JP2000038904A - Various kinds of steam gas turbine integrated engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To improve specific power as well as heat efficiency of a gas turbine by effectively utilizing air for combustion which is compressed by heat exchange by using a swage block shaped device which serves as both a combustor and a heat exchanger. SOLUTION: Compressed air 15 for combustion is supplied to receiving ports of a device 4 which serves as both a combustor and a heat exchanger. The receiving ports are arranged by pressurizing pressure in a high level, and are formed by forming their multiple small diameters in a swage block shape. Supplied high compression air 15 is supplied from a fuel supplying means of the most upstream side of the device 4, it is burnt in the device 4 where a heat exchange heating surface area is enlarged. As a result, heat exchange is carried out, and heat exchange cooling NOx is reduced and burnt by a water cooled outer wall of a water leading pipe and a steam pipe. Combustion gas 10 formed by carrying out heat exchange for setting a combustion gas temperature to a turbine heat resistance limit temperature or less, is injected in order toward a downstream side including a first stage of an outer turbine moving blade group and a second stage of an inner turbine moving blade group through a combustion gas sump by the device 4, and thereby, large rotating power is generated.

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 that include a suitable engine.

[0002]

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

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

[0004]

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

[0005] That is, the obstacle to increase the pressure ratio and the specific output of the gas turbine is the fuel calorific value of the supplied calorific value.
In the previous application, the length of the gas turbine combustor was increased to accommodate the infinite number of applications, including various steam turbines.However, in addition to the complicated shape, there are many applications where it is difficult to increase the length. Conversely, it is provided in the shape of a large number of small diameter honeycombs,
High pressure, supply combustion gas from the inner side of superheated steam,
In addition to having a rational cylindrical shape, it also doubles as a heat exchanger with a greatly increased heat transfer area. Provide an engine that can increase the pressure ratio and the specific output to the maximum without exceeding the limit temperature,
For example, it is possible to increase the fuel combustion mass up to a stoichiometric air-fuel ratio up to about four times that of the prior art, and to reduce the amount of heat used by the gas turbine in the supplied heat by increasing the pressure ratio and the fuel combustion mass. And a steam turbine compressor or steam turbine and a gas turbine using superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature. For driving various vehicles, for example, driving various aircraft, driving various ships, or using it for heat and electricity supply equipment.

[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 a numerical value), that is, in the prior art, a large amount of heat energy is consumed and nearly 80% of the compressed air is wastefully exhausted, and in addition, it is used to reduce the combustion temperature, resulting in a large loss. For this reason, air compressed for combustion by heat exchange can be effectively used up to nearly 100%, and for other uses requiring compressed air, a bypass is provided to cope with the pressure ratio and fuel combustion due to heat exchange and temperature decrease. Due to the large increase in mass, the amount of heat used by the gas turbine among the supplied heat is greatly reduced, the thermal efficiency of the gas turbine is greatly increased two to three times, and the specific power is greatly increased. But Superheat including supercritical steam conditions in which the steam turbine and gas turbine are driven by superheated steam obtained by exchanging heat so as to be below the heat-resistant limit temperature of the bin, and the pressure ratio is 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 a factor of about 2 to 3 and to greatly increase the specific output by using steam.

When the gas turbine combustor is shortened in a honeycomb shape with a large number of small diameters and is also used as a heat exchanger having a large heat transfer area, the higher the pressure ratio, the higher the thermal efficiency of the gas turbine becomes. In combustion, the higher the pressure ratio, the higher the temperature can be obtained, and the higher the gas temperature at the turbine inlet is 700 C to 1000 C, the easier the heat exchange. For this reason, the heat transfer area of the heat exchanger can be reduced and shortened, so that the fuel supply means is possible only on the most upstream side, and NOx reduction combustion by cooling is also possible. Further, the present invention provides an ultra-high-performance and ultra-high-efficiency steam-gas-turbine combined engine capable of effectively utilizing the calorific value to the utmost, which enables a significant reduction in exhaust loss due to an increase in pressure ratio and a decrease in heat exchange exhaust heat temperature. At the same time, make the most of the magnetic friction power transmission device,
The purpose is to reduce power transmission loss to the limit.

[0008]

SUMMARY OF THE INVENTION The combustion gas as the working gas of the prior art gas turbine generally has a very high proportion of air and contains about four times the theoretical mixing ratio. In other words, a large amount of heat energy is consumed, and about 80% of the compressed air is wasted, and in addition, it is used for lowering the combustion temperature, resulting in a large loss. In order to make it possible to effectively use approximately 100% of the generated air, the combustor / heat exchanger is shortened into a small number of honeycombs according to the application, and the combustion gas is supplied from the most upstream side of the gas turbine. Along with enabling a cylindrical shape, increasing the pressure and facilitating the addition of only the most upstream side of the fuel supply means,
Spiral welding structure that allows the maximum fuel supply amount to be increased to about four times that of the prior art, greatly increases the heat transfer area as a combustor / heat exchanger, and includes a combustor outer wall including a water pipe. As a water-cooled outer wall or a spiral welding structure, a water-cooled outer wall unit assembly structure or a spiral water-cooled outer wall unit assembly structure, a relatively large pressure ratio is set, and supercritical steam or the like obtained by heat exchange is injected. We provide rockets.

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 pipe 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 a significantly higher pressure,
When the heat exchange amount is small and the diameter is the largest, it becomes a honeycomb shape with a single row on the outer circumference. In addition, since a cylindrical combustor / heat exchanger is provided in a honeycomb shape, a space can be formed. However, the space may be a space combustor / heat exchanger not shown in the figure. d) Use a water-cooled external wall combustor / heat exchanger. The heat exchange lowers the turbine inlet temperature to below the turbine heat-resistant limit temperature, brings the total compressed air compressed for combustion closer to the stoichiometric air-fuel ratio combustion, and increases the fuel combustion mass up to about four times, thereby generating fuel heat. By converting the use of superheated steam into superheated steam, including the supercritical steam conditions, the pressure ratio rises nearly 10 times that of air compression, greatly increasing thermal efficiency and specific power, saving fuel, and reducing combustion gas. The superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature drives the gas turbine and the steam turbine,
The rotating power rotates propellers, wheels, generators, machines, etc. to drive various aircraft, automobiles, ships, machines, etc., and, depending on the application, injects superheated steam exhaust or combustion gas exhaust to produce various aircraft, ships, etc. We will provide equipment that promotes levitation exhaust injection, including a control device that controls the husband and wife.

