compressor, and superheated steam (5) is supplied from the center of the inner shaft device.
A combined steam gas turbine engine comprising a device for driving the all-blade steam turbine compressor. 113. The all-blade steam turbine compressor,
An inner shaft unit is provided with an inner turbine blade group (20), and an outer shaft unit is provided with an outer turbine blade group (19). The front inner shaft device is provided with an inner compressor blade group (17), and the outer shaft device and the outer compressor blade group (16) are provided on the outer side, so that the outer shaft device and the inner shaft which are mutually inverted are provided. A device that is combined with a magnetic friction power transmission device to form a full blade compressor, supplies superheated steam (5) from the center of the inner shaft device, and drives the device as the full blade steam turbine compressor. A combined steam gas turbine engine, comprising: 114. The steam turbine compressor, wherein an inner turbine stationary blade is provided on an inner fixed shaft device, and an outer turbine rotor blade group (19) is provided on an outer shaft device, and superheated steam (5) is provided from the center of the inner shaft device. The steam turbine is configured to be drivable by supplying the inner compressor rotor blade group (17) to the outer shaft device, and the inner compressor device blade group (17) is also used as the inner shaft device.
A combined steam and gas turbine engine comprising a compressor and a compressor provided by providing a casing and a stationary vane outside of the steam turbine. 115. In the steam turbine compressor, an inner turbine rotor group (20) is provided in an inner shaft device, and a stationary blade is provided in an outer shaft device, and superheated steam (5) is injected and supplied from the upstream side. A steam turbine is configured so as to be drivable, a compressor is provided by providing an inner compressor moving blade group (17) in a front inner shaft device, and a casing and a stator blade provided outside the inner compressor moving blade group (17). A combined steam gas turbine engine provided as a steam turbine compressor. 116. The all-blade steam turbine compressor comprises:
A combined steam and gas turbine engine, wherein an all-blade compressor is removed to provide a full-blade steam turbine. 117. A combined steam gas turbine engine, wherein the steam turbine compressor is provided as a steam turbine by removing the compressor. 118. The all-blade steam turbine is provided with an inner turbine blade group (20) provided on an inner shaft device and an outer turbine blade group (19) provided on an outer shaft device, so that two shafts which are inverted with respect to each other are provided. An all-blade steam turbine is constituted by coupling with a magnetic friction power transmission device, and a device for supplying superheated steam (5) from the center of the inner shaft device to drive the all-blade steam turbine is provided. Steam gas turbine combined engine. 119. The steam turbine, wherein an inner turbine stationary blade is provided on an inner fixed shaft device, and an outer turbine blade group (19) is provided on an outer shaft device, and superheated steam (5) is provided from a center of the inner fixed shaft device. A steam gas turbine combined engine, wherein a steam turbine is constructed and provided so as to be drivable and supplied.