JP2001295665A - Steam and gas combination turbine engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide an internal combustion engine, capable of halving the fuel cost thereof, eliminating the exhaustion of pollutants including CO2, and supplying heat, electricity, and cold heat so as to urgently prevent global warming, reduce electric power fee charge, and reduce environmental pollution due to cars. SOLUTION: Heat exchange is conducted to the utmost by a combustor and heat exchanger of a steam and gas combination turbine, engine and the total heating amount of fuel approximately four times that of prior art is converted into the extremely superheated steam in a high pressure atmosphere with the same compressed air volume to a theoretical air/fuel ratio to near the calculated combustion gas exhaust temperature to -273 deg.C. Specific power is increased by condensed water, dry ice, or liquid nitrogen with a gravitational power which markedly increased by increasing a unit volume mass 1,700 to 1,000 times, and an evaporated film is formed in a space thereof from a heated turbine blade annularly cast for each stage to allow assured and easy heating to markedly reduce a heat amount consuming frictional loss, so as to eliminate waste of a reheating steam turbine. Thus, the heat efficiency of the steam and gas combination turbines can be increased to approximate 80%, the structure thereof can be simplified, and specific power can be increased significantly.

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 (fully rotating engine) which aims at zero harmful exhaust gas such as CO2 and NOx and at a heat efficiency or a power generation efficiency of 80%. A fuel supply means or a fuel vapor supply means is provided on the upstream side of the total number of combustors / heat exchangers of the turbine, and heat exchange cooling combustion control combustion or heat exchange cooling combustion superheated steam injection cooling combustion is performed in a high pressure atmosphere as much as possible. By performing controlled combustion, the temperature of the combustion gas inlet of the gas turbine or the steam gas turbine can be reduced to 600 ° C. or less, the pressure ratio can be increased to 10 MPa or more, which is twice or more the conventional technology, and the supplied fuel can be reduced to the stoichiometric air-fuel ratio. Gas turbine exhaust temperature by -273
° C, and the heat consumption of the gas turbine approaches 0,
In the process of generating output as combustion gas such as dry ice or liquid nitrogen, the turbine blades and the like are heated to a high temperature by combustion gas, superheated steam, electricity, etc. Provide a vaporization film between
With dry ice and liquid nitrogen, etc., whose unit mass, centrifugal force, and gravitational power have increased 1000 times or more, friction loss is minimal.
The gas turbine is driven by reducing the heat consumption to zero, and the thermal efficiency is approached to infinity, and the combustion gas with the smallest volume is the maximum of small and large output, and the compressed air of -273 ° C or higher is separated as dry ice, liquid nitrogen, etc. The gas turbine to be recovered. With the superheated steam of the total heat obtained by heat exchange,
In the process of driving the steam turbine, a vaporization film is provided between the high-temperature turbine blades and the condensed water whose unit volume, gravitational power, and centrifugal force have increased 1700 times, and the steam turbine is driven with a minimum friction loss. The present invention also relates to various types of steam gas turbine combined engines that aim to significantly increase the thermal efficiency.

Further, as a gas turbine + steam turbine = steam gas turbine, superheated steam such as supercritical pressure of the total heat obtained by infinitely exchanging heat with a combustor / heat exchanger is applied to the steam gas turbine. Supply to the upstream side to generate output,
A combustion gas having twice the head and the like × 4 times the mass of the prior art obtained by performing heat exchange at the middle stage optimal stage is supplied, and the heat consumption of the combustion gas approaches 0, and the superheated steam is cooled to cool the superheated steam. By stopping the increase in volume and providing a vaporization film between the high-temperature turbine blades and the condensed water, etc., a small, simple, and large-output steam gas turbine with minimal friction loss is achieved. In order to obtain an output from the combustion gas and the superheated steam, the amount of generation of the superheated steam, which is the combustion gas of hydrogen, is maximized, and a global warming gas (CO
2) etc. are dissolved and discharged, and emission of pollutant gas such as CO2 is reduced to 0.
And a steam gas turbine close to. For example, the superheated steam is stored in a superheated steam reservoir, and an output is obtained from the combustion gas and the superheated steam, including a solid rocket or the like launched from a space flight parent aircraft, which instantaneously terminates the injection of the superheated steam from the superheated steam reservoir. As a steam gas turbine, it can be used for various applications such as various aircraft, various ships, various vehicles, various heat and electricity and cold heat supply equipment, electricity supply equipment, etc. The present invention relates to various steam gas turbine combined engines.

[0003]

2. Description of the Related Art Japanese Patent Application Laid-Open No. 50-97737 discloses a prior art in which a heat exchanger is provided inside a gas turbine combustor in a combined steam turbine / gas turbine engine. The present invention provides a steam turbine cycle superheater or reheater in a high temperature region of a gas turbine combustor, thereby eliminating the need for a special auxiliary combustor.
The purpose is to increase the superheated steam temperature of the steam turbine cycle and improve the efficiency of the entire combined plant. Also, Japanese Patent Laid-Open No. 52
No. 156248 discloses that by performing evaporation by heat exchange with combustion gas between gas turbines, the temperature of waste gas at the outlet of the waste heat recovery boiler is reduced, and the boiler efficiency is improved. However, none of these aims to improve the thermal efficiency of the supercharging boiler cycle, and does not aim to simultaneously increase the pressure ratio and the specific output of the gas turbine, nor to increase the thermal efficiency of the gas turbine.

[0004] Further, as a prior application, a gas turbine combustor is improved.
No. 5074, Japanese Patent Application No. 7-335595, Japanese Patent Application No. 8-4
1998, Japanese Patent Application No. 8-80407, Japanese Patent Application No. 8-14
No. 3391, Japanese Patent Application No. 8-204049, Japanese Patent Application No. 8-2
No. 72806, Japanese Patent Application No. 9-106925, Japanese Patent Application No. 9-106
There are 181944, Japanese Patent Application No. 10-134720, Japanese Patent Application No. 10-134721, Japanese Patent Application No. 11-69406, and Japanese Patent Application No. 11-77189. The priority claim application based on the above-mentioned prior application generally includes a heat exchanger including a whole rotor blade and / or a plurality of combustors of a gas turbine being lengthened, and a water-cooled outer wall spirally provided as a high-pressure vessel. An apparatus and method that can simultaneously increase the pressure ratio and the specific output to the maximum without exceeding the turbine heat-resistant limit temperature by being able to convert most of the supplied heat into superheated steam, also serving as an exchanger. Thing.

[0005]

The above conventional internal combustion engine technology basically emits pollutant gas such as CO2 and global warming gas to the environment, so that power plants, automobiles, ships and airplanes, etc. And global warming acceleration sources,
It is an object of the present invention to provide various steam gas turbine combined engines in which the emission of pollution and global warming combustion gas such as CO2 is brought close to zero and the thermal efficiency or the power generation efficiency is about 80.

[0006]

Means for Solving the Problems Ideas will be described including numbers and the like. Important as an internal combustion engine is a mission to reduce harmful exhaust gas to zero and maximize thermal efficiency. Thermal efficiency and specific output are important factors in the performance of a gas turbine cycle. The higher the pressure ratio, the higher the thermal efficiency is obtained when the amount of compressed air is constant, and the amount of heat supplied to the cycle when the pressure ratio and the amount of compressed air are constant. Is larger, a larger specific output is obtained. 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, if the high temperature is considered to be a decrease in the mass per unit volume = a decrease in the work per unit volume, the heat efficiency x the specific output = the pressure ratio x the mass of the combustion gas = the speed x the mass. Because of its small size, in the same-volume gas turbine, the lower the combustion gas temperature at the turbine inlet, the greater the output that can be obtained, and the greater the pressure ratio. Therefore, the pressure ratio is set to about 10 MPa, which is twice the conventional value, and the combustion gas temperature at the gas turbine inlet is set to 400 ° C.
If it is below, the exhaust temperature will not be -273 ° C or less and it will not be explained, but superheat including supercritical, obtained by infinite heat exchange with a combustor and heat exchanger of the same input compressed air amount combustion The amount of steam = the compressed air-273 ° C or more and the total heat quantity or more?
+ The total heating value of the fuel is four times that of the conventional technology, and a huge superheated steam head x mass far exceeding the conventional state-of-the-art technology can be obtained, making it possible to drive a steam turbine etc. with the total heat.

In addition, since the exhaust gas temperature approaches -273 ° C., the gas turbine output with the same amount of compressed air and the consumed heat of approximately zero as the conventional gas = two times the head of the combustion gas × the mass of the combustion gas can be four times the mass. The heat efficiency or power generation efficiency can be greatly increased to around 80%. Since the exhaust gas temperature approaches -273 ° C, it is possible to separate and collect combustion gas as dry ice or liquid nitrogen. If tap water is cooled and stored with excessively large amounts of dry ice or liquid nitrogen, the ozone hole can be repaired by removing CFCs, eliminating commercial and household coolers. Cooling seawater with excessively large amounts of dry ice and liquid nitrogen enables CO2, nitrogen and oxygen to be supplied to the sea floor and deep sea, enabling the breeding of seaweed and deep-sea fish. For example, if a combustor / heat exchanger converts heat into superheated steam as much as possible and converts it into electricity with a steam turbine, the greater the amount of power generation, the greater the production of cold heat. It is possible to cool the section almost free of charge and to create an optimal environment.
In this case, a gas turbine can be designed to be compact in order to generate power with dry ice or liquid nitrogen with a small volume and a large mass, but the turbine blade can be designed with an annular casting 84 that is easy to heat the core technology of the present invention. Outer diameter assembly annular portion 85
And an inner diameter assembling annular portion 86, and the heating blade 79 = the heating blade 81
+ Heating vanes 82 + Heating nozzles 83 provide a vaporization film between the heating blades 79 and dry ice or liquid nitrogen by heat to minimize friction loss.

