JPH11107778A - Steam gas turbine combined engine, transportation and generating equipment - Google Patents

Abstract

PROBLEM TO BE SOLVED: To generate great output by converting most of a supplied heat quantity into super heated steam so as to use it for the purpose including a steam turbine and sucking and injecting air/water by means of steam provided by heat exchange or the superheated steam so that a combustion gas temperature becomes a turbine heat resistant limit temperature or less. SOLUTION: A combustor-heat exchanger 4 is constructed by forming a water cooling outside wall 26 of a spiral water cooling wall pipe unit 52, which includes a plurality of conduits 1, and arranging a steam pipe 6 spirally substantially inside the water cooling outside wall 26. Intake air is compressed by means of operation of groups of internal and external compressor moving blades 17, 16 and fed to the combustor-heat exchanger 4 so as to be stirred and mixed with fuel fed from a fuel feeding means 27, so that high pressure high temperature combustion gas is generated. When combustion gas 10 generated in this process is led into groups of external and internal turbine moving blades 19, 20, power is generated to drive a generator-motor. Water inside the conduits 1 is evaporated by means of the heat exchanger 4 so as to be turned into super heated steam, which is jetted to a gas turbine from a group of jetting port group 24.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combined steam and gas turbine engine, and more particularly, to an outer wall of a plurality of combustors of a gas turbine, a substantially spiral welded water-cooled outer wall heat exchanger or a spiral water-cooled wall pipe. By using a unit-assembly heat exchanger, it is possible to greatly increase the pressure, and to extend the length of the combustor / heat exchanger according to the application, for example, by providing a generator / motor in the middle to increase the fuel supply. The means can be expanded more than three times,
A steam superheater is provided in the combustor / heat exchanger in a substantially spiral shape to obtain an output from the superheated steam and the combustion gas (hereinafter referred to as a steam gas turbine); The present invention relates to a new technology of various types of steam gas turbine combined engine transport power generation equipment including a magnetic friction power transmission device, which can be used for various applications such as heat and electricity co-supply equipment, including various jet pumps for obtaining the above.

[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
181944 and Japanese Patent Application No. 9-212373. The priority claim application based on the earlier application is schematically
Increasing the length of all combustors, including all rotor blades, and / or the gas turbine, and using the water-cooled outer wall in a spiral shape to serve as a heat exchanger that is also used as a high-pressure vessel, and superheat most of the supplied heat By making it possible to convert to steam, it is a device and method that can simultaneously raise the pressure ratio and specific output to the maximum without exceeding the turbine heat resistance limit temperature.

[0004]

The important things as the performance of the gas turbine cycle such as the Preyton cycle are thermal efficiency and specific output. The higher the pressure ratio, the higher the thermal efficiency is obtained, and the thermal efficiency (pressure ratio) is constant. In, a larger specific output is obtained as the amount of heat supplied to the cycle increases. 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 supply heat quantity (fuel combustion mass) to the maximum without exceeding the heat-resistant limit temperature of the turbine is to convert most of the supply heat quantity (fuel heat generation quantity) into superheated steam, The thermal efficiency x specific output = pressure ratio x combustion gas mass (velocity x mass) is greatly increased,
It is an object of the present invention to use it for transporting people or luggage by sucking and injecting air or water with steam or superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than a turbine heat-resistant limit temperature.

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. The fuel calorific value is converted into superheated steam or steam.
Since there are infinite numbers including various steam gas turbines, various jet pumps, and various steam turbines, the gas turbine combustor is also used as a heat exchanger with a large and large heat transfer area by increasing the length and pressure of the fuel. To provide an engine that can increase the pressure ratio and the specific output to the maximum without exceeding the heat-resistant limit temperature of the turbine by converting large to superheated steam and using it for other applications. By increasing the air-fuel ratio to about four times that of a general engine,
A device that increases the heat efficiency and specific output of the gas turbine by reducing the amount of heat used by the gas turbine out of the supplied heat by increasing the pressure ratio and the fuel combustion mass is provided. Use to drive a steam gas turbine with superheated steam obtained by heat exchange as follows, and to suction and inject air or water with the superheated steam, such as driving various vehicles, driving various aircraft, or various ships It is intended to drive or to be used for combined heat and electricity facilities.

[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. As a result, the air compressed by heat exchange can be used almost 100% effectively for combustion, and the pressure ratio and the fuel combustion mass greatly increase due to heat exchange and temperature decrease, thereby increasing the amount of heat used by the gas turbine among the supplied heat. It is obtained by increasing the thermal efficiency of the gas turbine by a factor of 2 to 3 and greatly increasing the specific output, or by exchanging heat so that the temperature of the combustion gas and the combustion gas is lower than the heat-resistant limit temperature of the turbine. Overheating Drives the steam gas turbine by a gas, the use of superheated steam containing a large elevated supercritical steam conditions the pressure ratio 10 times before and after the air compressor, the heat efficiency 3
An object of the present invention is to greatly increase the specific output as well as about twice as much as possible, or to use it for the purpose of injecting superheated steam to efficiently suction and inject air or water.

If the gas turbine combustor is also used as a heat exchanger having a large heat transfer area by increasing its length and pressure, the greater the pressure ratio, the higher the thermal efficiency of the gas turbine. The higher the ratio, the higher the temperature is obtained, and the gas temperature at the turbine inlet is 700 C
Heat exchange becomes easier as the temperature increases to about 1000 C or higher. For this reason, NOx reduction combustion by reducing the heat transfer area of the heat exchanger and cooling is possible, and it is possible to greatly reduce exhaust loss by increasing the pressure ratio and lowering the heat exchange exhaust heat temperature, thereby reducing the amount of heat generated. It provides an ultra-high performance / ultra-high heat efficiency gas turbine or steam gas turbine combined engine that can be effectively used to the extremes, and uses superheated steam obtained by heat exchange so that the combustion gas temperature becomes lower than the turbine heat-resistant limit temperature. Or, while providing various jet pumps that suction and jet water most efficiently,
An object of the present invention is to minimize the power transmission loss by making the most of a magnetic friction power transmission device.

[0008]

The combustion gas as the working gas of the gas turbine generally has a very high air ratio,
The air contains about 4 times the theoretical mixing ratio. That is, since about 80% of the compressed air which consumes a large amount of heat energy is wasted, and is used to reduce the combustion temperature, which results in a large loss. In order to effectively use 100% for combustion, the length of the combustor / heat exchanger is increased by providing a generator / motor at approximately the center of the gas turbine, so that the fuel supply means can be increased about four times. At the same time, the heat transfer area is greatly increased as a combustor / heat exchanger, and the outer wall is formed as a spirally welded water-cooled outer wall including a water pipe or a water-cooled wall pipe unit 52 including a spirally welded structure. Increase the pressure and set a relatively large pressure ratio. In addition, in the superheating process, a steam pipe is provided in a substantially spiral shape in the combustor / heat exchanger to serve also as a significantly high-pressure ultra-high-performance heat exchanger. The temperature is reduced below the turbine heat-resistance limit temperature, the compressed whole compressed air approaches the stoichiometric air-fuel ratio combustion, and the fuel combustion mass can be increased up to about four times. The steam gas turbine is driven by superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are lower than the turbine allowable temperature limit by reducing the pressure ratio by nearly 10 times the compression, and the air is heated by the superheated steam. We provide a variety of jet pumps, such as jet engines and marine floating water jet propulsion devices, which suction and jet gas or liquid such as water with a jet pump most efficiently.