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 having a pressure ratio of about 10 times that of air compression, it is possible to obtain a large volume far exceeding 1700 times, and a large increase in thermal efficiency. The best way to effectively utilize substantially all of the air for combustion is to convert and use the most efficient superheated steam, 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 in an atmosphere of high temperature and high pressure as much as possible. The maximum amount of heat (superheated steam) extracted from the fuel is obtained to obtain superheated steam most efficiently, the mass of combustion gas driving the steam gas turbine is maximized, and the amount of heat of the driven combustion gas is minimized by the heat exchange. In addition to driving the steam gas turbine with high thermal efficiency, the heat of the exhaust gas is drastically injected as a small amount of low-temperature exhaust gas to significantly reduce the exhaust loss as a low-temperature exhaust gas. Including and using any auxiliary equipment by using or using the magnetic friction power transmission device of the previous application appropriately or entirely instead of the gear device used and used normally. , As a drive device for transmitting the most efficient power, the highest thermal efficiency of the steam gas turbine cycle comprising Zendotsubasa, we will a large increase in the 2-fold to 3-fold the front and rear.

[0011]

DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiments and examples of the present invention will be described with reference to the drawings. The reference numerals are given and the overlapping description is omitted, and the characteristic portions and the portions that are insufficiently described will be sequentially described. In addition, some parts are described with numbers in order to specifically and clearly explain the intended and expected aspects of the invention, but are not limited to numbers.
Further, the combustor / heat exchanger 4 used in the present invention, which has been enlarged in the previous application, is shortened into a large number of small-diameter honeycombs to increase the heat transfer area of the heat exchanger. Gas,
A rational shape was adopted for the configuration to supply to the most upstream side of the turbine cascade. 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. A relatively large pressure ratio is set as the combustor / heat exchanger 4 which is shortened in a shape, and the steam pipe 6 is provided inside in a substantially spiral shape or a nearly straight spiral shape, for example, to generate power not shown in the figure. As a combustor / heat exchanger 4 which is provided with a machine and an electric motor and is also used as a heat and electricity co-supply facility and as a starting device, and is shortened into a large number of small diameter honeycombs,
Providing a large number of fuel supply means 27, such as providing them at the most upstream side of each husband, facilitates the expansion of the fuel supply means 27 and greatly increases the heat exchange rate.

Referring to FIG. 1 and FIG. 2, an embodiment of a core portion of a combined blade / steam gas turbine engine will be described. The idea of a fixed blade is that when a vehicle is pushed by hand and the vehicle is moved, a brake is applied. Pushing it while it is very tired, but the workload is 0, and you can move easily by releasing the brake and pushing.
Therefore, if a compressor or a turbine has a stationary blade, a large loss of energy will 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 set to approximately 2
To increase the specific power and the thermal efficiency greatly, or to reduce the peripheral speed by approximately half of that of the prior art so that the allowable stress is reduced to approximately one-fourth.
It is intended to greatly increase the thermal efficiency while enabling various designs (commercial or household combined use of heat and electricity, etc.) such as low cost and quiet.

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. Referring to another explanation, air is normally sucked in from the first stage 16 of the replaced outer compressor blade group at the right end of the whole rotor compressor, and the inner compressor blade group 17 of the even number stage and the outer side of the odd number stage are sucked. The compressor blade group 16 cooperates to efficiently compress the air by all the blades, and compresses the compressed air 15 from the outer compressor blade group final stage 16 through the annular outlet 21 through the annular receiving port 22, From the compressed air reservoir 8, the combustor / heat exchanger 4 which has been shortened into a large number of small diameter honeycombs to increase the heat transfer area.
The high-compressed air 15 supplied is supplied from a fuel supply means 27 on the upstream side of each of them according to a command from a known control device (not shown). Combustion and heat exchange are performed while controlling combustion in the combustor / heat exchanger 4 so that the fuel is mixed and stirred and burned, including substantially stoichiometric air-fuel ratio combustion, so that the combustion gas temperature becomes lower than the turbine heat resistant limit temperature. Then, the combustion gas 10 is cooled by the water cooling outer wall 26 and the steam pipe 6 of each of the water guide pipes 1 and the combustion gas 10 obtained by the NOx reduction combustion is annularly combusted by the respective combustor / heat exchanger 4. Through the gas reservoir 9 and the annular injection port group 24, it is supplied to the outer turbine blade group 1 stage 19 of the full blade gas turbine having the annular receiving port 23, and the rotary power is sequentially generated downstream and exhausted. You.

Most of the supplied heat energy is converted to superheated steam 5 and is passed through a steam control valve 7 including a steam pipe 6 of a combustor / heat exchanger 4 and a control device, or a superheated steam reservoir 30 or From the most upstream side of the steam turbine of the steam turbine compressor including all the moving blades to the outer turbine moving blade group 1 stage 19 or the inner turbine stationary blade or the prior art stationary blade, and sequentially downstream as usual. , Which in turn generates a large rotation output to drive the compressor strongly. The superheated steam that has been supplied to the downstream side and has become wet steam or water droplets is injected to the outer peripheral side by centrifugal force from the outer turbine blade group 19 except for those using the conventional stationary blade, and includes all the blades. Used to increase thrust as injection mass together with compressor injection air flow. In other words, the gas turbine and the steam turbine are driven to obtain a rotational force, and the respective exhausts are spouted to inject the right front air strongly to the left rear to require the rotational force and the levitation propulsion force. Various uses, for example, used for injection propulsion of various aircraft and ships such as helicopters and jet aircraft, or used for levitation injection propulsion of intermediate between aircraft and ships, or the superheated steam reservoir 30 and It is used as a rocket that injects superheated steam into a vacuum by providing an injection port 29, or is used to rotate a propeller, wheels, a generator, a machine, etc., and the pressure ratio is 10 times that of a conventional air compressor. The core of the combined rotor and steam gas turbine engine, which has various known control devices, will greatly increase the thermal efficiency, propulsion efficiency and levitation propulsion efficiency due to the near superheated steam.

Referring to FIG. 1, the heat transfer area of the combustor / heat exchanger 4 can be easily increased and the small-diameter multi-honey structure can be easily shortened. Is installed on the most upstream side about four times as much as the conventional technology. A magnetic friction power transmission device 14 is provided on each of the left and right sides of the center, and an outer compressor rotor group final stage 16 and an outer turbine rotor blade group 1 stage 19 provided in an annular shape are provided on the outer periphery with the inner shaft device fixed thereto. Stuck,
The outer shaft device is rotatably fitted to the outer shaft device, and the two shafts rotating in the opposite directions are respectively connected by the magnetic friction power transmission device 14 at an optimum rotation ratio. The final stage 17 of the blade group and the second stage 20 of the inner turbine blade group are fixed to each other, and the odd-numbered final stage 16 of the outer compressor blade group of the outer shaft device is thereafter mounted.
The odd-numbered stage 16 of the outer compressor blade group is fixed to the outer compressor blade group, and the even-numbered stage 17 of the inner compressor blade group is fixed to the inner compressor blade group final stage 17 to transmit power most efficiently. The drive unit including the magnetic friction power transmission device makes up the entire moving blade and compressor. Then, the outer turbine blade group odd-numbered stage 19 is fixed to the outer turbine blade group first stage 19 of the outer shaft device, and the inner turbine blade group even-numbered stage 20 is fixed to the inner turbine blade group second stage 20. The inner turbine blade group even-numbered final stage 20 is alternately secured to the inner shaft device, and the outer turbine rotor group odd-numbered final stage 1 is secured.
9 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 rotor and steam gas turbine engine.