When driving various automobiles, various ships, various aircraft, and various machines, since the demand for cooling is small, the micro gas turbine is directly driven by a combustor and a heat exchanger.
In response to power generation and cooling demands, most of the heat energy uses gas turbine + steam turbine = steam gas turbine. In other words, superheated steam such as supercritical pressure obtained by infinitely exchanging heat up to 600 ° C. or lower with a combustor / heat exchanger is supplied to the uppermost stream side of the steam gas turbine, and the combustion gas is supplied to the middle stream optimal stage. In the process of supplying power and generating a huge amount of superheated steam and combustion gas, the combustion gas whose adiabatic expansion temperature drops to the -273 ° C side releases adiabatic expansion condensation heat and cools the superheated steam that hesitates the temperature drop. Then, to the superheated steam condensate,
Combustion gases such as CO2 are synthesized and mixed and discharged, resulting in zero pollution exhaust gas and stoichiometric air-fuel ratio combustion. For example, the fuel combustion mass is increased to a stoichiometric air-fuel ratio up to about four times that of the prior art, the pressure ratio is doubled, the combustion gas is doubled, the head is doubled, the mass is increased, and the superheated steam is discharged at a temperature of -273 ° C. By cooling,
Of the supplied heat, the amount of combustion gas used by the steam gas turbine is greatly reduced to 0, etc., and the total heat is generated as superheated steam. In this process, the unit mass becomes 1700 times, and the centrifugal force and gravitational power are reduced. In order to generate power by the increased enormous amount of superheated steam condensate, the steam gas turbine is designed to be compact, and the outer diameter of the turbine blade 8 is formed as an annular casting 84 which is easy to heat the core technology of the present invention.
5 and inner diameter assembling annular section 86, and as a high-temperature heating blade 79, heat generates a vaporized film between the condensed water and the heating blade, minimizing friction loss, minimizing the volume of superheated steam, and greatly increasing thermal efficiency. Rise to

Combustion gas as a working gas for a gas turbine generally has a very high air ratio and includes air that is about four times the stoichiometric air-fuel ratio. Is not limited to numerical values). That is, in the conventional technology, nearly 80% of the compressed air that consumes a large amount of heat energy is wastefully discharged, and in addition, it is used to reduce the combustion temperature, resulting in a large loss. Approximately all of the compressed air can be made four times the fuel combustion mass up to the stoichiometric air-fuel ratio, and 100% combustion is used to eliminate NOx, and heat is exchanged as much as possible in a high pressure atmosphere. The superheated steam obtained by replacement is greatly increased to the total heat. Although the prevention of global warming has been loudly shouted, the actual situation in Japan is completely opposite, and the increase in CO2 emissions is accelerating. Pollution victims are also increasing on a global scale, especially those living along roads around metropolitan cities are reaching the limits of patience. To prevent global warming while operating an internal combustion engine, it is necessary to reduce CO2 emissions to zero as soon as possible. In order to eliminate pollution from internal combustion engines, the emission of pollutants such as NOx and suspended particulate matter should be reduced to zero as soon as possible. Therefore, according to the present invention, a substance that promotes fixing of harmful combustion gas water and harmless effluent is mixed into the water supply, etc. in accordance with the use of all internal combustion engines to make harmless exhaust and harmless effluent.

[0010]

DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiments and embodiments of the present invention will be described with reference to the drawings. The reference numerals are used to omit duplicate explanations, and the characteristic parts and the parts that are not explained are added and explained sequentially. In addition, some parts are described with numbers in order to specifically and clearly explain the intended and expected aspects of the invention, but are not limited to numbers.
As the combustor / heat exchanger 4 used in the present invention, a combustor / heat exchanger already applied for a patent is selected and used according to the application.

In the all-blade gas turbine shown in FIGS. 1, 2, and 5, the air compressed by the all-blade compressor and the all-blade compressor with a bypass adds heat without limitation to the combustor / heat exchanger. Exchange to make the amount of compressed air the same, up to the stoichiometric air-fuel ratio, to burn about four times the fuel of the conventional technology, and obtain the total heat value of the conventional fuel four times obtained by the heat exchange + -273 ° C of the compressed air. Above total heat is supplied as superheated steam such as supercritical pressure to all blade steam turbines and steam turbines. By supplying the combustion gas of about 600 ° C. obtained from the heat exchange from the most upstream side of the all blade gas turbine, the pressure ratio can be doubled to about 10 MPa, and the exhaust temperature of the all blade gas turbine can be reduced. -2
Approach 73 ° C. Therefore, in addition to generating the adiabatic expansion output of the combustion gas, the unit volume is reduced to about 1/1000, and it is possible to efficiently generate the output even with dry ice, liquid nitrogen, etc. .

An outer diameter assembly ring of an outer shaft device, in which all or a part of a turbine blade is easily heated by superheated steam or electricity or combustion gas, and the turbine blades are integrally cast into a ring for each stage to form a ring casting 84. By connecting the annular portion as the portion 85 and the inner-diameter assembly annular portion 86 of the inner shaft device and the like, the flow paths of the superheated steam, electricity, and combustion gas are connected at this portion to communicate with the respective turbine blades and the like. To facilitate heating. Heating with superheated steam or combustion gas is performed by improving the cooling of turbine blades by air or steam of the prior art to heating,
Electric heating is performed by improving the electric blanket cloth to metal. Heating blade 79 = Heating moving blade 81 + Heating stationary blade 82
+ A vaporization film is provided between the turbine blades and dry ice as the heating nozzle 83, etc., greatly reducing friction loss and greatly increasing thermal efficiency. Combustion gases such as dry ice and liquid nitrogen can be efficiently separated and collected.For example, as the amount of power generation increases, the production of dry ice and liquid nitrogen increases, so electricity costs are greatly reduced and tap water is reduced. Eliminate commercial coolers and household coolers, such as by cooling and storing whole urban areas to create an optimal cooling environment by eliminating CFCs and prevent global warming. It cools seawater with excessively large amounts of dry ice and liquid nitrogen, supplies CO2, nitrogen, and oxygen to the sea floor, breeds seaweed and fish and shellfish, and activates the sea area.

In the gas turbine shown in FIGS. 3, 4 and 6, the air compressed by the compressor / bypass compressor is exchanged by the combustor / heat exchanger 4 as much as possible, and the compressed air amount is the same. Up to the stoichiometric air-fuel ratio, allowing about four times the fuel of the conventional technology to be burned, and exchanging the total heat value of the conventional fuel obtained by performing the heat exchange plus -273 ° C. or more of the compressed air of -273 ° C. or more. As superheated steam such as critical pressure, it supplies almost the total amount of heat to steam turbines. By supplying the combustion gas of about 600 ° C. obtained from the heat exchange from the most upstream side of the gas turbine, the pressure ratio is doubled to about 10 MPa, the exhaust temperature of the gas turbine approaches -273 ° C., and the heat consumption Assuming that the combustion gas has a double drop and four times the mass of the conventional combustion gas, the thermal efficiency of the gas turbine approaches an infinite increase. Therefore, in the process of generating the adiabatic expansion output of combustion gas, output can be generated even with dry ice or liquid nitrogen, etc., whose unit volume has been reduced to about 1/1000, making it possible to design a gas turbine compactly.

[0014] All or a part of the turbine rotor blade, the stationary blade, and the nozzle are easily heated by steam, electricity, or combustion gas.
The turbine blades are integrally cast annularly in each stage to form an annular casting 84. The outer diameter assembly annular portion 85 of the outer shaft device, the inner diameter assembly annular portion 86 of the inner shaft device, and the like are connected by an annular portion, resulting in overheating. The steam, electricity, and combustion gas flow paths are connected at this part and communicate with each turbine blade to facilitate heating. Heating with superheated steam or combustion gas improves the cooling of the turbine blades with air or steam of the prior art to heating, and heating by electricity improves the electric blanket cloth to metal. Heating blade 79 = Heating moving blade 81 + Heating stationary blade 82 + Heating nozzle 83, a vaporization film is provided between the turbine blade and dry ice, liquid nitrogen, etc. to greatly reduce friction loss and greatly increase thermal efficiency To do. Combustion gases such as dry ice and liquid nitrogen can be efficiently separated and collected.For example, as the amount of power generation increases, the production of dry ice and liquid nitrogen increases, so electricity costs are greatly reduced and tap water is reduced. Eliminate commercial coolers and household coolers, such as by cooling and storing whole urban areas to create an optimal cooling environment by eliminating CFCs and prevent global warming. It cools seawater with excessively large amounts of dry ice and liquid nitrogen, supplies CO2, nitrogen, and oxygen to the sea floor, breeds seaweed and fish and shellfish, and activates the sea area.

In the all-blade steam gas turbine shown in FIGS. 7, 8, and 11, various fuels including pulverized coal are burned by air compressed by the all-blade compressor and the all-blade compressor with bypass. Then, heat is exchanged as much as possible in the combustor / heat exchanger 4 to make it possible to burn approximately four times the fuel of the conventional technology up to the stoichiometric air-fuel ratio with the same amount of compressed air. Approximately -273 ° C or more of the total heating value of the double fuel + the compressed air is supplied to the uppermost stream of the all-blade steam gas turbine as superheated steam such as supercritical pressure. Combustion gas of about 600 ° C obtained by heat exchange is converted to the middle stage optimal stage of all blade steam gas turbine.
The pressure ratio temperature is twice that of the prior art, around 10MPa 600
° C, the calculated combustion gas exhaust temperature -27
By allowing superheated steam to be cooled down by using the combustion gas at around 3 ° C, the condensed water temperature of the exhaust gas from all moving blade steam gas turbines is greatly increased to 100 ° C or less. Therefore, in the process of generating the output by the superheated steam and the combustion gas, the superheated steam is cooled by the combustion gas to stop the increase in the volume. Cooling superheated steam with combustion gas, such as pulverized coal, to generate power including a huge amount of condensed water, makes it possible to design an all-blade steam gas turbine with a significantly simpler, smaller and larger output.

An outer diameter assembly annular portion 85 of the outer shaft device, in which all or a part of the turbine blade is easily heated by steam, electricity, or combustion gas, and the turbine blade is integrally cast into a ring for each stage to form a ring casting 84. And, by connecting the annular portion as the inner diameter assembly annular portion 86 of the inner shaft device, the flow paths of the superheated steam, electricity, and combustion gas are connected at this portion and communicated with the respective turbine blades and the like for heating. Facilitates. Heating with superheated steam or combustion gas improves the cooling of the turbine blades with air or steam of the prior art to heating, and heating by electricity improves the electric blanket cloth to metal. As the heating blade 79 = the heating blade 81 + the heating stationary blade 82 + the heating nozzle 83, etc., a vaporization film of water vapor is provided between the high-temperature turbine blade and the condensed water, so that the friction loss can be greatly reduced and the output is generated. You. When using combustion gas as pulverized coal to increase the output by increasing the mass, since pulverized coal contains combustion gas, cooling of superheated steam by pulverized coal is assumed,
A vaporizing film is installed between the high-temperature turbine blade and the condensed water + pulverized coal to generate output. In the process of generating power, respectively, polluted gas such as CO2 is dissolved and mixed in condensed water and discharged.
Reduce emission of pollutant gas such as O2 to zero.