Further, when comparing the case where air is compressed and the case where water is compressed, it is much more advantageous to compress water in which water vapor is condensed to approximately 1/700, In addition to being able to increase the amount of heat (the amount of retained heat energy), if it is released as superheated steam with a pressure ratio close to 10 times that of air compression, a large volume far exceeding 1700 times can be obtained, so that almost all compressed air is burned. The best way to effectively utilize is to convert and use superheated steam most efficiently, including substantially all of the increased supply fuel. 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 pressure as high as possible to achieve the most efficient heat exchange and NOx reduction combustion by cooling, and achieve the same heating value. The amount of heat (superheated steam) extracted from the fuel is maximized to obtain the most efficient superheated steam, and the mass of the combustion gas that drives the gas turbine or steam gas turbine is maximized to minimize the amount of heat, and the most efficient gas turbine or steam is obtained. In addition to driving the gas turbine, the exhaust heat is injected as a very low temperature low amount of exhaust heat to significantly reduce the exhaust loss as the low temperature exhaust. A gas turbine cycle that includes all rotor blades as a drive that transmits power most efficiently, including all auxiliary equipment, by fully using the equipment The highest thermal efficiency will strive to large increases to twice or three times before and after.

[0010]

DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiments and embodiments of the present invention will be described with reference to the drawings. The overlapping description will be omitted, and the characteristic portions and the lack of description 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. The combustor / heat exchanger 4 used in the present invention has a water-cooled outer wall 26 and a plurality of water pipes 1 as shown in FIGS. As a spiral welding structure or water cooling wall tube unit 52 assembling structure, the pressure is increased, a relatively large pressure ratio is set, the steam pipe 6 is provided in a substantially spiral shape, and a generator / motor is provided substantially in the middle of the center. In addition to using both as a heat and electricity co-supply facility and a starter, a long combustor / heat exchanger 4 with a large heat transfer area and additional fuel supply means 27 is used.

An embodiment of a combined rotor / steam gas turbine engine will be described with reference to FIGS. 1, 2, 5, 6 and 9. The idea of the combined rotor and blade is that the vehicle is pushed by hand and moved. If you do, you will be very tired if you push with the brake applied, but the workload is 0, and you can easily move by releasing the brake and pushing. Therefore, if there is a stationary blade in a compressor or a turbine, a large loss of energy will result in a large loss of energy. Therefore, the stationary blade is replaced with a moving blade as a whole moving blade. The inner shaft device and the outer shaft device, which rotate in opposite directions, are connected to each other by a magnetic friction power transmission device, so that the two shafts are most efficiently driven in double reversal and the peripheral speed is shared by approximately half. Then, the outer diameter is approximately doubled and the fluid passage is approximately quadrupled to increase the specific output greatly and to greatly increase the thermal efficiency, or to substantially double the relative speed between the moving blades at substantially the same peripheral speed. In order to greatly increase the specific output and the thermal efficiency, or to reduce the peripheral speed by about half, the allowable stress is about 1/4, and it is inexpensive and quiet, and various designs (such as household heat and electricity supply equipment) And greatly increase thermal efficiency.

Another explanation will be given with reference to FIG. 1. In other words, air is normally sucked in from the right-stage replaced outer compressor blade group 1 stage 16 and the even-numbered inner compressor blade group 17 and the odd-numbered stage. The outer compressor rotor blade group 16 cooperates to efficiently compress the air by all the rotor blades and supplies the compressed air to the combustor / heat exchanger 4.
Agitated and mixed with the fuel containing approximately double the amount, and heat exchanged so that the combustion gas temperature including the stoichiometric air-fuel ratio combustion was lower than the turbine heat resistance limit temperature. To generate rotating power, most of the heat energy is converted into superheated steam, and is transmitted through a steam pipe 6 and a steam control valve 7 to the upstream annular portion of the entire moving blade / steam gas turbine. Injection is performed downstream from the nozzle group 24 to generate a large output.
A jet pump 28a that directly reheats by joining with the combustion gas containing the gas from 0 (mist spraying principle) and drives and exhausts all blades / steam gas turbine without exceeding the heat-resistant limit temperature of the turbine; And / or the superheated steam is injected directly downstream from the jet pump 28b via the steam control valve 7, and the jet and the jet from the jet pump 28a cause the front air to be centered and to the rear left from the inner circumference of the outer cylinder 29. It is used for various aircrafts and the like that require strong injection to obtain a pressurized gas and / or require propulsion.
Propelling efficiency is greatly increased by nearly double superheated steam.

Referring to FIG. 1, a further explanation will be given. A generator / motor is provided substantially near the center to constitute a generator / motor so that the length of the combustor / heat exchanger is increased. The inner shaft device is fixed to the left and right sides of the rotor, and the outer compressor rotor blade group final stage 16 and the outer turbine rotor blade group one stage 1 provided in an annular shape are provided.
The outer shaft device to which the fixing shaft 9 is fixed is rotatably fitted to the outer shaft device, and the two shafts rotating in the opposite directions are respectively coupled by the magnetic friction power transmission device 14 at an optimum rotation ratio, and are connected to the inner shaft device. The final stage 17 of the inner compressor blade group and the second stage 20 of the inner turbine blade group are fixed, and thereafter, the odd-numbered outer compressor blade group 16 and the even-numbered inner compressor blade group 17 are alternately fixed. A drive unit for transmitting power constitutes a full-blade compressor, and an odd-numbered outer turbine blade group 19 is fixed to the outer turbine blade group 1 stage 19, and a two-stage inner turbine blade group 2
0, the even-numbered inner turbine blade groups 20 are alternately fixed to each other.
Is fixed to the inner shaft device, and the odd-numbered final stage outer turbine blade group 19 is fixed to the outer shaft device, and is rotatably fitted to the inner shaft device.