Referring to FIG. 2, another description will be given of a second embodiment of the core portion of the combined engine with all the moving blades and the steam gas turbine combined with the bypass. In the prior art, a large amount of heat energy is consumed for combustion. Without using nearly 80% of the compressed air, it wastes (reversely lowers the combustion temperature) and emits large amounts of waste, so the compressed air for combustion can be used 100% effectively for combustion. At the same time, 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 and achieve a large increase in 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 includes air that is about four times the stoichiometric air-fuel ratio, the compressed air for combustion does not exceed the heat-resistant limit temperature of the turbine. In order to use 100% for combustion, it is essential to convert most of the supplied heat to superheated steam. Therefore, according to the present invention, the heat exchanger 4 is converted into superheated steam by reducing the size of the combustor / heat exchanger 4 into a large number of small-diameter honeycombs to increase the heat transfer heat exchange area. At the same time, the water-cooled outer wall 26 has a spiral welded structure including at least one or more plurality of water guide tubes 1 or an assembled structure of the water-cooled outer wall unit 52 of the spiral water guide tube 1 including a welded structure. It enables the injection of superheated steam including large rise and supercritical, greatly increases the specific power, and enables almost all of the air compressed for combustion to be effectively used for combustion. A bypass is provided for separate use, and for applications that require rotational force, an output shaft 12 is provided to extract rotational power, eliminating waste of air compression and greatly increasing thermal efficiency.

Another explanation will be given with reference to FIGS. 2 and 5 to 12. As shown in FIG. 2, the air is normally discharged from the first stage 16 of the replaced outer compressor blade group of the rightmost full blade compressor including the bypass 28. Intake, the even-numbered inner compressor blade group 17 and the odd-numbered outer compressor blade group 16 cooperate to compress the air more efficiently by all the blades. Compressed air 15 for combustion is optimally supplied from a bypass 28 passage provided as appropriate according to the application, and is pressurized and arranged in a small-diameter multiple honeycomb form from an annular outlet 21 of the full-blade compressor.
It is supplied to the annular receiving port 22 of the husband's combustor / 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, respectively, at most about four times the conventional technology. Combustor / heat exchanger 4 with an expanded heat exchange heat transfer area, including the mixed fuel and agitated mixed combustion, including approximately stoichiometric air-fuel ratio combustion
The heat exchange cooling NOx is performed by the water-cooled outer wall 26 and the steam pipe 6 of each of the water guide tubes 1 while performing combustion control and combustion in the inside.
Reduce combustion. The combustion gas 10 obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature is transferred from the respective combustor / heat exchanger 4 to the annular receiving port 23 through the annular combustion gas reservoir 9. From the annular nozzle group 24 rotatably inserted and hermetically sealed, the fuel is sequentially injected to the downstream side including the replaced outer turbine blade group 1 stage 19 and the inner turbine blade group 2 stage 20, and a large rotation as usual. Generate power.

The superheated steam 5 obtained by exchanging heat so as to be lower than the heat-resistant limit temperature of the turbine is passed through the steam control valve 7 of the respective combustor / heat exchanger 4 and the steam shown in FIGS. As shown in FIGS. 10 and 11, the pipe 6 supplies the steam to the uppermost stream 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 rotational force. A compressor including all blades is driven by a steam turbine to generate thrust or rotational force, and together with various core parts as a turboshaft engine, a turboprop engine, a turbojet engine, a turbofan engine, a ship levitation propulsion device, and the like. Used for various aircraft and various ships. Similarly, in FIG. 9, the core portion of the combined engine of the steam gas turbine including all the moving blades, the superheated steam reservoir 30 and the injection port 29 in which the water pipes 1 are densely arranged in a spiral cylindrical shape, are connected between the stop valves 13 and 13. The rocket is configured by making it detachable. FIG. 1
In No. 2, the steam turbine including all the moving blades is driven to be used mainly for driving a propeller, a wheel, a generator, a machine, or the like by the rotational force, and the thrust and the levitation force may be simultaneously used. It is also used as a combined heat and electricity facility to utilize the heat of the turbine, and is a combined rotor / steam gas turbine engine with known various control devices. It is used for many applications like the first embodiment.

Referring to FIG. 2, another explanation will be given. A combustor / heat exchanger 4 which is shortened and arranged in the shape of a large number of small diameter honeycombs is provided, and a magnetic friction power transmission device 14 on the inner left and right sides of the center of the inner shaft device is provided. And the inner shaft devices of the respective compressors, the left and right inner shaft devices are connected to the outer compressor rotor blade group final stage 1 provided annularly.
6 and the outer shaft device to which the outer turbine blade group 1 stage 19 is fixed are rotatably fitted on the outer shaft device, and the two shafts rotating in opposite directions to each other are optimally rotated by the magnetic friction power transmission device 14. And the final stage 17 of the inner compressor blade group and the second stage 20 of the inner turbine blade group are fixed to the respective inner shaft devices. Thereafter, the odd-numbered stage 16 of the outer compressor blade group and the inner compressor The even-numbered stages 17 of the blade groups are alternately fixed, but alternately fixed, including the one with an enlarged outer diameter, as the compressed air bypass used for purposes other than combustion, and the outer compressor rotor blade group 1 stage 1
6, an outer shaft device is fixedly attached to the inner shaft device, and is rotatably fitted to the inner shaft device so as to be rotatably fitted to the outer shaft device. Configure the compressor. The outer turbine blade group 1 stage 19
The outer turbine blade group odd-numbered stage 19 is fixed to the inner turbine blade group even stage 20 and the inner turbine blade group even-number stage 20 is fixed to the inner turbine blade group second stage 20. The stage 20 is fixed to the inner shaft device, the outer turbine blade group odd-numbered final stage 19 is fixed to the outer shaft device, and is rotatably fitted to the inner shaft device so as to be rotatably fitted to the inner shaft device. Constructs the core of the Turbine Combined Engine.

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. Is used as the core of a steam and gas turbine combined engine, and the replacement rotor blades are reduced to conventional stator vanes, enabling the compressor and gas turbine of the conventional technology to be driven. Therefore, the first of FIG.
The elements from the third embodiment to the third embodiment are appropriately replaced, and are used for various purposes, for example, for moving a vehicle and propelling a ship or an aircraft, as in the first embodiment.