In the steam gas turbine shown in FIGS. 9, 10 and 12, the air compressed by the compressor and the bypass-added compressor can be used regardless of the type of fuel, such as up to three types of co-firing including pulverized coal. By burning various fuels and exchanging heat infinitely in the combustor / heat exchanger 4, it is possible to burn about four times as much fuel as the conventional technology up to the stoichiometric air-fuel ratio with the same amount of compressed air. Obtained conventional 4-fold fuel total heat generation + -2 of compressed air
Almost total heat of 73 ° C or more is supplied to the uppermost stream of a steam gas turbine as superheated steam such as supercritical pressure. By supplying combustion gas of about 600 ° C obtained by heat exchange to the middle stage of the middle stage of the steam gas turbine, the pressure ratio and temperature are twice that of the conventional technology, and are supplied at about 600 ° C of about 10 MPa. By enabling the combustion gas exhaust temperature to be around -273 ° C and cooling the superheated steam by the combustion gas, the condensed water temperature of the exhaust gas of the steam gas turbine can be greatly increased below 100 ° C. Therefore, in the process of generating the output by the superheated steam and the combustion gas, the superheated steam is cooled by the combustion gas to stop the increase in the volume, and the heat of condensation is released to reduce the volume by 1 /.
The superheated steam, which hesitates to lower the temperature while being reduced to 1700, is cooled with combustion gas such as pulverized coal to generate an output including a huge amount of condensed water. It becomes.

The outer diameter assembly annular portion 85 of the outer shaft device, in which all or a part of the turbine rotor blade is easily heated by steam, electricity or combustion gas, and the turbine blade is integrally cast into a ring for each stage to form a ring casting 84. And, by connecting the annular portion as the inner diameter assembly annular portion 86 of the inner shaft device, the flow paths of the superheated steam, electricity, and combustion gas are connected at this portion and communicated with the respective turbine blades and the like for heating. Facilitates. Heating with superheated steam or combustion gas improves the cooling of the turbine blades with air or steam of the prior art to heating, and heating by electricity improves the electric blanket cloth to metal. As the heating blade 79 = heating blade 81 + heating stationary blade 82 + heating nozzle 83, etc., a vaporization film of steam is provided between the high-temperature turbine blade and the condensed water to generate output with greatly reduced friction loss. As a special case, if the output is to be increased by increasing the mass by using combustion gas as pulverized coal, since pulverized coal contains combustion gas, cooling of superheated steam by pulverized coal is assumed, and pulverized coal containing condensed water and high-temperature turbine blades A vaporizing film is provided between the two to generate power with increased mass and minimum friction loss.
In the process of each output generation, the pollutant gas such as CO2 is easily synthesized and dissolved in the condensed water. Substances and chemical substances are mixed in advance, and the pollutant gas such as CO2 is synthesized, dissolved and mixed in the condensed water and discharged. And emission of pollutant gas such as CO2 and CO2.

The full-blade steam turbine or the full-blade steam turbine compressor shown in FIGS. 13 and 14 is limited to the gas turbine combustor / heat exchanger 4 by the full-blade compressor or the air compressed by the compressor. Without heat exchange, it is possible to burn about 4 times the fuel of the conventional technology up to the stoichiometric air-fuel ratio with the same amount of compressed air,
The total heat generation of the conventional quadruple fuel obtained by the heat exchange + approximately 273 ° C. or more of the compressed air is converted into superheated steam such as supercritical pressure, etc. In the process of generating output by superheated steam dynamic pressure, it generates condensed water between the turbine blades and generates high frictional loss, which significantly reduces thermal efficiency. In addition, the conventional technology employs a reheat turbine, and has a disadvantage that the structure becomes very complicated. Therefore, the unit mass and gravitational power were increased by 1,700 times, etc., and an output including a huge amount of condensed water was generated. In addition, the reheat turbine was abolished and the all-blade steam turbine was greatly simplified. You.

The outer diameter assembly annular portion 85 of the outer shaft device, in which all or a part of the turbine rotor blade is easily heated by steam, electricity or combustion gas, and the turbine blade is integrally cast annularly in each stage to form an annular casting 84. And, by connecting the annular portion as the inner diameter assembly annular portion 86 of the inner shaft device, the flow paths of the superheated steam, electricity, and combustion gas are connected at this portion and communicated with the respective turbine blades and the like for heating. Facilitates. Heating with superheated steam or combustion gas improves the cooling of the turbine blades with air or steam of the prior art to heating, and heating by electricity improves the electric blanket cloth to metal. Heating blade 79 = Heating moving blade 81 + Heating stationary blade 82 + Heating nozzle 83, etc., provided a vaporization film of water vapor between the high-temperature turbine blade and the condensed water. Combustion gas is synthesized and mixed, and the emission is devised so that it is close to zero emission gas such as CO2.

The steam turbine or the steam turbine compressor shown in FIGS. 15 and 16 exchanges heat as much as possible in the gas turbine combustor / heat exchanger 4 with the air compressed by the gas turbine compressor, so that the compressed air amount is the same. The fuel can be burned up to about four times that of the conventional technology up to the stoichiometric air-fuel ratio, and the total calorific value of the conventional fuel obtained by performing the heat exchange plus -273 ° C. or more of the compressed air of -273 ° C. or more is supercritical. As superheated steam such as pressure,
In the process of supplying power to the uppermost stream of the steam turbine shown in FIG. 16 and generating output due to superheated steam dynamic pressure, condensed water is generated between the turbine rotor blades and stationary blades, and the thermal efficiency is greatly reduced due to large friction loss. To do. In addition, the conventional technology employs a reheat turbine, and has a disadvantage that the structure becomes very complicated. Therefore, the unit mass and gravitational power are increased by 1700 times, etc., and an output is generated including an enormous amount of condensed water. The reheat turbine is almost completely eliminated, and the steam turbine is greatly simplified and designed to be small and large output. To do.

All or a part of the turbine rotor blade, the stationary blade, and the injection port are easily heated by steam, electricity, or combustion gas.
4, the outer diameter assembly annular portion 85 of the outer shaft device, the inner diameter assembly annular portion 86 of the inner shaft device, and the like are connected by an annular portion, so that the flow path of superheated steam, electricity, and combustion gas is formed in this portion. Connected to each turbine blade, etc. to facilitate heating. Heating with superheated steam or combustion gas improves the cooling of the turbine blades with air or steam of the prior art to heating, and heating by electricity improves the electric blanket cloth to metal. Heating blade 79 = heating blade 81
+ Heating vanes 82 + Heating nozzles 83, etc. are provided with a vaporization film of water vapor between the high-temperature turbine blades and vanes and the nozzles and the condensed water, enabling a significant reduction in friction loss. Combustion gas is synthesized and mixed and discharged to improve C
Close to zero emission gas such as O2.

In FIG. 1 to FIG. 16, the heating blade 81, the heating stationary blade 82, and the heating nozzle 83 of the turbine heating blade 79 heated by steam, electricity or combustion gas are used for the turbine blade by air or steam. There is a completely opposite purpose of prior art, which cools the gas and raises the gas turbine combustion gas inlet temperature to raise the turbine heat resistance limit temperature.
Since the cooling and heating methods may be the same, the turbine heating moving blade 81 and the heating stationary blade 8 are heated by steam or combustion gas.
2 and the heating nozzle 83, all the cooling methods were diverted to the heating method, and the one that had cooled the most upstream side was expanded from the most downstream heating nozzle 83 toward the upstream side to expand the heating blade. Heating vanes 82 and heating blades 8 in the uppermost stream according to
Move on to heating 1. As for the heating rotor blade 81, the heating stationary blade 82, and the heating nozzle 83 of the turbine heating blade 79 that is heated by electricity, there are an electric blanket and an electric cushion in the prior art. By changing, the same idea can be used to heat the turbine heating blade 81, the heating stationary blade 82, and the heating nozzle 83.

FIGS. 17a, 17b, 17c, and 17d
-The magnetic friction power transmission device 14 will be described with reference to Figs. 17e, 17f, and 18. Various power transmission devices including normal speed change and reverse rotation mainly use a gear device.
For this reason, in order to require a sliding tooth surface including a large load on the tooth surface, in addition to requiring lubricating oil, the frictional heat loss is extremely large, and the transmission device for large power including high speed rotation is required. There is a problem that it cannot be used. For this reason, in order to commercialize an all-blade / steam gas turbine combined engine, an ultra-high-speed and large-power transmission device by rolling contact is indispensable. In order to do so, a power transmission device by rolling contact is required, in which the sliding tooth surfaces of the gear device are almost zero.

For this reason, the rolling contact power transmission device is used as the low unevenness 40 in which the meshing height of the gears is reduced as much as possible, as shown in FIG. 18 in the rotation direction 35 on the upstream and downstream sides, or on the upstream or downstream side. , A bar magnet 33 or an electromagnet 34, and utilizing the strong attractive force of the magnet, for example, FIG.
a, FIG. 17b, FIG. 17c, FIG.
7a and 37a and 37b and 37b, or FIG.
17e and 17f of various magnetically-attached friction wheels 39 and 39,
Alternatively, it is preferable to use the entire magnetic friction power transmission device 14 including various combinations such as the inner magnetized friction wheel device 49a and the inner magnetized friction wheel device 49b shown in FIGS. In other words, by approaching rolling contact, friction heat loss is greatly reduced, and ultra-high-speed large-power transmission equipment and water-free pollution-free water cooling can be used instead of lubricating oil.