The high-compressed air supplied from the annular outlet 21 to the annular receiving port 22 is stirred and mixed with fuel supplied from the fuel supply means 27 including a plurality of portions, and is appropriately burned. The combustion is performed while controlling the temperature and the superheated steam temperature in the plurality of combustors and heat exchangers 4, and the combustion gas is cooled by the water cooling wall pipe 26 and the steam pipe 6 of the water guide pipe 1, thereby reducing the NOx combustion. And the fuel supply means 27 can be added without causing the combustion gas temperature to exceed the heat-resistant limit temperature of the turbine, and the fuel supply amount can be increased up to about four times the normal air-fuel ratio by heat exchange to the stoichiometric air-fuel ratio. Means 27 can be added to convert the majority of the supplied heat into superheated steam 5 and supply it to the annular receiving port 23 through the respective steam control valve 7, and the superheated steam 5 collected in this portion is Group of spouts 4 than 1 stage outer turbine Dotsubasagun 19
And the downstream side is sequentially driven to merge with the combustion gas 10 as usual, but the combustion gas is supplied to the combustor / heat exchanger 4.
According to the combustion gas pressure, it is supplied to the optimal stage of the all-blade steam gas turbine in accordance with the combustion gas pressure. Thereafter, the superheated steam is directly reheated by the combustion gas 10 while the superheated steam and the combustion gas jointly drive the all-blade steam gas turbine. And the final stage outer turbine blade group 1
9 to form a jet pump 28a, which sucks and injects air in the center side and the outer cylinder 29 to the rear left, and separate mobilization of the superheated steam 5 through a plurality of steam control valves 7 respectively. From the jet pump 28b of the outer cylinder 29
The inner air is suctioned and jetted to the rear left, and the jet pumps 28a and 2
8b, including the air in the right front, is strongly jetted to the rear left.
All blades and steam gas turbine combined engine.

Referring to FIG. 2, another description of the second embodiment of the all-blade steam-injected gas turbine combined engine is as follows. In the prior art, 80% of the compressed air consumes a large amount of heat energy.
Since the waste is discharged wastefully (by lowering the combustion temperature) without using a nearby area, a large loss is caused. By making the compressed air available for combustion 100% effectively, the specific output is increased to the limit and the thermal efficiency is increased. It is intended to make a great rise. That is, since the combustion gas as the working gas of the 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 without exceeding the heat-resistant limit temperature of the turbine is 100%. In order to use it for combustion, it is necessary to convert most of the supplied heat into superheated steam. Therefore, the present invention provides a generator / motor in the vicinity of the center to increase and lengthen the heat transfer area of the plurality of combustors / heat exchangers 4 so that most of the supplied heat can be converted to superheated steam. The water-cooled outer wall has a spiral welding structure including at least one water-cooled wall tube 26 or an assembled structure of the spiral water-cooled wall tube unit 52 to enable a large increase in the pressure ratio.
The specific output is greatly increased, and waste is completely eliminated to achieve a significant increase in thermal efficiency.

Another explanation will be given with reference to FIG. 2. In other words, air is normally sucked from the first stage 16 of the replaced outer compressor blade group at the right end, and the inner compressor group 17 of the even-numbered stage and the odd-numbered stage. The outer compressor blade group 16 cooperates to efficiently compress air by all the blades and supply the compressed air to the plurality of combustor / heat exchangers 4,
The agitated mixed combustion with the supplied fuel including about four times the normal amount supplied from the fuel supply means 27 including a plurality of the respective parts can be performed, and the combustion gas temperature including the substantially stoichiometric air-fuel ratio combustion becomes the turbine heat resistant limit temperature. The combustion gas obtained by heat exchange as described below is rotatably inserted into the annular receiving port 23 of the all-blade blade gas turbine, and is provided from the hermetically sealed annular injection port group 24.
Injection is performed on the downstream side including the replaced outer rotor blade group 1 stage 19 to obtain rotational power, and combustion gas is injected to the rear left to form a jet pump 28a to form air in the center side and the outer cylinder 29. To the left rear, the superheated steam obtained by heat exchange is directly injected to the left rear from the jet pump 28b through the steam control valve 7, and the air in the outer cylinder 29 is sucked and injected to the left rear,
It is an all-blade steam gas turbine combined engine that injects the air in the front right strongly to the rear left.

Referring to FIG. 2, another description will be given. A generator / motor for increasing the length of the combustor / heat exchanger is provided substantially in the vicinity of the center. In connection with the left and right inner shaft devices, an outer compressor rotor blade group final stage 16 and an outer turbine rotor blade group first stage 19 provided annularly are provided.
The outer shaft device to which the shaft is fixed is rotatably fitted on the outer shaft, and the two shafts rotating in the opposite directions are coupled to each other at the optimum rotation ratio by the magnetic friction power transmission device 14 to be connected to the inner shaft device. Inner compressor blade group final stage 17 and inner turbine blade group 2
The stage 20 is fixed, and then the odd-numbered outer compressor blade groups 16 and the even-numbered inner compressor blade groups 17 are alternately fixed.
An all-stage moving blade compressor for driving the shaft is constituted, an odd-numbered outer turbine moving blade group 19 is fixed to the outer turbine moving blade group first stage 19, and an even-numbered inner turbine moving blade group is fixed to the second-stage inner turbine moving blade group 20. The even-numbered last stage turbine blade group 20 is fixed to the inner shaft device by alternately fixing the group 20, and the odd-numbered last stage outer turbine blade group 19 is fixed to the outer shaft device so as to fix the inner shaft. Externally pivoted to the device so that it can rotate freely.

The highly compressed air supplied from the annular outlet 21 to the annular receiving port 22 is mixed with the fuel supplied from the fuel supply means 27 including a plurality of the respective portions, and is appropriately burned. Combustion while controlling the gas temperature and the superheated steam temperature in the plurality of combustors / heat exchangers 4 and the reduction of the NOx by cooling the combustion gas by the water cooling wall pipe 26 and the steam pipe 6 of the water pipe 1 respectively. Combustion is enabled, the fuel supply means 27 can be added without the combustion gas temperature exceeding the heat-resistant limit temperature of the turbine, and the fuel supply amount can be increased to approximately four times the stoichiometric air-fuel ratio by heat exchange. The fuel supply means 27 can be added, and the superheated steam obtained by heat exchange without exceeding the heat-resistant limit temperature of the turbine is jetted from the jet pump 28b through the steam control valve 7 and the surroundings. The air inside the outer cylinder 29 is suction-injected to the left rear, and all the blades / gas turbines are driven by the combustion gas obtained by heat exchange without exceeding the heat resistant limit temperature of the turbine, and the combustion gas is injected to the left rear. And jet pump 2
8a, the air in the outer cylinder 29 on the center side and the outer cylinder is suction-injected to the rear left, and the combustion gas and superheated steam inject the air in the front right to the rear left to move the whole blade steam gas. Used as a combined engine of turbines, for example, as a jet engine.

Referring to FIG. 3, a third embodiment of the combined steam / gas turbine engine will be described. The difference from the first embodiment of FIG. As an engine, a replacement rotor blade is reduced to a conventional stator blade so that a compressor or a steam gas turbine closer to the related art can be driven, and the jet pumps 28a and 28b are substantially similar to the jet pumps 28a and 28b. is. Therefore, the elements of the first to third embodiments shown in FIG. 1 can be appropriately replaced with each other and used, for example, for propulsion of a ship or an aircraft.

Referring to FIG. 4, a fourth embodiment of the steam gas turbine combined engine will be described. The difference from the second embodiment of FIG. As the engine, the displacement rotor blades are reduced to conventional stator vanes to enable driving of a compressor or gas turbine approaching the prior art, and the infinitely large number of jet pump type jet pumps 28a and 28b are substantially similar to jet pumps. 28a ・ 28b
It was a thing. Therefore, the elements from the first embodiment to the fourth embodiment in FIG. 1 can be appropriately replaced, and used for propulsion of a ship or an aircraft, for example.