Referring to FIG. 3 and FIG. 12 which are close to the steam / gas turbine combined cycle thermal power generation facility, a case where it is used as a state-of-the-art thermal power generation facility will be described in comparison with the prior art. When the generator is driven in the third embodiment using the conventional gas turbine shown in FIG. 3, the combustor / heat exchanger 4 which also uses the combustor as a heat exchanger is provided in a short honeycomb shape with a small diameter and a large number of honeycombs. In addition, it enables various heat exchanges according to the application, achieves up to four times the fuel combustion of the conventional technology with the same amount of compressed air for combustion, and significantly increases the combustion gas mass. , Greatly increase output and allow for significantly lower temperature exhaust. As for the comparison of pressure ratios, the combustion gas temperature can be reduced by heat exchange, so the pressure ratio can be increased to the utmost and the thermal efficiency can be increased. In addition, in order to perform heat exchange with the pressure ratio raised to the limit, the amount of superheated steam energy including supercritical steam conditions extracted from the combustion gas is also compared with the amount of heat energy in the conventional heat recovery heat exchange. It will be too much. Furthermore, since the gas turbine is driven by the combustion gas that has undergone heat exchange with the pressure ratio raised to the limit, the amount of exhaust heat can be minimized. That is, the higher the pressure ratio, the higher the thermal efficiency of the gas turbine, the greater the mass of the combustion gas, the greater the output of the gas turbine, and the lower the calorific value of the exhaust gas, the higher the thermal efficiency of the gas turbine, and the amount of thermal energy extracted from the same fuel amount The more, the higher the steam turbine output and the higher the overall thermal efficiency.

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. Is used as the core of a steam and gas turbine combined engine, and the replacement rotor blades are reduced to conventional stator vanes, enabling the compressor and gas turbine of the conventional technology to be driven. Therefore, the first of FIG.
The elements from the fourth embodiment to the fourth embodiment 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.

Referring to FIG. 5, a first embodiment of the all-blade / steam turbine compressor will be described. The all-blade is obtained by using superheated steam 5 obtained by exchanging heat at the core of various steam gas turbine combined engines. The steam turbine is driven to generate torque, which is used by the output shaft 12 at the left end as torque. Or
By rotating the full-blade compressor shown in Fig. 5 by the rotational force, high compressed air or high-speed airflow is obtained, and rotational force, thrust, levitation, etc. are obtained. Therefore, the superheated steam 5 obtained by heat exchange 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. To generate a large rotational power, and by the magnetic friction power transmission device 14 at the left end,
The outer turbine blade group 19 and the outer shaft device rotating in opposite directions to the inner turbine blade group 20 and the inner shaft device are connected at an optimum rotation ratio. Further, the right-most 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 rotor 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.

Referring to FIG. 6, a description will be given of a second embodiment of the all-blade / steam turbine compressor. The all-blades are obtained by using superheated steam 5 obtained by exchanging heat at the core of various steam gas turbine combined engines. The steam turbine is driven to generate torque, which is used by the output shaft 12 at the left end as torque. Or
The rotating blade compressor shown in Fig. 6 is rotated by the rotational force to obtain high compressed air or high-speed airflow, and obtains rotational force, thrust, levitation, and the like. Therefore, the superheated steam 5 obtained by heat exchange 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. To generate a large rotational power, and by the magnetic friction power transmission device 14 at the left end,
The outer turbine blade group 19 and the outer shaft device rotating in opposite directions and the inner turbine blade group 20 and the inner shaft device are coupled at an optimum rotation ratio to form a full blade steam turbine. Furthermore, the rightmost compressor-side magnetic friction power transmission device 1
4, the inner compressor blade group 17 and the inner shaft device are connected to the outer compressor blade group 16 and the outer shaft device at an optimum counter-rotating rotation ratio to form a full blade compressor, and This is the second embodiment of the turbine compressor.

Referring to FIG. 7, a third embodiment of the steam turbine compressor will be described. The superheated steam 5 obtained by exchanging heat at the core of various steam gas turbine combined engines drives the steam turbine to rotate. A force is generated and used by the output shaft 12. Alternatively, the compressor shown in FIG. 7 is rotated by the rotational force to obtain high compressed air or high-speed airflow, and obtains rotational force, thrust, levitation, and the like. Therefore, the superheated steam 5 obtained by the heat exchange is conveyed to the most upstream side of the steam turbine by the steam control valve 7 and the steam pipe 6 to drive the most upstream side and sequentially drive the downstream side, so that By generating the rotational power and rotating the outer turbine blade group 19 and the outer shaft device, which are opposite to the normal, the superheated steam 5 that has become wet steam or water droplets is ejected outward by centrifugal force,
The propulsion force is increased as the mass of the compressed air flow is increased, and the propulsion force is externally fitted to the inner fixed shaft device at the left end, and the steam turbine is configured with the left end of the outer shaft device as the output shaft 12. The right ends of the inner turbine stator blades and the inner fixed shaft device are fixed by a horizontal joint of a casing, and the casing is externally fitted to and supported by the inner shaft device that is also used as the inner compressor blade group 17 and the turbine outer shaft device. The third embodiment of the steam turbine compressor will be described.

Referring to FIG. 8, a fourth embodiment of the steam turbine compressor will be described. The superheated steam 5 obtained by exchanging heat in the core of the combined steam gas turbine engine drives the steam turbine to rotate it. A force is generated and used by the output shaft 12. Alternatively, the compressor shown in FIG. 8 is rotated by the rotational force to obtain high compressed air or high-speed airflow, and obtains rotational force, thrust, levitation, and the like. Therefore, the superheated steam 5 obtained by heat exchange is supplied from the steam control valve 7 to the steam pipe 6 through the steam pipe 6.
It is conveyed to the most upstream side of a known steam turbine, drives the most upstream side as usual, and sequentially drives the downstream side to generate a large rotational power, and the left end of the inner shaft device is connected to the output shaft 12. As a steam turbine that extracts rotational power. That is, the stationary blade is fixed to a casing that can be disassembled and assembled with a horizontal joint on the outer side of the inner turbine rotor blade group 20 and the inner shaft device, and a steam turbine is configured by externally fitting and pivoting. Similarly, a compressor in which a casing to which a stationary vane is fixed is externally pivotally supported on the outer side of the inner compressor rotor blade group 17 and the inner shaft device to constitute a compressor is referred to as 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. In addition to accelerating the heat exchange rate due to the increase in area and increasing the most upstream side of the fuel supply means 27, the entire steam gas turbine has a reasonable cylindrical shape. That is, (a)
As in the embodiment shown in (b), a combustor outer box part 25 is provided slightly away from the spirally provided water pipe 1 in the radial direction,
One or more water pipes 1 are spirally welded such as in a T-shape in the axial direction to greatly enable the combustor / heat exchanger 4 of the high-pressure vessel and the heat transfer area of the combustor / heat exchanger 4. It also allows for a huge increase. Further, as in the embodiment shown in (c), a combustor outer box 25 to a water-cooled outer wall 26 are provided radially outward of the spirally provided water pipe 1 so that one or more water pipes 1 can be axially connected. Spiral welding makes it possible to greatly increase the heat transfer area of the combustor / heat exchanger 4 with a significantly higher pressure than supercritical steam conditions. or,
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 spirally provided water guide tube 1, and one or more water guide tubes 1 are welded in an axial spiral manner. It enables a large increase in the heat exchange heat transfer area of the combustor / heat exchanger 4 under supercritical steam conditions and at a relatively high pressure ratio.