Referring to FIGS. 17, 19 and 20, the magnetic friction power transmission device 14 will be described. Instead of various gears,
Various magnetized friction wheels 37a and 37b and various internal magnetized friction wheels 38
a.38b, various magnetically-attached friction wheels 39, various internal-magnetized friction wheels 44 not shown, etc.
As 0, for example, a spur gear is replaced by a flat irregularity 41 car, a helical gear is replaced by a helical gear irregularity 42 car, a yamaba gear is replaced by a yamaba irregularity 43 car, and a spur internal gear is replaced by a spur inner irregularity 41 car.
The a wheel is replaced with a helical internal gear, and the boss internal unevenness 42a is replaced with a yamaba internal gear. As a result, various types of magnetic friction power transmission devices 14 are configured and used as the magnetic friction power transmission device 14 in the same manner as known various gear type power transmission devices.

The magnetized friction wheel 37a shown in FIGS. 17a and 17b
Are magnetized on the left and right in the radial direction of a ring-shaped ferromagnetic material, the magnetic poles of which are extended to the outer radial power transmission surface 31 with both sides sandwiched by a ring-shaped yoke 47. The power transmission surface is provided with a friction increasing and durable means 45 in an annular shape, and the outer peripheral surface thereof is provided with flat irregularities 41 and boss irregularities 42 of low irregularities 40, as magnetized friction wheels 37a and 37a, respectively. Used as rolling contact magnetic friction power transmission device 14.

A magnetized friction wheel 37b shown in FIG. 17C is configured such that N-poles and S-poles of magnetic poles are magnetized on the inner and outer diameter sides of a ring-shaped ferromagnetic material, and the yoke 47 is moved from the inner circumference side of the magnet. It extends to the left and right outer diameter power transmission surfaces 31, and a friction increasing and durable means 45 is provided between the yoke and the magnet to the power transmission surfaces to be enlarged and fixed to the power transmission surfaces. 43 is provided and used as the magnetic friction power transmission device 14 in rolling contact as the magnetized friction wheels 37b, 37b, etc., respectively.

The magnetically attached friction wheel 39 shown in FIGS. 17d, 17e and 17f is a power transmission surface 3 of an outer diameter surface of a ring-shaped ferromagnetic material.
1 is provided with friction increasing and durable means 45, and on its outer peripheral surface, flat irregularities 41, boss irregularities 42, and yamaba irregularities 43 of low irregularities 40 are respectively provided, and magnetically attached friction wheels 39a, 39b, 39, respectively.
Used as rolling contact magnetic friction power transmission device 14 as c.

FIGS. 18a and 18b show a bar magnet 33 and an electromagnet 34 provided on the upstream side and the downstream side in the rotational direction of FIGS. 17c and 17a, respectively. The poles are repelling bar magnets 33 and electromagnets 34, the different poles are to double the attraction force, and the frictional force is increased to make the low irregularities 40 as low as possible. The same poles are repelling bar magnets 33 and electromagnets 34. Is the simplest clutch.

The inner magnetized friction wheel device 49a shown in FIG. 19 magnetizes N and S poles of magnetic poles on the left and right sides in the radial direction of a ring-shaped ferromagnetic material, and the both sides thereof are ring-shaped yoke 47. A friction increasing and durable means 45 is annularly provided in the concave portion of the inner diameter between the yokes, and the inner surface of the yoke and the inner peripheral surface of the yoke are provided with a low unevenness 40. Unevenness 4
3a, the inner magnetized friction wheel 38 is magnetized with N and S poles of magnetic poles on the left and right sides in the radial direction of a ring-shaped ferromagnetic material inside thereof, and both sides thereof are ring-shaped yoke 47. And is fixed to the outer radial power transmission surface 31 by protruding from the outer radial direction power transmission surface 31. A friction increasing and durable means 45 is annularly provided in the outer diameter concave portion between the yokes. An uneven magnet 43 is provided to form a magnetized friction wheel 37a, and an electromagnet 34 for attracting different poles is provided on the upstream and downstream sides in the rotational direction to be used as the magnetic friction power transmission device 14 in rolling contact.

The inner magnetized friction wheel device 49b shown in FIG. 20 magnetizes the N and S poles of the magnetic poles on the inner and outer diameter sides of a ring-shaped ferromagnetic material, and connects the yoke 47 to the outer peripheral side of the magnet. To the power transmission surface 31 on the left and right sides, a friction increasing and durable means 45 is provided between the yoke and the magnet to the power transmission surface, and the power transmission surface is enlarged and fixed to the power transmission surface. An inner magnetized friction wheel 38b is provided with irregularities 41a, and N-poles and S-poles of magnetic poles are magnetized on the inner and outer diameter sides of a ring-shaped ferromagnetic material inside the inner magnetized friction wheel 38b. It extends from the inner peripheral side to the left and right outer diameter power transmitting surfaces 31, and a friction increasing and durable means 45 is provided between the yoke and the magnet to the power transmitting surface to be enlarged and fixed to the power transmitting surface. 40 are provided with flat irregularities 41 to form a rolling friction magnetic transmission device 14 as a magnetized friction wheel 37b. You use.

The magnetized friction wheels 37a and 37a of the magnetized friction wheel device 51a shown in FIG. 21 magnetize N and S poles of magnetic poles on the left and right in the radial direction of a plurality of annular ferromagnetic materials, respectively. They are alternately arranged, and both sides thereof are alternately sandwiched by annular plate-shaped yokes 47 so as to protrude from the outer radial power transmission surface 31 and are fixed. And extended to the power transmission surface, and provided with flat irregularities 41 of low irregularities 40 on the outer peripheral surface thereof. Electromagnets 34 are provided on the upstream side in the rotation direction 35 as magnetized friction wheels 37a and 37a, respectively. Only the side with different polarity has increased the attractive force as a magnet to attract,
Used as rolling contact magnetic friction power transmission device 14.

The magnetized friction wheels 37b and 37b of the magnetized friction wheel device 51b shown in FIG. 22 magnetize N and S poles of magnetic poles on the inner and outer diameter sides of a plurality of annular cylindrical ferromagnetic materials, respectively. Then, the yokes 47 are respectively moved from the inner peripheral side of the magnet to the left and right outer diameter power transmission surfaces 31.
To the power transmission surface, a friction increasing and durable means 45 is provided between the yoke and the magnet to expand and adhere to the power transmission surface, and a Yamaba unevenness 43 of the low unevenness 40 is provided on the outer peripheral surface thereof. Electromagnets 34 are provided on the upstream side and the downstream side in the rotation direction 35 as the magnetized friction wheels 37b, 37b, respectively. The attraction force is increased as a magnet for attracting a different pole on the upstream side, and the same pole repels on the downstream side. Used as a rolling contact magnetic friction power transmission device 14 in the form of a magnet.

An apparatus driven by the rotational force of the combined steam gas turbine engine shown in FIG. 23 will be described. 1 to 6, the exhaust gas temperature is set to -273.
℃, as the amount of power generation increases, it is possible to increase the amount of cold heat such as dry ice and liquid nitrogen, so it is mainly used for ultra-large power generation equipment as small as possible, and heat, electricity and cold heat are used. Supply and collect and collect huge amount of dry ice and liquid nitrogen, etc., and as a dumping place of too much cold heat, select cold heat to cool seawater and supply oxygen, CO2, nitrogen, etc. to the sea floor, Revitalize the sea area.
7 to 12, the exhaust gas temperature is around the saturated steam temperature, and in the process of generating output by the huge amount of condensed water, pollutant gas such as CO2 is added to the condensed water. Because it can be synthesized and mixed and discharged, it is mainly used for various ships, various aircraft, various vehicles, various machines, various ships, and various fighters. 13 to 16, a large amount of condensed water in which the unit mass per unit volume is increased by 1700 times and the centrifugal force and the gravitational power are greatly increased by heating the turbine blades. Because the process of generating power can dramatically reduce friction loss, the thermal efficiency is dramatically increased and used for all of the above devices.

[0036]

The present invention is a combustor and heat exchanger for various steam gas turbine combined engines including all rotor blades, and performs a heat exchange without limit to reduce the fuel combustion mass up to the stoichiometric air-fuel ratio. And the inlet temperature of a gas turbine or a full-rotor blade gas turbine from about 600 ° C. or lower to about 400 ° C., so that the pressure ratio can be doubled to about 10 MPa, and the turbine rotor blade and the stationary blade and Including the injection port, as an integral casting of the turbine blades in a ring for each paragraph, in order to easily heat all or a part with steam or electricity or combustion gas,
Even when the exhaust temperature approaches -273 ° C, a friction film in the process of generating an output by a large dynamic pressure by generating a vaporized film between the turbine rotor blade and the like and dry ice or liquid nitrogen, etc. is greatly reduced. It has the effect of reducing the size of the gas turbine, and has the effect of being able to design a compact gas turbine. The effect of lowering the electricity bill and recovering global warming combustion gas such as CO2 emitted from power plants etc. most efficiently is also large. The abolition of business and household coolers and the elimination of CFCs will also have the effect of preventing global warming. As the amount of power generation increases, the production of dry ice and liquid nitrogen will increase. It has an effect of breeding and activating seaweeds and fishes by supplying oxygen and nitrogen and oxygen.

The present invention is a combustor / heat exchanger for various steam gas turbine combined engines including all the moving blades, and performs a heat exchange as much as possible to achieve a stoichiometric air-fuel ratio to increase the fuel combustion mass to about four times that of the prior art. And the combustion gas inlet temperature of a steam gas turbine or a full-blade steam
The pressure ratio can be doubled to 10MP because the temperature can be around 00 ° C.
a) The turbine blades, stator blades, and injection port, including the turbine rotor blades and nozzles, are integrally cast annularly in each stage, and all or part of the turbine blades is easily heated with steam, electricity, or combustion gas. This has the great effect of significantly reducing the large friction loss of condensed water generated in the process of generating output by the large dynamic pressure of steam, by forming a vaporized film between the turbine blades and the condensed water. Therefore, the effect of simplifying the structure by completely eliminating the normal reheating cycle is great,
The combustion gas supplied in the process of generating output releases the heat of condensation to 1/1700 condensed water, cools the superheated steam that avoids the temperature drop, and synthesizes combustion gas such as CO2 into a huge amount of condensed water. It has a great effect of dissolving and mixing to make it possible to discharge, and has the effect of greatly reducing pollution such as CO2 that can be discharged from various automobiles, various ships, various airplanes, and various mechanical devices.