Referring to FIG. 5, a fifth embodiment of the combined rotor / steam gas turbine engine will be described. The difference between the first embodiment and the first embodiment shown in FIG. In the fifth embodiment, a thrust force or a pressure gas is obtained by strongly sucking and moving air or the like to obtain a propulsion force or a pressure gas. This is a device that obtains propulsive force or high-pressure liquid by strongly sucking and moving liquid water. That is, the difference is that all the blades / steam gas turbines are driven by the combustion gas and 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, and the jet pump 28a is exhausted or the like. The air in the central side and the outer cylinder 29 is strongly suctioned and injected to obtain a propulsive force or a pressurized gas.
It is used for the purpose of injecting water from the above jet pump 28c and strongly sucking and moving water to the left rear, for example, to levitate a ship by air pressure and propell the ship by water injection.
Therefore, the elements from the first embodiment to the fifth embodiment can be appropriately replaced and used for various purposes.

Referring to FIG. 6, a sixth embodiment of the combined rotor / steam gas turbine engine will be described. The second embodiment is almost the same as the second embodiment of FIG. In the sixth embodiment, the thrust or pressure gas is obtained by strongly sucking and moving air or the like, while the device for obtaining thrust or pressure gas is obtained by strongly suctioning and moving gas. It is a device that mainly obtains propulsion or pressure liquid by powerful suction and injection of water. That is, the difference is that, of the combustion gas and 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, all combustion blades and gas turbines are driven by the combustion gas and jetted by the exhaust gas or the like. A pump 28a is formed, and the air in the center side and the outer cylinder 29 is sucked and ejected to the left rear to obtain a propulsive force or a pressurized gas, and the superheated steam obtained by the heat exchange is supplied to the steam control valve 7. And at least one or more jet pumps 28c appropriately extended through the nozzles to inject the liquid to the left rear, suck the liquid such as water in the right front to the rear left, and float the ship by air pressure, for example. Used for propulsion of the ship by injection.
Therefore, the elements from the first embodiment to the sixth embodiment can be appropriately replaced and used for various purposes.

Referring to FIG. 7, a seventh embodiment of the combined steam and gas turbine engine will be described. The difference between the seventh embodiment and the third embodiment shown in FIG. 3 is that the third embodiment mainly uses a strong gas such as air. In the seventh embodiment, air or the like is suctioned and moved to obtain a propulsion force or a pressure gas, and water or the like is strongly suctioned. It is a device that obtains propulsion or pressure liquid by spraying. That is, the difference is that, of the combustion gas and the superheated steam obtained by performing heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat resistance limit temperature, a portion of the combustion gas and the superheated steam are passed through the steam control valve 7 through the steam control valve 7. The turbine is driven to form a jet pump 28a by the exhaust gas or the like, and the air in the center side and the outer cylinder 29 is suction-injected to the rear left to obtain a propulsive force or a pressurized gas, and the remainder of the superheated steam Is jetted to the left rear from at least one or more jet pumps 28c appropriately extended through the steam control valve 7 of each husband, and the liquid such as water on the right front is strongly suction-jetted to the left rear, For example, it is used for the purpose of levitating a ship by air pressure and propelling the ship by water injection. Therefore, the elements of the first to seventh embodiments can be appropriately replaced and used for various purposes.

Referring to FIG. 8, the eighth embodiment of the combined steam / gas turbine engine will be described. The difference between the fourth embodiment and the fourth embodiment shown in FIG. 4 is that the fourth embodiment suctions and injects gas such as air. In the eighth embodiment, air or the like is suctioned and moved to obtain a propulsion or pressure gas, and water or the like is strongly suctioned and injected in the eighth embodiment. It is a device that obtains propulsion or pressure liquid. That is, the difference is that, of the combustion gas and superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature,
The gas turbine is driven by the combustion gas and the exhaust gas or the like constitutes a jet pump 28a, and the air in the center side and the outer cylinder 29 is sucked and jetted to the left rear to obtain a propulsive force or a pressurized gas. By driving at least one or more jet pumps 28c appropriately extended by the steam through the respective steam control valves 7, the superheated steam is directly jetted to the left rear and the liquid such as water in the right front is jetted to the left rear. It is used for propulsion of the ship by water injection, for example, by levitation of the ship by air pressure. Therefore, the elements from the first embodiment to the eighth embodiment can be appropriately replaced and used for various purposes.

Referring to FIG. 9, a ninth embodiment of the combined steam and gas turbine engine will be described. The jet pump 28 and the outer cylinder 29 are omitted from the first embodiment of FIG.
While the first embodiment is a device that mainly obtains a thrust or a pressure gas by strongly sucking and moving a gas such as air, the ninth embodiment is a device that mainly obtains rotational power.
Alternatively, as shown in FIG. 16, by equipping a well-known exhaust heat recovery heat heat exchanger 11, it can also be used for household ultra-small as a combined heat and electricity supply facility. In other words, the difference is that all the moving blades / steam gas turbines are driven by all the superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are below the turbine heat-resistant limit temperature.

Referring to FIG. 10, a description will be given of a tenth embodiment of a combined steam and gas turbine engine. In the tenth embodiment, a jet pump 28 and an outer cylinder 29 are omitted from the third embodiment of FIG. In the tenth embodiment, a device for mainly obtaining rotational power is provided as a device for obtaining a propulsive force or a pressurized gas by strongly sucking and moving a gas such as air. Heat recovery heat exchanger 1
By equipping with 1, it will be a combined heat and electricity facility. That is, the difference is that the steam gas turbine is driven by all the superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature become lower than the turbine heat resistance limit temperature.

The welding structure of the means for increasing the pressure and length of the combustor / heat exchanger 4 will be described with reference to FIG.
(B) As shown in (c) and (d), a water-cooled outer wall including at least one or more spiral water pipes 1 has a spiral welding structure to enable a large pressure ratio and increase the length. Make it easy. That is, as in the embodiment shown in (a) and (b),
A combustor outer box part 25 is provided slightly outward in the radial direction of the water guide pipe 1 provided in a spiral shape, and one or more water guide pipes 1 are welded in a spiral shape such as a T-shape in the axial direction to greatly reduce the size. It enables a high-pressure vessel combustor and a large heat transfer area for the combustor / heat exchanger 4. Further, as in the embodiment shown in (c), the combustor outer casing 25 is disposed radially outward of the water guide pipe 1 provided spirally.
Is installed, and one or more water pipes 1 are welded in a spiral shape in the axial direction, enabling a large increase in the heat transfer area of the combustor / heat exchanger 4 with a significantly higher pressure under supercritical steam conditions. Further, as in the embodiment shown in (d), a combustor outer box 25 is provided substantially at the center in the radial direction of the spirally provided water pipe 1, and one or more water guide pipes 1 are welded in an axially spiral manner. As a result, it is possible to increase the heat transfer area of the combustor / heat exchanger 4 having a pressure ratio lower than the supercritical steam condition and a relatively high pressure ratio.