Referring to FIG. 13 and FIG. 14, the water-cooled outer wall unit 52 of the means for increasing the heat transfer area, which has a large number of small diameter combustor / heat exchangers 4 and is arranged in a honeycomb shape and shortened, 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
As a unit that can be assembled by providing flanges 53 at both ends,
It is the main part of the combustor / heat exchanger 4 that can be connected to multiple water-cooled outer wall units 52 to greatly increase the pressure and reduce the size. That is, as in the embodiments shown in FIGS. 13A and 14B, the at least one or more spirally provided water pipes 1 are slightly separated radially outward from the combustor including the welding structure. A box portion 25 is provided, and flanges 53 are provided at both ends of the box portion 25. The water pipe 1 is opened at the flange 53 so that the water-cooled outer wall unit 52 including the water pipe 1 can be connected. Further, as in the embodiments shown in (c), (d), and (c), at least one or more spirally provided water pipes 1 outside the combustor including a welding structure radially outward or substantially at the center in the radial direction. A box portion 25 is provided, and flanges 53 are provided at both ends thereof. The water pipe 1 is opened at the flange 53 so that the water-cooled outer wall unit 52 including the water pipe 1 can be connected. It enables a large increase in the heat exchange heat transfer area of the combustor / heat exchanger 4 below the critical steam conditions and at a relatively high pressure ratio.

Referring to FIGS. 15 and 16, the magnetic friction power transmission device 14 will be described. Various power transmission devices including normal speed change and reverse rotation mainly use gears.
For this reason, since a sliding tooth surface including a large load is essential for the tooth surface, in addition to requiring lubricating oil, friction heat loss is extremely large, and it is used for transmission of large power including high speed rotation. There is a problem of impossibility. For this reason, in order to commercialize an all-blade / steam gas turbine combined engine, an ultra-high-speed large power transmission device by rolling contact is indispensable, enabling an ultra-high-speed large power transmission device and eliminating the need for lubricating oil. For this purpose, it is necessary to provide a power transmission device by rolling contact, in which the sliding tooth surfaces of the gear device are almost zero. For this reason, the meshing height of the gears is reduced to an infinitesimally low irregularity 40, and 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. For example, various magnetized friction wheels 37, 37 and 39.3 shown in FIGS. 15 and 16 utilizing the strong attraction force of the magnet.
It is preferable to use the magnetic friction power transmission device 14 in its entirety including various combinations such as 9 and the like. In other words, by bringing rolling contact closer, friction heat loss can be reduced to almost zero, and ultra-high-speed large-power transmission equipment and water-free cooling can be achieved in place of lubricating oil.

Referring to 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 irregularities 40, for example, 41 flat irregularities instead of spur gears, 42 helical irregularities instead of helical gears, and 43 Yama irregularities instead of Yamaba gears. As a result, various magnetic friction power transmission devices 14 are configured and used as the magnetic friction power transmission device 14 in the same manner as known various gear type power transmission devices.

[0031]

According to the present invention, the outer wall of a combustor / heat exchanger is provided as a core part of a combined steam and gas turbine engine including all the moving blades, and a spiral welding structure including a water pipe or a spiral structure including a welding structure. The water-cooled outer wall unit assembly structure has a small diameter and a large number of honeycombs, so it is easy to expand the core of the combined engine of the steam and gas turbine into an ideal cylindrical shape. In addition, as a combustor / heat exchanger for a high-pressure vessel with a greatly increased heat transfer area, the fuel supply means can be easily added to the most upstream side up to four times that of the conventional technology, and the majority of the supplied heat can be converted to superheated steam. It has an effect. When the rotating power is obtained by the combustion gas and the superheated steam obtained by exchanging heat without exceeding the heat-resistant limit temperature of the turbine, and the amount of compressed air for combustion is the same as that of the conventional technology, the maximum of the conventional gas turbine is 4%. It has the effect that the heat output can be greatly increased and the specific output greatly increased up to stoichiometric air-fuel ratio combustion with about twice the fuel. Since the amount of air compressed for combustion is used for 100% combustion, superheated steam having a pressure ratio close to 10 times the normal pressure ratio and less than the supercritical pressure can be injected,
As a steam gas turbine combined cycle with the highest thermal efficiency, it has a great effect on a large increase in thermal efficiency.

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

[Brief description of the drawings]

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

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

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

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

FIG. 5 is a 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 steam gas turbine combined engine.

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

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

FIG. 16 is a diagram 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 socket 23: annular socket 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 (107)