The present invention is a combustor and heat exchanger for various steam gas turbine combined engines including all blades, and the fuel combustion mass is increased to about the stoichiometric air-fuel ratio up to about four times that of the prior art by exchanging heat infinitely. And the combustion gas inlet temperature of the gas turbine, all blades gas turbine, steam gas turbine and all blades steam gas turbine can be changed from 600 ° C or less to around 400 ° C, so the pressure ratio is doubled to around 10MPa. Is possible. The turbine blades, including the turbine blades, the stationary blades, and the nozzles of the steam turbine and all blades steam turbine driven by the superheated steam obtained by exchanging heat with the combustor and heat exchanger, are integrally cast with the turbine blades in a ring for each paragraph. By easily heating all or a part thereof with steam or electricity or combustion gas, large frictional loss of condensed water generated in the process of generating output due to the large dynamic pressure of superheated steam, It produces a steam vapor film between the water and the condensed water, which has the great effect of greatly reducing the temperature and has the effect of greatly increasing the thermal efficiency. Therefore,
Eliminating the usual complicated reheat turbine and making the structure compact is also a great effect. The huge amount of condensed water generated in the process of power generation is mixed with combustion gas such as CO2 to dissolve and mix.
It has a great effect of enabling emission, and also has the effect of significantly reducing pollution such as CO2 emitted from various vehicles, various ships, various airplanes, and various mechanical devices.

The greatest effect of the present invention is that in the conventional steam turbine technology, the saturation temperature of the turbine rotor blades and the stationary blade surface rises drastically due to the large dynamic pressure of the superheated steam in the process of generating the output, so that the amount of reheating is increased. Even so, it becomes humid steam (condensed water), which inevitably increases the friction loss of a huge area. More problematic is that the volume is greatly increased by reheating, so the structure is more complicated and the friction loss is greatly increased while the head x mass remains constant. Therefore, the present invention provides a unitary casting of a turbine blade including a heated rotor blade, a heating stationary blade, and a heating nozzle, in a ring-like manner in each stage, and easily heats all or a part of the blade with steam, electricity, or combustion gas. Volume mass of 17
Increased centrifugal force and gravitational power from 00 times to 1000 times, dramatically increasing the amount of heat consumed by generating vaporized film between condensed water, liquid nitrogen, dry ice, etc. and turbine blades Output can be generated with minimum and friction loss. Since the structure is significantly smaller and simpler than the conventional technology, and the heat consumption and friction loss are dramatically smaller than the conventional technology, the gas turbine, all-blade gas turbine, steam gas turbine, all-blade steam gas turbine, It has a significant effect on dramatically increasing the thermal efficiency of turbines and all-blade steam turbines.

[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 partial cross-sectional view showing an eleventh embodiment of the combined steam gas turbine engine.

FIG. 12 is a partial cross-sectional view showing a twelfth embodiment of the combined steam gas turbine engine.

FIG. 13 is a partial sectional view showing a first embodiment of the steam turbine compressor.

FIG. 14 is a partial sectional view showing a second embodiment of the steam turbine compressor.

FIG. 15 is a partial sectional view showing a third embodiment of the steam turbine compressor.

FIG. 16 is a partial sectional view showing a fourth embodiment of the steam turbine compressor.

FIG. 17 is a partial sectional view showing an embodiment of a magnetized friction wheel and a magnetically friction wheel.

FIG. 18 is a diagram illustrating a magnetized friction wheel device.

FIG. 19 is a partial cross-sectional view showing an embodiment of the inner magnetized friction wheel device.

FIG. 20 is a partial sectional view showing an embodiment of the inner magnetized friction wheel device.

FIG. 21 is a partial sectional view showing an embodiment of a magnetized friction wheel device.

FIG. 22 is a partial sectional view showing an embodiment of a magnetized friction wheel device.

FIG. 23 is an explanatory view showing a device driven by a combined steam gas turbine engine.

[Explanation of symbols]

1: water pipe 2: water supply pump 3: water supply 4: combustor and heat exchanger 5: superheated steam 6: steam pipe
7: Steam control valve 8: Annular compressed air reservoir 9: Annular combustion gas reservoir 10 Combustion gas 11: Fuel 1
2: Output shaft 13: 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 Exit 22: Annular socket 23: Annular socket
24: annular nozzle group 25: combustor outer box 26:
Water-cooled outer wall 27: Fuel vapor supply means 28: Bypass 29: Injector 30: Cooling blade 31: Power transmission surface 32: Superheated steam reservoir 33: Bar magnet 34: Electromagnet 35: Rotation direction 36: Magnetic pole 37: Magnetized friction wheel 38: Inner magnetized friction wheel 39: Magnetically magnetized friction wheel
40: low unevenness 41: flat unevenness 42: boss unevenness 43: Yamaba unevenness 44: inner magnetized friction wheel 4
5: friction increasing durability means 46: magnet part 47: yoke (for magnetized friction wheel) 48: insulating material 49a: inner magnetized friction wheel device 49b: inner magnetized friction wheel device 50: support shaft 51a: magnetized friction wheel Apparatus 51
b: magnetized friction wheel device 51c: magnetized friction wheel device 51d: magnetized friction wheel device 52: water-cooled outer wall unit 5
3: Tsuba 54: Water-cooled inner wall 55: Cooling means 5
6: Water injection means 57: Capillary discharge means 58: Exhaust heat exchanger 59: Superheated steam cylinder mouth 60:
Fuel nozzle 61: Needle valve 62: Small fuel hole 63: Fuel hole switch 64: Air hole switch 65: Air hole 66: Condensate heat exchanger
67: Condenser 68: Condensed water 69: Exhaust 7
0: tap water 71: warm heat 72: cold heat 73: cooling water 74: thrust 79: heating blade 80: yoke 81: heating moving blade 82: heating stationary blade 83: heating nozzle 84: annular casting 85: outer diameter assembling annular portion
86: Inner diameter assembling ring

──────────────────────────────────────────────────続 き Continued on the front page (51) Int.Cl. ⁷ Identification symbol FI Theme coat ゛ (Reference) // H02K 49/10 H02K 49/10 A

Claims (312)