Referring to FIG. 12, the water cooling wall tube unit 52 of the means for increasing the pressure and lengthening the combustor / heat exchanger 4 will be described.
(A) As shown in (b) and (c), a water cooling wall pipe unit 52 including at least one or more spiral water pipes 1 is provided with flanges 5 at both ends.
As a unit that can be assembled by providing 3 units, a plurality of water cooling wall tube units 52 are connected to form the main part of the combustor / heat exchanger 4 that can be significantly increased in pressure and lengthened. That is, as in the embodiment shown in (a) and (b), the combustor outer box part 25 is slightly apart from the spirally provided at least one or more water guide pipes 1 in the radial direction.
The water cooling wall tube unit 52 including the water guide tube 1 is provided with the flange 53 provided at both ends thereof, and the water guide tube 1 is respectively opened at the flange 53.
To be concatenated. Also, as in the embodiment shown in FIG.
A combustor outer box part 25 is provided radially outward of at least one or more water guide pipes 1 provided in a spiral shape, and flanges 53 are provided at both ends thereof. The water cooling wall pipe unit 52 including the water pipe 1 can be connected so as to be openable, and the heat transfer area of the combustor / heat exchanger 4 having a supercritical steam condition or less and a relatively high pressure ratio can be increased. To

The magnetic friction power transmission device will be described with reference to FIGS. 13 and 14. Various power transmission devices including normal speed change and reverse rotation mainly use a gear device. For this reason, since a sliding tooth surface that includes a large load is essential for the tooth surface, in addition to the need for lubricating oil, the friction heat loss is also very large, so it can not be used for high power transmission equipment including high speed rotation There is a problem. 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. Requires a power transmission device by rolling contact with the sliding tooth surface of the gear device being almost zero. For this reason, the meshing height of the gears is reduced as much as possible to provide low irregularities 40, and a bar magnet 33 or an electromagnet 34 is provided on the upstream and downstream sides in the rotation direction 35,
Various magnetized friction wheels 3 utilizing the strong attraction of the magnet
It is preferable to use the device as a whole as various magnetic friction power transmission devices including various combinations with the 7.37 and various magnetically-attached friction wheels 39,39. In other words, by bringing rolling contact closer, the frictional heat loss can be reduced to almost zero, and harmless water cooling can be achieved in place of ultra-high-speed large power transmission and lubricating oil.

The magnetic friction power transmission device will be described with reference to FIGS. 14 and 15. Power transmission is performed by using various magnetized friction wheels 37, 37 and various magnetic friction wheels 39, 39 instead of various gears. On the surface 31, low unevenness 40 is used, for example, a flat unevenness 41 wheel instead of a spur gear, and a helical unevenness 42 instead of a helical gear.
The car is replaced with a Yamaba gear, and 43 Yamaba irregularities are provided.
As a result, various magnetic friction power transmission devices are configured and used as the magnetic friction power transmission device 14 in the same manner as the known various gear type power transmission devices. As the special magnetic friction power transmission device 14, there is a combination of a rail 54, a wheel 55, a bar magnet 33 or an electromagnet 34 as in the embodiment of FIG. In this embodiment, the material of the wheel 55 does not matter as long as the rail 54 is a substance that is attracted to the magnet. Therefore, the magnetic friction power transmission device 1 in which the magnet is only the bar magnet 33 or the electromagnet 34 is used.
By constructing No.4, practical use of railway transportation equipment that travels at very high speed on railways including steep hills by using the strong attraction of magnets.

The eleventh embodiment of the combined steam / gas turbine engine will be described with reference to FIG. 16. If the combined combined gas / gas turbine engine for obtaining rotational power is used, the means for increasing the length of the combustor / heat exchanger 4 is as follows. One or both of the steam gas turbine and the compressor are reversed, and the length of the combustor / heat exchanger 4 is increased. That is, air is sucked and compressed as usual from the leftmost inverted compressor, and high-pressure compressed air is supplied to the combustor / heat exchanger 4. 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 by stirring and mixing combustion so as to be combustible is transferred downstream from the most upstream side of the steam gas turbine through the steam control valve 7. The power is injected to generate power, and the combustion gas obtained by the heat exchange is supplied to the optimum intermediate stage of the steam gas turbine to increase the power, and is directly reheated by contact with the superheated steam to recover the exhaust heat. Exhaust after cooling heat exchange in heat exchanger 11. The hot-water supply water and the feed water 3 obtained by the heat exchange are appropriately used. However, since the exhaust gas itself is a low temperature close to 100 ° C., the refuse-burning furnace 12 and the refuse-burning furnace heat exchanger 13 are provided and the temperature of the feed water 3 To be supplied to the combustor / heat exchanger 4 by the feedwater pump 2.

Referring to FIG. 17, a first embodiment of a combined steam gas turbine engine will be described. A combined steam gas turbine engine used for various aircrafts for obtaining a propulsion force by strongly sucking and injecting air. Also, since it is necessary to inject superheated steam and combustion gas to obtain a propulsion force, the main part of FIGS. 1 to 4 is a full-blade steam gas turbine, a full-blade gas turbine, a steam gas turbine, or a gas turbine. Uses a steam gas turbine coalescence engine. The power transmission device
We will gradually switch from using normal power transmissions, including accessories, to developing and using magnetic friction power transmissions.

A second embodiment of the combined steam and gas turbine engine will be described with reference to FIG. 18. A steam used for various types of ships that obtains propulsion by floating and inflating a hull by strongly sucking and injecting air and water. In the combined gas turbine engine, it is necessary to inject superheated steam and combustion gas to obtain the propulsion force while floating the hull, so that the main parts in FIG. 5 to FIG. Use a steam gas turbine combined engine, which is a wing gas turbine or a steam gas turbine or a gas turbine. The power transmission system will gradually switch from using normal power transmission systems, including accessories, to developing and using magnetic friction power transmission systems.

Referring to FIG. 19, a third embodiment of the combined steam and gas turbine engine will be described. This is a combined combined steam and gas turbine engine for rotating various wheels to move various vehicles. Since it is necessary to obtain rotational power by injecting gas, use a steam gas turbine combined engine with the main part as a whole blade steam gas turbine or a steam gas turbine as shown in Fig. 9, Fig. 10, and Fig. 16. . The power transmission system will gradually switch from using normal power transmission systems including reversing and shifting including auxiliary equipment to developing and using magnetic friction power transmission systems.

Referring to FIG. 20, a fourth embodiment of the steam-gas-turbine combined engine will be described. The steam-gas-turbine combined engine used in various aircraft for obtaining propulsion or levitation by rotating various blades strongly. In both cases, it is necessary to inject superheated steam and combustion gas to obtain rotational power.
As shown in Fig.10 and Fig.16, a steam gas turbine combined engine with the main part being a whole blade steam gas turbine is used. The power transmission system will gradually switch from using normal power transmission systems including reversing and shifting including auxiliary equipment to developing and using magnetic friction power transmission systems.