[Claims] 1. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure with a small diameter and a plurality of honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. ,
An all-blade gas turbine that obtains output with combustion gas, an injection port (29) that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and superheated steam is supplied to the injection port. A combined steam gas turbine engine having a superheated steam reservoir (30) to supply. 2. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure, and a combustor / heat exchanger shortened into a small-diameter multi-honeycomb shape, and a whole rotor blade for supplying compressed air to the combustor / heat exchanger. A compressor, an all-blade gas turbine that obtains output with combustion gas, and an injection port (2) 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.
9) and a superheated steam reservoir (3) for supplying superheated steam to the nozzle.
0). 3. As a spiral water-cooled outer wall unit assembly structure,
A combustor / heat exchanger that is shortened in a small-diameter multi-honeycomb shape, a full-blade compressor that supplies compressed air to the combustor / heat exchanger, a full-blade gas turbine that obtains output using combustion gas, and combustion. A steam gas turbine having an orifice (29) for obtaining an output with superheated steam obtained by heat exchange so that the gas temperature becomes equal to or lower than the turbine heat resistant limit temperature, and a superheated steam reservoir (30) for supplying the superheated steam to the orifice. Coalition organization. 4. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure with a small diameter and a plurality of honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine that obtains an output by a superheater, an injection hole (29) that obtains an output by using 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 superheated steam reservoir that supplies the superheated steam to the injection hole (30). 5. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure, and a combustor / heat exchanger shortened into a large number of small diameter 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 gas turbine engine having a superheated steam reservoir (30). 6. A spiral water-cooled outer wall unit assembly structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and a combustion gas temperature that is at the turbine heat resistance limit. A combined steam gas turbine engine having an injection port (29) for obtaining an output with superheated steam obtained by heat exchange so as to have a temperature lower than or equal to a 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, the gas turbine, the 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 combined steam gas turbine engine wherein the superheated steam reservoir (30) is formed by densely packing a water guide pipe (1) in a cylindrical spiral shape with a honeycomb structure. 10. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multiple-honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine that obtains output with combustion gas, and a combustion gas Apparatus for lifting 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 temperature is equal to or lower than the turbine heat-resistant limit temperature . 11. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure, and a combustor / heat exchanger shortened into a small-diameter multi-honeycomb shape, and a whole rotor blade for supplying compressed air to the combustor / heat exchanger. Thrust of a compressor, a full-blade gas turbine 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 allowable temperature limit And a device for levitating and moving the aircraft body according to the invention. 12. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. The aircraft body is driven by the thrust of a full-blade gas turbine, which obtains output with combustion gas, and a full-blade steam turbine compressor, which 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 steam turbine. 13. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and the combustion gas temperature is the turbine heat-resistant limit temperature. A combined steam and gas turbine engine having a device for levitating and moving an aircraft body by the thrust of a steam turbine compressor that obtains output with superheated steam obtained by heat exchange as follows. 14. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welded unit assembling structure, the combustor / heat exchanger being shortened into a large number of small diameter honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. To lift the aircraft body by the thrust of a gas turbine that obtains output with combustion 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-resistant limit temperature. A combined steam and gas turbine engine having a device. 15. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger shortened into a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. And a device for levitating and moving the aircraft body by the thrust of a 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. Steam gas turbine combined engine having. 16. The combined steam and gas turbine engine according to claim 13, wherein at least two of the compressor, the steam turbine compressor, and the gas turbine are all blades. 17. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multiple-honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine that obtains output with combustion gas, and a combustion gas A steam turbine combined engine having a device for levitating and moving a ship by the power of a full-blade steam turbine compressor that obtains an output with superheated steam obtained by heat exchange so that the temperature becomes equal to or lower than a turbine heat-resistant limit temperature. 18. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and a combustor / heat exchanger shortened into a small-diameter multi-honeycomb shape, and all blades for supplying compressed air to the combustor / heat exchanger. Compressor, full-blade gas turbine that obtains output with combustion gas, and power of 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 allowable temperature limit And a device for levitating and moving a ship. 19. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. The ship is powered by a full-blade gas 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 levitation movement. 20. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and the combustion gas temperature is the turbine heat-resistant limit temperature. 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 heat exchange as follows. 21. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure having a small diameter and a plurality of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. A device for lifting and moving a ship by the power of a gas turbine that obtains output with combustion 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-resistant limit temperature And a combined steam and gas turbine engine. 22. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger shortened into a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. And a device for levitating and moving the ship by the power of a 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. Steam gas turbine combined engine. 23. The combined steam / 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. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multiple-honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine that obtains output with combustion gas, and a combustion gas A device for floating the airframe by rotating a propeller with the output and thrust of a full-blade steam turbine that obtains output with superheated steam obtained by heat exchange so that the temperature is equal to or lower than the turbine heat-resistant limit temperature Steam gas turbine combined engine. 25. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure, and a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade for supplying compressed air to the combustor / heat exchanger. The output of the compressor, the output of a full-blade gas turbine that obtains output with combustion gas, and the output of a full-blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine allowable temperature limit. A combined device for rotating a propeller by thrust to levitate and move the airframe. 26. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. The propeller is driven by the power and thrust of the full-blade gas turbine, which obtains output with combustion gas, and the full-blade steam turbine, which obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine allowable temperature limit. And a device for rotating the airframe to levitate and move the airframe. 27. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and the combustion gas temperature is the turbine heat-resistant limit temperature. A combined steam and gas turbine engine comprising: a steam turbine that obtains an output with superheated steam obtained by heat exchange as described below; and a device for causing a propeller to rotate by a power and a thrust to levitate and move an airframe. 28. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure, and a compressor for supplying compressed air to the combustor / heat exchanger. The propeller is rotated by the output and thrust of the gas turbine that obtains the output with the combustion gas and the steam turbine that obtains the output with the superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. And a device for levitation movement. 29. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. The propeller is rotated by the power and thrust of the gas turbine that obtains the output and the steam turbine that obtains the output with the superheated steam obtained by exchanging heat so that the combustion gas temperature is lower than the turbine heat resistance limit temperature, and the airframe is lifted and moved. And a combined apparatus for a steam gas turbine. 30. The method according to claim 27, 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. 31. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multiple-honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine that obtains output with combustion gas, and a combustion gas And a device for floating the hull by rotating the propeller with the output and thrust of an all-blade steam turbine that obtains output with superheated steam obtained by heat exchange so that the temperature is equal to or lower than the turbine heat-resistant limit temperature Steam gas turbine combined engine. 32. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a whole rotor blade for supplying compressed air to the combustor / heat exchanger. The output of the compressor, the output of a full-blade gas turbine that obtains output with combustion gas, and the output of a full-blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine allowable temperature limit. An apparatus for rotating a propeller by thrust to lift and move a hull. 33. A helical water-cooled outer wall unit assembling structure, comprising: a combustor / heat exchanger shortened into a large number of small diameter honeycombs; and a full blade compressor for supplying compressed air to the combustor / heat exchanger. The propeller is driven by the power and thrust of the full-blade gas turbine, which obtains output with combustion gas, and the full-blade steam turbine, which obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine allowable temperature limit. And a device for rotating the boat to levitate and move the hull. 34. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and the combustion gas temperature is the turbine heat-resistant limit temperature. An integrated steam gas turbine engine comprising: a steam turbine that obtains an output with superheated steam obtained by heat exchange as described below; and a device for rotating a propeller by means of output and thrust to lift and move the hull. 35. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure having a small diameter and a large number of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. The propeller is rotated by the power and thrust of the gas turbine that obtains output with combustion 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-resistant limit temperature. And a device for levitation movement. 36. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. The propeller is rotated and the hull is levitated by the output and the thrust of the gas turbine that obtains the output and the steam turbine that obtains the output by the superheated steam obtained by exchanging heat so that the combustion gas temperature becomes lower than the turbine heat-resistant limit temperature. And a combined apparatus for a steam gas turbine. 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 that has been shortened into a honeycomb shape with many small diameters,