[Claims] 1. An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and an annular casting (84) is assembled and assembled. A combined steam gas turbine engine comprising a heating blade (79) in each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20). 2. An all-blade steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are annularly cast (84) and assembled. A combined steam gas turbine engine comprising a heating blade (79) in each of an outer turbine rotor blade group (19) and an inner turbine rotor blade group (20) having a structure. 3. An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are assembled by annular casting (84). A combined steam gas turbine engine comprising a heating blade (79) in each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20). 4. A full-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio.
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam gas turbine engine including a heating blade (79). 5. An all-blade gas turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer turbines having an annular casting (84) and an assembled structure. A combined steam and gas turbine engine comprising a heating blade (79) in a blade group (19) and an inner turbine blade group (20). 6. In a full-blade steam gas turbine in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer structures is formed by annular casting (84) and assembled. A combined steam gas turbine engine comprising a turbine blade group (19) and an inner turbine blade group (20) including a heating blade (79). 7. An outer blade device and an inner shaft device, which are rotated in opposite directions by a generator, are coupled to each other at an optimum rotation ratio. A combined steam and gas turbine engine comprising a heating blade (79) in a blade group (19) and an inner turbine blade group (20). 8. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of which has an annular casting (84) and an assembled structure. A combined steam and gas turbine engine comprising a heating blade (79) included in an outer turbine blade group (19) and an inner turbine blade group (20). 9. In a gas turbine, an annular casting (8
4) Each of the outer turbine blade groups (1
9) and the inner turbine blade group (20)
9) A combined steam gas turbine engine comprising: 10. A gas turbine, comprising: an annular casting (8);
4) A combined steam gas turbine engine, wherein a heating blade (79) is included in each of the turbine rotor blades and the turbine stationary blades which are assembled. 11. In a steam gas turbine, a heating blade (79) is included in each of an outer turbine blade group (19) and an inner turbine blade group (20) formed into an annular casting (84) and assembled. A combined steam and gas turbine engine. 12. A steam gas turbine combined engine in a steam gas turbine, wherein a heating blade (79) is included in each of a turbine rotor blade and a turbine stationary blade which are assembled by annular casting (84). . 13. A steam turbine, comprising: an annular casting (8);
4) Each of the outer turbine blade groups (1
9) and the inner turbine blade group (20)
9) A combined steam gas turbine engine comprising: 14. In a steam turbine, an annular casting (8)
4) A combined steam gas turbine engine, wherein a heating blade (79) is included in each of the turbine rotor blades and the turbine stationary blades which are assembled. 15. In a steam turbine compressor, a heating blade (79) is included in each of an outer turbine blade group (19) and an inner turbine blade group (20) formed into an annular structure by an annular casting (84). A combined steam and gas turbine engine. 16. A steam gas turbine combined with a steam turbine compressor, wherein a heating blade (79) is included in each of the turbine moving blade and the turbine stationary blade formed into an assembled structure by annular casting (84). organ. 17. A heating blade (79) is provided to each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20), which are assembled by annular casting (84) in a full blade gas turbine. A combined steam gas turbine engine comprising: 18. A heating blade (79) for each of a group of outer turbine blades (19) and a group of inner turbine blades (20), which are assembled by annular casting (84) in an all-blade steam gas turbine. A combined steam and gas turbine engine comprising: 19. A heating blade (79) is provided to each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20) in the assembled structure by annular casting (84). A combined steam gas turbine engine comprising: 20. A full-blade steam turbine compressor, comprising:
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam gas turbine engine including a heating blade (79). 21. An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are assembled by annular casting (84). A combined steam gas turbine engine comprising: a heating blade (79) heated by steam in each of the outer turbine blade group (19) and the inner turbine blade group (20). 22. An all-blade steam gas turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio.
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam and gas turbine engine comprising a heating blade (79) for heating by steam. 23. An all-rotor steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and an annular casting (84) is assembled and assembled. A combined steam gas turbine engine comprising: a heating blade (79) heated by steam in each of the outer turbine blade group (19) and the inner turbine blade group (20). 24. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are annularly cast (84). Outer turbine blade group (19) and inner turbine blade group (20) each having an assembled structure
A steam gas turbine combined engine further comprising a heating blade (79) for heating with steam. 25. In a full-blade gas turbine in which an outer shaft device and an inner shaft device that rotate in mutually opposite directions by a generator are combined at an optimum rotation ratio, each outer turbine having an annular casting (84) and an assembled structure. A combined steam and gas turbine engine comprising: a moving blade group (19) and an inner turbine moving blade group (20) including a heating blade (79) heated by steam. 26. An all-blade steam gas turbine in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of which is formed by annular casting (84) into an assembled structure. A combined steam gas turbine engine comprising a turbine blade group (19) and an inner turbine blade group (20) including heating blades (79) heated by steam. 27. In a full-blade steam turbine in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer turbines has an annular casting (84) and an assembled structure. A combined steam and gas turbine engine comprising: a moving blade group (19) and an inner turbine moving blade group (20) including a heating blade (79) heated by steam. 28. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of which has an annular casting (84) and an assembled structure. A combined steam and gas turbine engine comprising a heating blade (79) heated by steam in an outer turbine blade group (19) and an inner turbine blade group (20). 29. In a gas turbine, an annular casting (8
4) Each of the outer turbine blade groups (1
9) The combined steam and gas turbine engine, wherein the turbine blade group (20) includes heating blades (79) for heating by steam. 30. In a gas turbine, an annular casting (8
4) A combined steam and gas turbine engine comprising a turbine blade and a turbine vane which are assembled to have a heating blade (79) heated by steam. 31. In a steam gas turbine, heating blades (79) heated by steam are provided to each of an outer turbine moving blade group (19) and an inner turbine moving blade group (20) which are formed into an annular structure by an annular casting (84). ). A combined steam gas turbine engine comprising: 32. A steam gas turbine, wherein each of the turbine rotor blades and the turbine stationary blades, which are assembled by annular casting (84), includes a heating blade (79) heated by steam. Gas turbine combined engine. 33. In a steam turbine, an annular casting (8
4) Each of the outer turbine blade groups (1
9) The combined steam and gas turbine engine, wherein the turbine blade group (20) includes heating blades (79) for heating by steam. 34. A steam turbine, comprising: an annular casting (8);
4) A combined steam and gas turbine engine comprising a turbine blade and a turbine vane which are assembled to have a heating blade (79) heated by steam. 35. In the steam turbine compressor, the outer blade moving blade group (19) and the inner turbine moving blade group (20), each of which is formed by annular casting (84) and assembled, are heated by steam to be heated. 79) A combined steam and gas turbine engine comprising: 36. A steam turbine compressor, wherein each of a turbine rotor blade and a turbine stationary blade formed into an assembled structure by annular casting (84) includes a heating blade (79) heated by steam. Steam gas turbine combined engine. 37. Heating blades for heating all steam turbine blades (19) and inner turbine blade groups (20) in a ring-cast (84) and assembled structure in an all-blade gas turbine. (79) A combined steam gas turbine engine comprising (79). 38. In an all-blade steam gas turbine, steam-heated steam is applied to each of the outer turbine blade group (19) and the inner turbine blade group (20), which are formed into an assembled structure by annular casting (84). A combined steam gas turbine engine comprising a blade (79). 39. Heating blades for heating all steam turbine turbines by means of steam to each of an outer turbine blade group (19) and an inner turbine blade group (20) formed into an annular structure by an annular casting (84). (79) A combined steam gas turbine engine comprising (79). 40. In a full bucket steam turbine compressor,
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam and gas turbine engine comprising a heating blade (79) for heating by steam. 41. An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and an annular casting (84) is assembled and assembled. A combined steam gas turbine engine comprising: a heating blade (79) heated by electricity in each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20). 42. An all-blade steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio.
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam gas turbine engine comprising a heating blade (79) heated by electricity. 43. An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are assembled by annular casting (84). A combined steam gas turbine engine comprising: a heating blade (79) heated by electricity in each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20). 44. An annular casting steam turbine compressor in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are coupled at an optimum rotation ratio. Outer turbine blade group (19) and inner turbine blade group (20) each having an assembled structure
A steam gas turbine combined engine, further comprising a heating blade (79) heated by electricity. 45. In a full blade gas turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer turbines has an annular casting (84) and an assembled structure. A combined steam gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20) including a heating blade (79) heated by electricity. 46. In an all-blade steam gas turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a generator are connected at an optimum rotation ratio, each of the outer structures is formed by annular casting (84) and assembled. A combined steam gas turbine engine comprising a turbine blade group (19) and an inner turbine blade group (20) including a heating blade (79) heated by electricity. 47. A full-blade steam turbine in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer turbines having an annular casting (84) and an assembled structure. A combined steam gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20) including a heating blade (79) heated by electricity. 48. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of which has an annular casting (84) and an assembled structure. A combined steam and gas turbine engine comprising: an outer turbine blade group (19) and an inner turbine blade group (20) including a heating blade (79) heated by electricity. 49. In a gas turbine, an annular casting (8
4) Each of the outer turbine blade groups (1
9) The combined steam and gas turbine engine, wherein the inner turbine moving blade group (20) includes a heating blade (79) heated by electricity. 50. In a gas turbine, an annular casting (8
4) A combined steam gas turbine engine, wherein each turbine rotor blade and turbine stationary blade having an assembled structure includes a heating blade (79) heated by electricity. 51. In a steam gas turbine, an outer turbine bucket group (19) and an inner turbine bucket group (20).
A steam gas turbine combined engine, further comprising a heating blade (79) heated by electricity. 52. A steam gas turbine, wherein each of the turbine rotor blades and the turbine stationary blades formed into an annular structure by annular casting (84) includes a heating blade (79) heated by electricity. Gas turbine combined engine. 53. In a steam turbine, an annular casting (8
4) Each of the outer turbine blade groups (1
9) The combined steam and gas turbine engine, wherein the inner turbine moving blade group (20) includes a heating blade (79) heated by electricity. 54. In a steam turbine, an annular casting (8
4) A combined steam gas turbine engine, wherein each turbine rotor blade and turbine stationary blade having an assembled structure includes a heating blade (79) heated by electricity. 55. In a steam turbine compressor, each of an outer turbine moving blade group (19) and an inner turbine moving blade group (20) formed into an annular structure by annular casting (84) is heated by electric heating blades (20). 79) A combined steam and gas turbine engine comprising: 56. A steam turbine compressor, wherein each of a turbine rotor blade and a turbine stationary blade formed into an assembled structure by annular casting (84) includes a heating blade (79) heated by electricity. Steam gas turbine combined engine. 57. In the all-blade gas turbine, heating blades for electrically heating the outer turbine blade group (19) and the inner turbine blade group (20) formed into an annular structure by annular casting (84). (79) A combined steam gas turbine engine comprising (79). 58. In an all-blade steam gas turbine, heating is performed by electrically heating each of the outer turbine blade group (19) and the inner turbine blade group (20), which are formed by annular casting (84) and assembled. A combined steam gas turbine engine comprising a blade (79). 59. A heating blade for electrically heating an outer turbine blade group (19) and an inner turbine blade group (20), which are assembled by annular casting (84), in an all-blade steam turbine. (79) A combined steam gas turbine engine comprising (79). 60. A full bucket steam turbine compressor, comprising:
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam gas turbine engine comprising a heating blade (79) heated by electricity. 61. An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and an annular casting (84) is assembled and assembled. A combined steam gas turbine engine comprising: a heating blade (79) heated by combustion gas in each of the outer turbine blade group (19) and the inner turbine blade group (20). 62. A full-blade steam gas turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio.