Referring to FIG. 21, a fifth embodiment of the combined steam and gas turbine engine will be described. A combined steam and gas turbine combined engine used for various ships that obtains propulsion by strongly rotating various screw propellers. FIG. 9 also shows that it is necessary to obtain rotational power by injecting superheated steam and combustion gas.
-As shown in Fig. 10 and Fig. 16, use a steam gas turbine combined engine whose main part is a whole blade steam gas turbine or a steam gas turbine. The power transmission system will gradually switch from using normal power transmission systems including reversing and shifting including auxiliary equipment to developing and using magnetic friction power transmission systems.

A sixth embodiment of the combined steam and gas turbine engine will be described with reference to FIG. 22. A combined steam and gas turbine combined engine capable of driving heat and electricity, including microminiatures, by driving various generators. In any case, it is necessary to obtain rotational power by injecting superheated steam and combustion gas and use exhaust heat,
As shown in FIG. 9, FIG. 10 and FIG. 16, a main part is a full-blade steam gas turbine generator or a steam gas turbine combined engine having a steam gas turbine generator as shown in FIG. Using a vessel 11 or a garbage furnace 1
2 and the refuse incinerator heat exchanger 13 are used for the combined supply of heat and electricity. The power transmission system will gradually switch from using normal power transmission systems, including accessories, to developing and using magnetic friction power transmission systems.

[0038]

According to the present invention, an outer wall of a gas turbine combustor is provided as a combined steam and gas turbine engine including all rotor blades.
High pressure and length as a spiral welding structure including a water pipe or a spiral water cooling wall tube unit assembly structure, and as a combustor and heat exchanger for a high pressure vessel with a large heat transfer area, a large supply of heat. The part can be converted to superheated steam, and the combustion gas and superheated steam obtained by exchanging heat without exceeding the heat-resistant limit temperature of the turbine obtains rotational power and configures various jet pumps. In the case of the same as the conventional technology, the specific heat can be greatly increased by increasing the supplied heat amount up to the stoichiometric air-fuel ratio combustion with about four times the fuel of the conventional gas turbine, and the compressed air amount can be used for 100% combustion. And super-high-pressure steam with a pressure ratio close to 10 times the normal pressure ratio can be injected, so that various types of steam gas turbine combined engines, including various gas turbine and steam turbine combined cycles, are the most efficient. Such as obtaining the like of the jet pump, there is a large effect on the large increase in thermal efficiency. Also, by fully developing and using the magnetic friction power transmission device, it has the effect of significantly reducing frictional heat loss due to the power transmission device of the prior art and further increasing thermal efficiency. Therefore, it is very effective to reduce CO2 on a global scale by using it as various transportation equipment and cogeneration equipment for heat and electricity.

[Brief description of the drawings]

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

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

FIG. 3 is a partial cross-sectional view illustrating a third embodiment of the combined steam gas turbine engine.

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

FIG. 5 is a partial sectional view showing a fifth embodiment of the steam gas turbine combined engine.

FIG. 6 is a partial cross-sectional view showing a sixth embodiment of the combined steam gas turbine engine.

FIG. 7 is a partial cross-sectional view showing a seventh embodiment of the steam gas turbine combined engine.

FIG. 8 is a partial cross-sectional view showing an eighth embodiment of the combined steam gas turbine engine.

FIG. 9 is a partial cross-sectional view showing a ninth embodiment of the combined steam gas turbine engine.

FIG. 10 is a partial sectional view showing a tenth embodiment of the steam gas turbine combined engine.

FIG. 11 is a sectional view showing a spiral welding structure of a water-cooled outer wall of the combustor / heat exchanger.

FIG. 12 is a cross-sectional view for explaining a spiral water cooling wall tube unit of the combustor / heat exchanger.

FIG. 13 is a conceptual diagram of a magnetic friction power transmission device for a steam gas turbine combined engine.

FIG. 14 is a view for explaining friction increasing means such as a magnetic friction wheel and a magnetic friction wheel.

FIG. 15 is a view for explaining a special embodiment of the magnetic friction power transmission device.

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

FIG. 17 is an overall configuration diagram showing a first embodiment of the steam gas turbine combined engine.

FIG. 18 is an overall configuration diagram showing a second embodiment of the combined steam gas turbine engine.

FIG. 19 is an overall configuration diagram showing a third embodiment of the steam gas turbine combined engine.

FIG. 20 is an overall configuration diagram showing a fourth embodiment of the steam gas turbine combined engine.

FIG. 21 is an overall configuration diagram showing a fifth embodiment of the steam gas turbine combined engine.

FIG. 22 is an overall configuration diagram showing a sixth embodiment of the combined steam gas turbine engine.

[Explanation of symbols]

1: water guide pipe 2: feed water pump 3: feed water 4: combustor and heat exchanger 5: steam 6: steam pipe 7: steam control valve 10 combustion gas 11: waste heat recovery heat exchanger 12: garbage furnace 13: refuse Furnace heat exchanger 1
4: Magnetic friction power transmission device 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-cooled outer wall 27: Fuel supply means 28: Jet pump 29: Outer cylinder 30: Pressure reducing means 31: Power transmission surface 32: Yoke 33: Bar magnet 34: Electromagnet 35: Rotation direction
36: Magnetic pole 37: Magnetized friction wheel 38: Inner magnetized friction wheel 39: Magnetized friction wheel 40: Low unevenness 41: Flat unevenness 42: Husva unevenness 43: Yamaba unevenness 44: Inner magnetized friction wheel 45: Increased friction durability Means 46: Magnet part 47: Yoke (for magnetized friction wheel)
48: Insulating material 50: Engine body 51: Support shaft
52: Water cooling wall tube unit 53: Tsuba 54: Rail
55: Wheel

──────────────────────────────────────────────────続 き Continued on the front page (51) Int.Cl. ⁶ Identification code FI F01D 15/10 F01D 15/10 B F02C 3/30 F02C 3/30 Z 7/00 7/00 G 7/36 7/36 F23R 3/00 F23R 3/00 C

Claims (48)