An all-blade compressor that supplies compressed air to the combustor / heat exchanger, and an all-blade gas turbine that obtains output with combustion gas, are heat-exchanged so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. And a power transmission device for rotating and moving wheels based on the output from the full-blade steam turbine that obtains output using superheated steam. 39. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multiple-honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine that obtains output with combustion gas, and a combustion gas The output is output from superheated steam obtained by heat exchange so that the temperature becomes equal to or lower than the turbine heat-resistant limit temperature. And a power transmission device for rotating wheels by an electric motor so as to be movable. 40. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure and the combustor / heat exchanger is shortened into a small-diameter multi-honey structure, and an all-rotor for supplying compressed air to the combustor / heat exchanger. The output of the compressor, the full-blade gas turbine that obtains output with combustion gas, and 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 allowable temperature limit A power transmission device for rotating wheels to move the steam turbine. 41. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure and the combustor / heat exchanger is shortened into a small-diameter multi-honeycomb shape, and all blades supplying compressed air to the combustor / heat exchanger. The output of the compressor, the full-blade gas turbine that obtains output with combustion gas, and 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 allowable temperature limit 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. 42. As a spiral water-cooled outer wall unit assembly structure, a combustor / heat exchanger shortened into a large number of small-diameter honeycombs, and a full-blade compressor for supplying compressed air to the combustor / heat exchanger. The wheels are rotated by the output of a full-blade gas turbine that obtains output with combustion gas and the 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-resistant limit temperature. And a power transmission device for moving by moving. 43. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. The wheels are rotated by the output of a full-blade gas turbine that obtains output with combustion gas and the 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-resistant limit temperature. And a power transmission device for generating and charging with the output and rotating the wheels with an electric motor to enable movement. 44. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and the combustion gas temperature is the turbine heat-resistant limit temperature. A combined steam and gas turbine engine having a power transmission device for rotating and moving wheels based on output from a steam turbine that obtains output using superheated steam obtained by heat exchange as described below. 45. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and the combustion gas temperature is the turbine heat-resistant limit temperature. The wheels are rotated by the output from the steam turbine that obtains an output from the superheated steam obtained by heat exchange as follows, and the wheels are movable, and the power is generated and charged by the output, and the wheels are rotated by the electric motor to move the wheels. And a power transmission for enabling. 46. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure having a small diameter and a plurality of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. For rotating and moving wheels by the output of a gas turbine that obtains output with combustion gas and a steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine allowable temperature limit. A combined steam gas turbine engine having a power transmission device. 47. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welded unit assembling structure, the combustor / heat exchanger being shortened into a large number of small diameter honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. The wheels are rotated and movable by the output of a gas turbine that obtains output from combustion gas and a steam turbine that obtains 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. And a power transmission device for generating and charging the output and rotating the wheels by an electric motor so as to be movable. 48. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A power transmission device for rotating and moving wheels by using the output of a gas turbine that obtains output from a steam turbine that obtains 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 And a combined steam and gas turbine engine. 49. As a spiral water-cooled outer wall unit assembly structure, a combustor / heat exchanger shortened in the form of a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas The wheel is rotated by the output of the gas turbine that obtains the output and the steam turbine that obtains the output with the superheated steam obtained by performing heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat resistant limit temperature, and the wheel is movable. A power transmission device for generating and charging the output and rotating the wheels by an electric motor so as to be movable. 50. The method according to claim 44, wherein any one of the compressor, the steam turbine, and the gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 51. The power transmission device according to claim 38, wherein the power transmission surface (31) of the rail (54) and the wheel (55) is provided with a low unevenness (40), respectively. 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. 52. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multiple-honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine that obtains output with combustion gas, and a combustion gas And a device for moving a hull by rotating a propeller based on output from a full-blade steam turbine that obtains output using superheated steam obtained by heat exchange so that the temperature is equal to or lower than the turbine heat-resistant limit temperature. Coalition organization. 53. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding unit assembly structure with a spiral shape, and a whole rotor blade for supplying compressed air to the combustor / heat exchanger. The output of the compressor, the full-blade gas turbine that obtains output with combustion gas, and 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 allowable temperature limit And a device for moving the hull by rotating the propeller. 54. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. The propeller is rotated by the output of a full-blade steam turbine that obtains output with combustion gas and the output of a full-blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine allowable temperature limit. And a device for moving the hull. 55. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and the combustion gas temperature is the turbine heat-resistant limit temperature. An apparatus for rotating a propeller to move a hull by an output from a steam turbine that obtains an output from superheated steam obtained by heat exchange as described below. 56. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure, and a compressor for supplying compressed air to the combustor / heat exchanger, wherein the combustor / heat exchanger has a small diameter and a large number of honeycombs. The propeller is rotated by the output of a gas turbine that obtains output with combustion 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 the hull is moved. And a combined apparatus for a steam gas turbine. 57. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger shortened in a honeycomb shape with a small diameter, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A device for moving a hull by rotating a propeller by the output of a gas turbine that obtains output from a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature And a combined steam and gas turbine engine. 58. The method according to claim 55, 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. 59. The combined steam and gas turbine engine according to claim 52, wherein an exhaust orifice containing the superheated steam is opened in a ship bottom. 60. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multiple-honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine that obtains output with combustion gas, and a combustion gas And a device for rotating the machine with the output from the all-blade steam turbine to obtain an output with superheated steam obtained by heat exchange so that the temperature is equal to or lower than the turbine heat-resistant limit temperature, and performing work by rotating the machine. organ. 61. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welding unit assembly structure and has a small diameter and a large number of honeycombs, and a whole rotor blade for supplying compressed air to the combustor / heat exchanger. The output of the compressor, the full-blade gas turbine that obtains output with combustion gas, and 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 allowable temperature limit An apparatus for rotating a machine to perform work. 62. As a spiral water-cooled outer wall unit assembly structure, a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. The machine is rotated by the output of a full-blade gas turbine that obtains output with combustion gas and the 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-resistant limit temperature. And a device for causing the work to be performed. 63. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and the combustion gas temperature is the turbine heat-resistant limit temperature. A combined steam gas turbine engine comprising: a steam turbine that obtains an output with superheated steam obtained by heat exchange as described below; 64. A combustor / heat exchanger in which the water-cooled outer wall has a spiral welding structure unit assembly structure having a small diameter and a large number of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. In order to make the machine work by rotating the machine with the output of the gas turbine that obtains the output with the combustion gas and the steam turbine that obtains the output with the 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. 65. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger shortened into a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A device for rotating a machine by the output of a gas turbine that obtains an output 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-resistant limit temperature, and performing work. A steam gas turbine combined engine having 66. The method according to claim 63, 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. 67. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multi-honeycomb, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine and a generator for obtaining output from combustion gas The heat from the exhaust of each of the rotor blade steam turbines and 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 resistance limit temperature and the output from the generator by the respective outputs And a device for supplying electricity. 68. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multi-honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine and a generator for obtaining output from combustion gas And a device for supplying electricity from a generator based on the output of 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 Turbine united engine. 69. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welded unit assembling structure and the combustor / heat exchanger is shortened into a small-diameter multi-honeycomb shape, and all blades supplying compressed air to the combustor / heat exchanger. A compressor, a full-rotor blade gas turbine that obtains output with combustion gas, a generator, and a full-rotor 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 and gas turbine engine having a device for supplying heat from the exhaust of each of the couples and electricity from a generator based on the outputs of the couples. 70. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welded unit assembling structure and the combustor / heat exchanger is shortened into a small-diameter multi-honeycomb shape, and all blades supplying compressed air to the combustor / heat exchanger. A compressor, a full-blade gas turbine that obtains output with combustion gas, a generator 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 device for supplying electricity from a generator by output. 71. A combustor / heat exchanger shortened into a large number of small diameter honeycombs as a spiral water cooling outer wall unit assembly structure, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. , A combination of a full-blade gas turbine that obtains output with combustion gas, a generator, and a full-blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine allowable temperature limit A combined steam gas turbine engine having a device for supplying heat from the exhaust of the vehicle and electricity from a generator based on the output of each of them. 72. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. , Power generation using 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 supplying electricity from the machine. 73. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multi-honeycomb, a compressor for supplying compressed air to the combustor / heat exchanger, a gas turbine for obtaining output with combustion gas, a generator, and a combustion gas temperature turbine A device for supplying heat from a generator based on the output of each of the steam turbine and a steam turbine that obtains output with superheated steam obtained by heat exchange so as to be below the heat-resistant limit temperature. Steam gas turbine combined engine having. 74. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multi-honeycomb, a compressor for supplying compressed air to the combustor / heat exchanger, a gas turbine for obtaining output with combustion gas, a generator, and a combustion gas temperature turbine An apparatus for supplying electricity from a generator based on the output of a steam turbine that obtains an output with superheated steam obtained by exchanging heat so that the temperature becomes equal to or lower than a heat-resistant limit temperature. 75. A combustor / heat exchanger in which the water-cooled outer wall is formed as a spiral welded unit assembling structure, the combustor / heat exchanger shortened into a small-diameter multi-honey structure, and a compressor for supplying compressed air to the combustor / heat exchanger. The heat generated by the exhaust gas of a gas turbine that obtains output from combustion gas, the power generator, and the heat generated by the exhaust gas of a steam turbine that obtains output by using 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 generator with the output of the husband and the wife. 76. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure, the combustor / heat exchanger being shortened into a large number of small diameter honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. Supplying electricity from a generator using the output of 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 Steam gas turbine combined engine having a device for performing 77. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger shortened into a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. The heat generated by the exhaust gas of each of the gas turbine, the generator, and the steam turbine that obtains the output with the superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and A device for supplying electricity from a generator by output. 78. A helical water-cooled outer wall unit assembling structure, comprising a combustor / heat exchanger shortened into a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. To provide electricity from the generator by the output of the superheated steam obtained by exchanging heat so that the temperature of the combustion gas is below the turbine heat resistant temperature. A combined steam and gas turbine engine having a device. 79. The method according to claim 73, 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. 80. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multi-honeycomb, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine and a generator for obtaining output with combustion gas And all the turbine blades, condensers, and generators that produce output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and the electricity from the generator by the output of each of them. And a device for supplying steam. 81. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding structure unit assembling structure and the combustor / heat exchanger is shortened into a large number of small diameter honeycombs. A compressor, an all-blade gas turbine that obtains output with combustion gas, and a generator and an all-blade steam turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature; and A combined steam and gas turbine engine having a condenser, a generator, and a device for supplying electricity from the generator based on the output of each of the condenser and the generator. 82. As a spiral water-cooled outer wall unit assembling structure, a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. Rotor blade gas turbine and generator that obtains output with combustion gas, all rotor blade steam turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is below the turbine heat-resistant limit temperature, and condensate A combined steam and gas turbine engine comprising a steam generator, a generator, and a device for supplying electricity from the generator with the outputs of the respective generators. 83. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multi-honeycomb, a compressor for supplying compressed air to the combustor / heat exchanger, a gas turbine and a generator for obtaining output from combustion gas, and a combustion gas temperature turbine. It has a steam turbine, a condenser, and a generator for obtaining an output with superheated steam obtained by heat exchange so as to be below the heat-resistant limit temperature, and a device for supplying electricity from the generator with the output of each of them. Steam gas turbine combined engine. 84. A combustor / heat exchanger in which the water-cooled outer wall is formed as a spiral welded unit assembling structure, the combustor / heat exchanger being shortened into a small-diameter multi-honey structure, and a compressor supplying compressed air to the combustor / heat exchanger. A steam turbine, a condenser, and a generator, each of which obtains an output with 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, and a gas turbine and a generator that obtain an output with a combustion gas. And a device for supplying electricity from the generator with the output of the husband. 85. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger shortened into a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A turbine and a condenser, and a generator, and a steam turbine, a condenser, and a generator, each of which outputs heat with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than a turbine heat-resistant limit temperature. And a device for supplying electricity from a generator according to the invention. 86. The method according to claim 83, 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. 87. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger shortened into a small-diameter multiple-honeycomb shape, a full-blade compressor for supplying compressed air to the combustor / heat exchanger, a full-blade gas turbine that obtains output with combustion gas, and a combustion gas A combined steam and gas turbine engine comprising: a full-blade steam turbine that obtains output with superheated steam obtained by heat exchange so that the temperature is equal to or lower than a turbine heat-resistant limit temperature. 88. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding unit assembly structure having a small diameter and a plurality of honeycombs, and a whole blade for supplying compressed air to the combustor / heat exchanger. A steam having a 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 allowable temperature limit. Gas turbine combined engine. 89. As a spiral water-cooled outer wall unit assembling structure, a combustor / heat exchanger shortened into a large number of small diameter honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. Combined steam gas turbine having a full-blade gas turbine that obtains output with combustion gas and a full-blade steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature organ. 90. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger that has been shortened into a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, a gas turbine that obtains output with combustion gas, and the combustion gas temperature is the turbine heat-resistant limit temperature. A combined steam gas turbine engine having a steam turbine that obtains output with superheated steam obtained by heat exchange as follows. 91. A combustor / heat exchanger in which a water-cooled outer wall is formed into a spiral welding unit unit assembling structure having a small diameter and a plurality of honeycombs, and a compressor for supplying compressed air to the combustor / heat exchanger. A combined steam and gas turbine engine comprising: a gas turbine that obtains output with combustion 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. 92. A helical water-cooled outer wall unit assembling structure, a combustor / heat exchanger shortened into a large number of small-diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A combined steam and gas turbine engine comprising: a gas turbine that obtains an output with a steam turbine; 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 a turbine heat-resistant limit temperature. 93. The method according to claim 90, 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. 94. The steam gas turbine combined engine according to claim 1, wherein the steam turbine uses superheated steam having a supercritical steam condition or less. 95. 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. 96. 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. 97. A combined steam gas turbine engine, wherein the magnetic friction power transmission device (14) has a cooling device. 98. A combined steam gas turbine engine, wherein a bypass is provided in a full blade compressor that supplies the compressed air to a combustor / heat exchanger. 99. A combined steam gas turbine engine, wherein a bypass is provided in a compressor for supplying the compressed air to a combustor / heat exchanger. 100. 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. 101. 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 compressor in double. 102. The all-blade steam turbine compressor,
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. 103. 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: 104. 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. 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 stator vane outside of the steam turbine. 105. In the steam turbine compressor, an inner turbine blade group (20) is provided on an inner shaft device, and a stationary blade is provided on 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. 106. The full-blade steam turbine comprises an inner shaft device provided with an inner turbine blade group (20), and an outer shaft device provided with an outer turbine blade group (19). 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. 107. 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.