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam gas turbine engine comprising a heating blade (79) heated by combustion gas. 63. An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and an annular casting (84) is assembled and assembled. A combined steam gas turbine engine comprising: a heating blade (79) heated by combustion gas in each of the outer turbine blade group (19) and the inner turbine blade group (20). 64. In a full-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, an annular casting (84) is performed. Outer turbine blade group (19) and inner turbine blade group (20) each having an assembled structure
And a heating blade (79) heated by combustion gas. 65. In a full-blade gas turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each outer turbine having an annular casting (84) and an assembled structure. A combined steam gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20) including a heating blade (79) heated by combustion gas. 66. In a full-blade steam gas turbine in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer structures is formed by annular casting (84) and assembled. A combined steam gas turbine engine comprising a turbine blade group (19) and an inner turbine blade group (20) including a heating blade (79) heated by combustion gas. 67. A full-blade steam turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer turbines having an annular casting (84) assembly structure. A combined steam gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20) including a heating blade (79) heated by combustion gas. 68. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of which has an annular casting (84) and an assembled structure. A combined steam gas turbine engine comprising: an outer turbine blade group (19) and an inner turbine blade group (20) including heating blades (79) heated by combustion gas. 69. In a gas turbine, an annular casting (8
4) Each of the outer turbine blade groups (1
(9) The combined steam and gas turbine engine, wherein the turbine blade group (20) includes heating blades (79) heated by combustion gas. 70. In a gas turbine, an annular casting (8
4) A combined steam gas turbine engine, wherein each of the turbine blades and the turbine stationary blades having an assembled structure includes a heating blade (79) heated by combustion gas. 71. In a steam gas turbine, each of an outer turbine moving blade group (19) and an inner turbine moving blade group (20) formed into an annular structure by annular casting (84) is heated by a combustion gas. 79) A combined steam and gas turbine engine comprising: 72. A heating blade (79) for heating each of the turbine rotor blades and the turbine stationary blades, which are assembled by annular casting (84) in a steam gas turbine, with a combustion gas.
A combined steam and gas turbine engine comprising: 73. In a steam turbine, an annular casting (8
4) Each of the outer turbine blade groups (1
(9) The combined steam and gas turbine engine, wherein the turbine blade group (20) includes heating blades (79) heated by combustion gas. 74. In a steam turbine, an annular casting (8
4) A combined steam gas turbine engine, wherein each of the turbine blades and the turbine stationary blades having an assembled structure includes a heating blade (79) heated by combustion gas. 75. In a steam turbine compressor, heating blades are heated by combustion gas to each of an outer turbine blade group (19) and an inner turbine blade group (20) formed into an annular structure by annular casting (84). (79) A combined steam gas turbine engine comprising (79). 76. In a steam turbine compressor, each of the turbine rotor blades and the turbine stationary blades formed into an assembled structure by annular casting (84) has heating blades (7) heated by combustion gas.
9) A combined steam gas turbine engine comprising: 77. In an all-blade gas turbine, heating is performed by using combustion gas to heat the outer turbine blade group (19) and the inner turbine blade group (20) which are annularly cast (84) and assembled. A combined steam gas turbine engine comprising a blade (79). 78. In the all-blade steam gas turbine, the outer turbine blade group (19) and the inner turbine blade group (20), each of which is annularly cast (84) and assembled, are heated by the combustion gas. A combined steam gas turbine engine including a heating blade (79). 79. In the full-blade steam turbine, heating is performed by heating the outer turbine blade group (19) and the inner turbine blade group (20), which are annularly cast (84) and assembled, by a combustion gas. A combined steam gas turbine engine comprising a blade (79). 80. In a full bucket steam turbine compressor,
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam gas turbine engine comprising a heating blade (79) heated by combustion gas. 81. An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are assembled by annular casting (84). A combined steam and gas turbine engine comprising: an outer turbine moving blade group (19) and an inner turbine moving blade group (20) including a heating blade (79) and a device driven by the output. . 82. An all-blade steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio.
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam gas turbine engine comprising: a device driven by the output including a heating blade (79). 83. An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and an annular casting (84) is assembled. A combined steam and gas turbine engine comprising: an outer turbine moving blade group (19) and an inner turbine moving blade group (20) including a heating blade (79) and a device driven by the output. . 84. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are annularly cast (84). Outer turbine blade group (19) and inner turbine blade group (20) each having an assembled structure
A steam-turbine combined engine, characterized by further comprising a device driven by the output, including a heating blade (79). 85. In a full-blade gas turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer turbines has an annular casting (84) and an assembled structure. A combined steam gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20), including a heating blade (79) and a device driven by the output. 86. In a full-blade steam gas turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, an annular casting (84) is used to form each of the outer structures. A combined steam gas turbine engine comprising: a turbine blade group (19) and an inner turbine blade group (20), including a heating blade (79), and a device driven by the output. 87. A full-blade steam turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer turbines having an annular casting (84) and an assembled structure. A combined steam gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20), including a heating blade (79) and a device driven by the output. 88. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of which has an annular casting (84) and an assembled structure. A combined steam gas turbine engine comprising: an outer turbine rotor blade group (19) and an inner turbine rotor blade group (20) including a device driven by the output, including a heating blade (79). 89. In a gas turbine, the annular casting (8
4) Each of the outer turbine blade groups (1
9) and the inner turbine blade group (20)
9. A combined steam gas turbine engine comprising: a device driven by the output including the above 9). 90. In a gas turbine, an annular casting (8
4) A combined steam gas turbine engine comprising a turbine blade and a turbine stationary blade each having an assembled structure and including a device driven by the output, including a heating blade (79). 91. In a steam gas turbine, a heating blade (79) is included in each of the outer turbine moving blade group (19) and the inner turbine moving blade group (20) formed into an annular casting (84) and assembled structure. A combined steam gas turbine engine comprising a device driven by the output. 92. In a steam gas turbine, each of the turbine rotor blades and the turbine stationary blades formed into an annular structure by annular casting (84) is provided with a device including a heating blade (79) and driven by the output. A combined steam gas turbine engine. 93. In a steam turbine, an annular casting (8
4) Each of the outer turbine blade groups (1
9) and the inner turbine blade group (20)
9. A combined steam gas turbine engine comprising: a device driven by the output including the above 9). 94. In a steam turbine, an annular casting (8
4) A combined steam gas turbine engine comprising a turbine blade and a turbine stationary blade each having an assembled structure and including a device driven by the output, including a heating blade (79). 95. In the steam turbine compressor, a heating blade (79) is included in each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an annular structure by the annular casting (84). A combined steam gas turbine engine comprising a device driven by the output. 96. A steam turbine compressor, comprising a turbine rotor blade and a turbine stationary blade each having an annular casting (84) and an assembled structure, including a heating blade (79) and a device driven by the output. A combined steam and gas turbine engine. 97. In the all-blade gas turbine, a heating blade (79) is provided to each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an annular structure by the annular casting (84). A combined steam and gas turbine engine comprising: a device driven by the output. 98. A heating blade (79) for each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20), which is formed by annular casting (84) in an assembled structure, in a full blade steam gas turbine. A combined steam and gas turbine engine comprising a device driven by the output, including: 99. A heating blade (79) is provided to each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20) in the assembled structure by annular casting (84) in the all blade steam turbine. A combined steam and gas turbine engine comprising: a device driven by the output. 100. An outer turbine blade group (19) and an inner turbine blade group (20) each having an annular casting (84) and an assembled structure in a full blade steam turbine compressor.
A steam-turbine combined engine, characterized by further comprising a device driven by the output, including a heating blade (79). 101. An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and an annular casting (84) is assembled and assembled. The steam turbine, wherein each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20) includes a device driven by the output, including a heating blade (79) heated by steam. Gas turbine combined engine. 102. An all-blade steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are annularly cast (84) and assembled. Each of the outer turbine blade groups (19) and the inner turbine blade group (20) having a structure.
And a device driven by the output including a heating blade (79) heated by steam. 103. An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are assembled by annular casting (84). The steam turbine, wherein each of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20) includes a device driven by the output, including a heating blade (79) heated by steam. Gas turbine combined engine. 104. In a full-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, an annular casting (84) is performed. Outer turbine blade group (19) and inner turbine blade group (20) each having an assembled structure
And a device driven by the output including a heating blade (79) heated by steam. 105. In a full-blade gas turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer turbines has an annular casting (84) and an assembled structure. A combined steam and gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20) including a device driven by the output, including a heating blade (79) heated by steam. 106. In a full-blade steam gas turbine in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer structures is formed by annular casting (84) and assembled. A combined steam and gas turbine engine comprising: a turbine blade group (19) and an inner turbine blade group (20) including a device driven by the output, including a heating blade (79) heated by steam. 107. An outer turbine device in which an outer shaft device and an inner shaft device which rotate in mutually opposite directions by a generator are combined at an optimum rotation ratio, and each of the outer turbines has an annular casting (84) and an assembled structure. A combined steam and gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20) including a device driven by the output, including a heating blade (79) heated by steam. 108. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of which has an annular casting (84) and an assembled structure. A combined steam and gas turbine engine comprising: an outer turbine rotor blade group (19) and an inner turbine rotor blade group (20), including a heating blade (79) heated by steam and a device driven by the output. . 109. A heating blade (79) for heating a group of outer turbine moving blades (19) and inner turbine moving blades (20) in a gas turbine by annular casting (84) and assembled. A combined steam and gas turbine engine comprising a device driven by the output, including: 110. In a gas turbine, there is provided an apparatus for driving each turbine rotor blade and turbine vane having an assembling structure by annular casting (84), including a heating blade (79) heated by steam, with the output. A combined steam gas turbine engine comprising: 111. In a steam gas turbine, heating blades (79) heated by steam are provided to each of an outer turbine blade group (19) and an inner turbine blade group (20) formed into an annular structure by an annular casting (84). A) a steam-gas-turbine combined engine, comprising: a device driven by the output. 112. An apparatus for driving a steam gas turbine by using an output including a heating blade (79) heated by steam to each of a turbine moving blade and a turbine stationary blade formed into an annular structure by an annular casting (84). A combined steam and gas turbine engine comprising: 113. In a steam turbine, a heating blade (79) for heating by steam to each of an outer turbine blade group (19) and an inner turbine blade group (20) formed into an annular structure by an annular casting (84). A combined steam and gas turbine engine comprising a device driven by the output, including: 114. In a steam turbine, there is provided an apparatus for driving each turbine rotor blade and turbine vane, which are assembled by annular casting (84), including a heating blade (79) heated by steam, with the output. A combined steam gas turbine engine comprising: 115. In the steam turbine compressor, the outer blade moving blade group (19) and the inner turbine moving blade group (20) which are formed by annular casting (84) into an assembled structure are heated by steam. 79) A combined steam gas turbine engine comprising a device driven by the output including the above 79). 116. A heating blade (79) for heating each of the turbine rotor blades and the turbine stationary blades formed into an assembled structure by annular casting (84) in a steam turbine compressor.
A combined steam and gas turbine engine comprising a device driven by the output, including: 117. Heating blades for heating all steam turbine blades (19) and inner turbine blade groups (20), which are formed by annular casting (84), in an all-blade gas turbine. (79) A combined steam gas turbine engine comprising a device driven by the output, including (79). 118. In a full bucket steam gas turbine,