[Claims] 1. A plurality of combustors and heat exchangers of which pressure and length are increased by using a spirally welded outer wall of a water-cooled outer wall, and a full blade compressor that supplies compressed air to the combustors and heat exchangers; An all-blade steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature, a jet pump (28a) including the exhaust gas,
A steam gas turbine combined engine transport having a jet pump (28b) including a superheated steam injection port for injecting the superheated steam and sucking and injecting air, and a device for levitating and moving the airframe by the thrust of the respective jet pumps. Power generation equipment. 2. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. An all-blade steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistant limit temperature, and a jet pump including the exhaust gas (28a)
And a jet pump (28b) including a superheated steam nozzle for injecting the superheated steam and sucking and injecting air, and a device for levitating and moving the airframe by the thrust of the respective jet pumps Engine transport power equipment. 3. A plurality of combustors and heat exchangers whose pressure and length are increased by using a water-cooled outer wall as a spiral welding structure, and an all-blade compressor that supplies compressed air to the combustors and heat exchangers. An all-blade gas turbine that obtains output with combustion gas, a jet pump (28a) containing the exhaust gas, and air by injecting 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 jet pump (28b) including a superheated steam jet port for sucking and injecting steam, and a device for levitating and moving the airframe by the thrust of the respective jet pumps. 4. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. And a jet blade pump (28a) containing the exhaust gas, which obtains an output from the combustion gas, and a superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature. A steam-gas-turbine combined engine transport power generation device having a jet pump (28b) including a superheated steam jet port for sucking and injecting air, and a device for levitating and moving the airframe by the thrust of the respective jet pumps. 5. A plurality of combustor / heat exchangers whose pressure and length are increased by using a spirally welded outer wall of a water-cooled outer wall, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, a jet pump (28a) including the exhaust gas, and air that is injected by injecting the superheated steam to generate air A steam-gas-turbine combined engine transport power generation device having a jet pump (28b) including a superheated steam jet port for suction injection, and a device for levitating and moving the airframe by the thrust of the respective jet pumps. 6. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, a compressor for supplying compressed air to the combustor / heat exchanger, and combustion gas And a steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, a jet pump (28a) including the exhaust gas, and air that injects the superheated steam and air And a jet pump (28b) including a superheated steam jet port for sucking and injecting steam, and a device for levitating and moving the airframe by the thrust of the respective jet pumps. 7. The steam and gas turbine combined engine transport power generation equipment according to claim 5, wherein one of the compressor and the steam gas turbine is a full blade. 8. A plurality of combustors and heat exchangers of which pressure and length are increased by using a spirally welded outer wall of a water-cooled outer wall, a compressor for supplying compressed air to the combustor and heat exchangers, and a combustion gas. A gas turbine for obtaining an output, and a jet pump (2
8a) and a jet pump (28b) including a superheated steam injection port for injecting superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat resistant limit temperature and sucking and injecting air.
And a device for levitating and moving the airframe by the thrust of the respective jet pumps. 9. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall unit assembly structure, a compressor for supplying compressed air to the combustor / heat exchanger, and combustion gas Gas turbine, a jet pump including the exhaust gas, a superheater that injects superheated steam obtained by heat exchange so that a combustion gas temperature is equal to or lower than a turbine heat resistant limit temperature, and suctions and injects air. Jet pump including steam nozzle (28
b) and a steam-gas-turbine combined-engine transport power generation device having a device for levitating and moving the airframe by the thrust of the respective jet pumps. 10. The steam and gas turbine combined engine transport power generation equipment according to claim 8, wherein either the compressor or the gas turbine is a full blade. 11. A plurality of combustors and heat exchangers whose pressure and length are increased by using a spirally welded outer wall of a water-cooled outer wall, and a full-blade compressor that supplies compressed air to the combustors and heat exchangers. A combustion blade and a full-blade steam gas turbine that obtains an output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resisting limit temperature, and a jet from a jet pump (28a) including the exhaust gas is sent to a ship bottom. Jet pump including a superheated steam nozzle for injecting the superheated steam and injecting water into the suction bottom of the ship (28)
and c) and a device for moving the ship by the force of the respective jet pumps. 12. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. An all-blade steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistant limit temperature, and a jet pump including the exhaust gas (28a)
A jet pump (28) including a superheated steam nozzle for injecting the superheated steam into the bottom of the ship,
and c) and a device for moving the ship by the force of the respective jet pumps. 13. A plurality of combustors and heat exchangers whose pressure and length are increased by using a spirally welded outer wall of a water-cooled outer wall, and an all-blade compressor that supplies compressed air to the combustors and heat exchangers. An all-blade gas turbine that obtains output with combustion gas, and a jet from a jet pump (28a) containing the exhaust gas are injected to the bottom of the ship, and heat exchange is performed so that the combustion gas temperature becomes equal to or lower than the turbine heat resistance limit temperature. A steam-gas-turbine combined-engine transport power generator having a jet pump (28c) including a superheated steam nozzle for injecting superheated steam and suctioning water to the bottom of the ship, and a device for moving the ship by the power of the respective jet pumps. machine. 14. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, and a full blade compressor for supplying compressed air to said combustor / heat exchanger. And an all-blade gas turbine that obtains an output from combustion gas, and a jet from a jet pump (28a) containing the exhaust gas is injected into the bottom of the ship, and heat exchange is performed so that the combustion gas temperature becomes equal to or lower than the turbine heat resistant limit temperature. Steam turbine having a jet pump (28c) including a superheated steam nozzle for injecting superheated steam and injecting water into a suction bottom of the ship, and a device for moving the ship by the power of the respective jet pumps Power generation equipment. 15. A plurality of combustors and heat exchangers of which pressure and length are increased by using a spirally welded outer wall of a water-cooled outer wall, a compressor for supplying compressed air to the combustor and heat exchangers, and a combustion gas. A steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, and a jet from a jet pump (28a) including the exhaust gas is injected to the bottom of the ship, A steam gas turbine combined engine transport power generator having a jet pump (28c) including a superheated steam nozzle for injecting steam and injecting water into a suction bottom of the ship, and a device for moving the ship by the power of the respective jet pumps. . 16. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, a compressor for supplying compressed air to the combustor / heat exchanger, and combustion gas And a steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, and a jet from a jet pump (28a) including the exhaust gas is jetted to the ship bottom. A steam-gas-turbine combined-engine transport power generator having a jet pump (28c) including a superheated steam nozzle for injecting superheated steam and suctioning water to the bottom of the ship, and a device for moving the ship by the power of the respective jet pumps. machine. 17. The steam-turbine combined engine transport power generation equipment according to claim 15, wherein one of the compressor and the steam gas turbine is a full blade. 18. A plurality of combustors / heat exchangers whose pressure and length are increased by using a spirally welded outer wall for water cooling, a compressor for supplying compressed air to the combustor / heat exchangers, and a combustion gas. A gas turbine for obtaining an output and a jet from a jet pump (28a) containing the exhaust gas are injected to the bottom of the ship, and superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat resistant limit temperature is injected. A steam-gas turbine combined engine transport power generation device including a jet pump (28c) including a superheated steam jet port for injecting water into a suction bottom of a ship, and a device for moving a ship by the power of the respective jet jet pumps. 19. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, a compressor for supplying compressed air to the combustor / heat exchanger, and combustion gas And a jet turbine including the exhaust gas from a jet pump (28a) is injected into the bottom of the ship, and 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 is injected. A steam jet turbine including a superheated steam jet port for injecting water into the bottom of a ship by suction and a device for moving a ship by the force of the respective jet jet pumps. 20. The steam and gas turbine combined engine transport power generation equipment according to claim 18 or 19, wherein one of the compressor and the gas turbine is a full blade. 21. A plurality of combustors and heat exchangers whose pressure and length are increased by making the water-cooled outer wall a helical welding structure, and a full-blade compressor that supplies compressed air to the combustors and heat exchangers. All-blade steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature, and power transmission for rotating and moving wheels by the output. And a steam-gas-turbine combined-engine transport power generator having a device. 22. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. An all-blade steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and a power for rotating and moving wheels by the output. A steam-gas-turbine combined-engine transport power generator having a transmission device. 23. A plurality of combustor / heat exchangers whose pressure is increased and lengthened by using a spirally welded water cooling outer wall, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A steam gas having a steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, and a power transmission device for rotating and moving wheels by the output. Turbine united engine transport power generation equipment. 24. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, a compressor for supplying compressed air to the combustor / heat exchanger, and combustion gas Steam having a superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, and a power transmission device for rotating and moving wheels by the output. Gas turbine combined engine transport power generation equipment. 25. The power generation equipment for a combined steam and gas turbine engine according to claim 23 or 24, wherein one of the compressor and the steam gas turbine is a full blade. 26. The power transmission surface (31) of the rail (54) and the wheel (55) according to claim 21 to 25, wherein the power transmission surface (31) is provided with low unevenness (40), respectively, and the front and rear of the wheel in the traveling direction. A bar magnet (33) or an electromagnet (34) is provided between the rail and the rail (54) to apply a suction force. 27. A plurality of combustors and heat exchangers whose pressure and length are increased by using a water-cooled outer wall as a spiral welding structure, and a full blade compressor that supplies compressed air to the combustors and heat exchangers. All rotor blade steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistant limit temperature, and for rotating the blades by the output to levitate the airframe And a superheated steam injection port including the exhaust gas. 28. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. An all-blade steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature, and the blades are rotated by the output to levitate the airframe. Gas turbine united engine transport power generation device having a power transmission device for the same and a superheated steam injection port including the exhaust gas. 29. A plurality of combustor / heat exchangers whose pressure is increased and lengthened by using a spirally welded outer wall for water cooling, a compressor for supplying compressed air to the combustor / heat exchanger, and combustion gas. A steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, a power transmission device for rotating the blades by the output to levitate and move the airframe, and A steam-gas-turbine combined-engine transport power generation device having a superheated steam injection port including exhaust gas. 30. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, a compressor for supplying compressed air to the combustor / heat exchanger, and combustion gas And a steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, a power transmission device for rotating the blades by the output to levitate the airframe, and And a superheated steam injection port containing the exhaust gas. 31. The power generation equipment for a combined steam and gas turbine engine according to claim 28, wherein one of the compressor and the steam gas turbine is a full blade. 32. A plurality of combustors and heat exchangers of which pressure and length are increased by making a water-cooled outer wall a spiral welding structure, and a full-blade compressor for supplying compressed air to the combustor and heat exchangers; An all-blade steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat-resistant limit temperature, and for rotating the screw by the output to move the hull. A steam-gas-turbine combined-engine transport power generation device having a power transmission device and an exhaust port containing the superheated steam. 33. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, and a full blade compressor for supplying compressed air to the combustor / heat exchanger. An all-blade steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and a screw that is rotated by the output to move the hull. And a power transmission device and an exhaust orifice containing the superheated steam. 34. A plurality of combustor / heat exchangers whose pressure is increased and lengthened by using a water-cooled outer wall as a spiral welding structure, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A steam gas turbine that obtains an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, a power transmission device for rotating a screw by the output to move a hull, and the superheat A steam-gas-turbine combined engine transport power generator having an exhaust port containing steam. 35. A plurality of combustor / heat exchangers of high pressure and length as a spiral water cooling wall tube unit assembly structure, a compressor for supplying compressed air to the combustor / heat exchanger, and combustion gas And a steam gas turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, a power transmission device for rotating a screw by the output to move a hull, and A steam-gas-turbine combined-engine transport power generation device having an exhaust port containing superheated steam. 36. The steam and gas turbine combined engine transport power generation equipment according to claim 34 or 35, wherein one of the compressor and the steam gas turbine is a full blade. 37. The steam-turbine combined engine transport power generation equipment according to claim 32, wherein an exhaust port including the superheated steam is opened at the bottom of the ship. 38. A plurality of combustor / heat exchangers having a water-cooled outer wall formed as a spiral welding structure having a high pressure and a generator provided in the middle to increase the length, and compressed air is supplied to the combustor / heat exchanger. A full-blade compressor, a full-blade steam gas turbine that obtains output with superheated steam obtained by exchanging heat so that a combustion gas and a combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature, and heat generated by the exhaust gas and a generator. And a device for supplying electricity from a steam-gas-turbine-combined-engine transport power plant. 39. A plurality of combustor / heat exchangers which are pressurized as a spiral water-cooled wall tube unit assembly structure and provided with a generator in the middle and which are lengthened, and compressed air is supplied to the combustor / heat exchanger. All-blade compressor, a full-blade steam gas turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and heat and power generation by the exhaust gas And a device for supplying electricity from the power plant. 40. A plurality of combustor / heat exchangers whose water cooling outer wall is formed into a spiral welded structure with a high pressure and a generator is provided in the middle to increase the length, and compressed air is supplied to the combustor / heat exchanger. A compressor, a steam gas turbine that obtains an output with superheated steam obtained by exchanging heat so that a combustion gas and a combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature, and supplies heat from the exhaust gas and electricity from a generator. And a steam-gas-turbine combined engine transport power generator having a device for the same. 41. A plurality of combustor / heat exchangers which are pressurized as a spiral water-cooled wall tube unit assembly structure and provided with a generator in the middle and which are lengthened, and compressed air is supplied to the combustor / heat exchanger. A compressor that generates heat, a steam gas turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas and the combustion gas temperature are equal to or lower than the turbine heat resistance limit temperature, and supplies heat from the exhaust gas and electricity from a generator. And an apparatus for transporting steam and gas turbines. 42. The power generation equipment for a combined steam and gas turbine engine according to claim 40 or 41, wherein one of the compressor and the steam gas turbine is a full blade. 43. The steam turbine combined engine transport power generation equipment according to claim 1, wherein the superheated steam used in the jet pump uses superheated steam having a supercritical steam condition or less. 44. The steam turbine combined engine transport power generation equipment according to claim 1, wherein the steam gas turbine uses superheated steam under supercritical steam conditions. 45. The combustion gas supplied to the steam gas turbine is supplied to an intermediate stage according to the pressure, mixed with superheated steam, and directly reheated.
A steam-powered turbine combined engine transport power generation device according to any one of the above. 46. A part of the combustion gas supplied to the steam gas turbine is supplied from a pressure reducing means (30) on the upstream side higher than the pressure, mixed with superheated steam, and directly reheated. 46. The steam turbine combined unit transport power generator according to any one of claims 1 to 45. 47. The steam-turbine combined engine transport power generation equipment according to claim 11, wherein the jet pump (28c) has one or more superheated steam injection ports. 48. The steam-gas-turbine combined engine transport power generation equipment according to any one of claims 11 to 20, and 32 to 37, comprising one or more of the jet pumps (28c).