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam and gas turbine engine comprising a device driven by said output, including a heating blade (79) heated by steam. 119. In an all-blade steam turbine, heated outer blades (19) and inner turbine blades (20), each of which is assembled by annular casting (84), are heated by steam. (79) A combined steam gas turbine engine comprising a device driven by the output, including (79). 120. An outer turbine blade group (19) and an inner turbine blade group (20) each having an annular structure (84) and assembled into an assembled structure in a full blade steam turbine compressor.
And a device driven by the output including a heating blade (79) heated by steam. 121. An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, an annular casting (84) and an assembling structure. Steam provided with a device driven by the output, including a heating blade (79) heated by electricity, in each of the outer turbine blade group (19) and the inner turbine blade group (20). Gas turbine combined engine. 122. An all-blade steam gas turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are coupled at an optimum rotation ratio, and are annularly cast (84) and assembled. Each of the outer turbine blade groups (19) and the inner turbine blade group (20) having a structure.
And a device driven by the output, including a heating blade (79) heated by electricity. 123. An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and an annular casting (84) is assembled and assembled. Steam provided with a device driven by the output, including a heating blade (79) heated by electricity, in each of the outer turbine blade group (19) and the inner turbine blade group (20). Gas turbine combined engine. 124. In a full-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are coupled at an optimum rotation ratio, an annular casting (84) is performed. Outer turbine blade group (19) and inner turbine blade group (20) each having an assembled structure
And a device driven by the output, including a heating blade (79) heated by electricity. 125. An outer turbine device in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are coupled at an optimum rotation ratio, and each of the outer turbines is formed by annular casting (84) into an assembled structure. A combined steam and gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20) including a device driven by the output, including a heating blade (79) heated by electricity. 126. In a full-blade steam gas turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each outer structure is formed by annular casting (84). A combined steam gas turbine engine comprising: a turbine blade group (19) and an inner turbine blade group (20) including a device driven by the output, including a heating blade (79) heated by electricity. 127. An outer blade device and an inner shaft device, which are rotated in opposite directions by a generator, are connected to each other in an optimum rotational ratio at an optimum rotation ratio. A combined steam and gas turbine engine comprising: a rotor blade group (19) and an inner turbine rotor blade group (20) including a device driven by the output, including a heating blade (79) heated by electricity. 128. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of which has an annular casting (84) and an assembled structure. A combined steam / gas turbine engine comprising: an outer turbine rotor blade group (19) and an inner turbine rotor blade group (20) including a device driven by the output including a heating blade (79) heated by electricity. . 129. In a gas turbine, a heating blade (79) for electrically heating each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an annular structure by annular casting (84). A combined steam and gas turbine engine comprising a device driven by the output, including: 130. In a gas turbine, an apparatus for driving the turbine rotor blade and the turbine vane, each of which has a ring-shaped casting (84) and an assembled structure, including a heating blade (79) that is heated by electric power, with the output. A combined steam gas turbine engine comprising: 131. Heating blades (79) that are heated by electricity to each of a group of outer turbine blades (19) and a group of inner turbine blades (20) that have been assembled by annular casting (84) in a steam gas turbine. A) a steam-gas-turbine combined engine, comprising: a device driven by the output. 132. In a steam gas turbine, an apparatus for driving the turbine rotor blade and the turbine vane, each of which has an annular structure (84) and an assembled structure, including a heating blade (79) heated by electric power with the output. A combined steam and gas turbine engine comprising: 133. A heating blade (79) for electrically heating an outer turbine blade group (19) and an inner turbine blade group (20) in a steam turbine, which are annularly cast (84) and assembled. A combined steam and gas turbine engine comprising a device driven by the output, including: 134. In a steam turbine, an apparatus for driving the turbine rotor blade and the turbine vane, each of which has an annular structure (84) and an assembled structure, including a heating blade (79) that is heated by electric power and driven by the output. A combined steam gas turbine engine comprising: 135. In the steam turbine compressor, the outer blade moving blade group (19) and the inner turbine moving blade group (20), each of which is annularly cast (84) and assembled, are heated by electric heating. 79) A combined steam gas turbine engine comprising a device driven by the output including the above 79). 136. In a steam turbine compressor, a heating blade (79) for electrically heating each of the turbine moving blades and the turbine stationary blades formed into an annular structure by the annular casting (84).
A combined steam and gas turbine engine comprising a device driven by the output, including: 137. In the all-blade gas turbine, heating blades for electrically heating each of the outer turbine blade group (19) and the inner turbine blade group (20), which are assembled by annular casting (84). (79) A combined steam gas turbine engine comprising a device driven by the output, including (79). 138. A full bucket steam gas turbine, comprising:
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam gas turbine engine comprising: a device driven by the output including a heating blade (79) heated by electricity. 139. A heating blade for electrically heating each of the outer turbine blade group (19) and the inner turbine blade group (20) which are assembled by annular casting (84) in an all-blade steam turbine. (79) A combined steam gas turbine engine comprising a device driven by the output, including (79). 140. An outer turbine blade group (19) and an inner turbine blade group (20) each having an annular casting (84) and an assembled structure in a full blade steam turbine compressor.
And a device driven by the output, including a heating blade (79) heated by electricity. 141. An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, an annular casting (84) and an assembling structure. Each of the outer turbine moving blade group (19) and the inner turbine moving blade group (20) includes a device driven by the output, including a heating blade (79) heated by combustion gas. Steam gas turbine combined engine. 142. An all-blade steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and are annularly cast (84) and assembled. Each of the outer turbine blade groups (19) and the inner turbine blade group (20) having a structure.
And a device driven by the output including a heating blade (79) heated by combustion gas. 143. An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in mutually opposite directions by a magnetic friction power transmission device (14) are connected at an optimum rotation ratio, and an annular casting (84) is assembled and assembled. Each of the outer turbine moving blade group (19) and the inner turbine moving blade group (20) includes a device driven by the output, including a heating blade (79) heated by combustion gas. Steam gas turbine combined engine. 144. In a full-blade steam turbine compressor in which an outer shaft device and an inner shaft device rotating in opposite directions by a magnetic friction power transmission device (14) are coupled at an optimum rotation ratio, an annular casting (84) is performed. Outer turbine blade group (19) and inner turbine blade group (20) each having an assembled structure
And a device driven by the output including a heating blade (79) heated by combustion gas. 145. In a full-blade gas turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each outer turbine having an annular casting (84) and an assembled structure. A combined steam gas turbine engine comprising: a blade group (19) and an inner turbine blade group (20), including a heating blade (79) heated by combustion gas and a device driven by the output. 146. In a full-blade steam gas turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of the outer structures is formed by annular casting (84). A combined steam gas turbine engine comprising: a turbine blade group (19) and an inner turbine blade group (20) including a device driven by the output, including a heating blade (79) heated by combustion gas. . 147. A full-blade steam turbine in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each outer turbine having an annular casting (84) and an assembled structure. A combined steam gas turbine engine comprising: a blade group (19) and an inner turbine blade group (20), including a heating blade (79) heated by combustion gas and a device driven by the output. 148. An all-blade steam turbine compressor in which an outer shaft device and an inner shaft device which are rotated in opposite directions by a generator are connected at an optimum rotation ratio, each of which has an annular casting (84) and an assembled structure. A steam gas turbine unit comprising: an outer turbine moving blade group (19) and an inner turbine moving blade group (20), including a heating blade (79) heated by combustion gas and a device driven by the output. organ. 149. In a gas turbine, each of the outer turbine moving blade group (19) and the inner turbine moving blade group (20) formed into an annular structure by an annular casting (84) is provided with a heating blade (79) heated by combustion gas. A) a steam-gas-turbine combined engine, comprising: a device driven by the output. 150. A heating blade (79) for heating a turbine rotor blade and a turbine stationary blade, each of which has an annular structure (84) and an assembled structure, with a combustion gas in a gas turbine.
A combined steam and gas turbine engine comprising a device driven by the output, including: 151. In a steam gas turbine, the outer blade moving blade group (19) and the inner turbine moving blade group (20), each of which is formed by annular casting (84), are assembled into a heating blade heated by a combustion gas. 79) A combined steam gas turbine engine comprising a device driven by the output including the above 79). 152. In the steam gas turbine, each of the turbine blades and the turbine vanes, which are assembled by annular casting (84), are heated by a combustion blade (7) heated by combustion gas.
9. A combined steam gas turbine engine comprising: a device driven by the output including the above 9). 153. In a steam turbine, the outer blade moving blade group (19) and the inner turbine moving blade group (20) which are formed into an annular structure by annular casting (84) are heated by a combustion gas to heat the blades (79). A) a steam-gas-turbine combined engine, comprising: a device driven by the output. 154. In a steam turbine, heating blades (79) for heating the respective turbine rotor blades and turbine stationary blades, which are assembled by annular casting (84), with a combustion gas.
A combined steam and gas turbine engine comprising a device driven by the output, including: 155. In the steam turbine compressor, each of the outer turbine moving blade group (19) and the inner turbine moving blade group (20), which are formed by annular casting (84) and assembled, is heated by combustion gas. (79) A combined steam gas turbine engine comprising a device driven by the output, including (79). 156. In the steam turbine compressor, each of the turbine rotor blades and the turbine stationary blades formed into an annular structure by the annular casting (84) has heating blades (7) heated by combustion gas.
9. A combined steam gas turbine engine comprising: a device driven by the output including the above 9). 157. In the full-blade gas turbine, heating is performed by heating the outer turbine blade group (19) and the inner turbine blade group (20), which are annularly cast (84) into an assembled structure, with a combustion gas. A combined steam gas turbine engine comprising a device including the blade (79) and driven by the output. 158. A full blade steam gas turbine, comprising:
Each of the outer turbine blade group (19) and the inner turbine blade group (20) formed into an assembled structure by annular casting (84) includes:
A combined steam gas turbine engine comprising: a device driven by the output including a heating blade (79) heated by combustion gas. 159. In the all-blade steam turbine, heating is performed by heating the outer turbine blade group (19) and the inner turbine blade group (20), each of which is annularly cast (84) and assembled, by a combustion gas. A combined steam gas turbine engine comprising a device including the blade (79) and driven by the output. 160. A group of outer turbine blades (19) and an inner turbine blade group (20) which are annularly cast (84) to form an assembled structure in a full blade steam turbine compressor.
And a device driven by the output including a heating blade (79) heated by combustion gas. 161. The magnetic friction power transmission device (14)
The magnetized friction wheel 37a magnetizes the N and S poles of magnetic poles on the left and right sides in the radial direction of a ring-shaped ferromagnetic material, and fixes both sides thereof with a ring-shaped yoke (47). The power transmission surface (31) is extended and fixed to the outer radial direction power transmission surface (31), and the power transmission surface (31) is provided with a friction increasing and durable means (45) in an annular shape. A) a rolling friction magnetic power transmission device (14) as the magnetized friction wheels 37a, 37a, respectively. 162. The magnetic friction power transmission device (14)
The magnetized friction wheel 37b is configured to magnetize the N and S poles of the magnetic poles on the inner diameter side and the outer diameter side of a ring-shaped ferromagnetic material, and
7) is extended from the inner peripheral side of the magnet to the left and right outer diameter power transmission surfaces (31), and a friction increasing endurance means (45) is annularly provided between the yoke and the magnet to the power transmission surface to enlarge the power transmission surface. The outer peripheral surface is provided with low irregularities (40) to form rolling contact magnetic friction power transmission devices (14) as magnetized friction wheels (37b) (37b), respectively. Steam gas turbine combined engine. 163. The magnetic friction power transmitting device (14)
Is provided with friction increasing durability means (45) on a power transmission surface (31) having an outer diameter of a ring-shaped ferromagnetic material,
Low irregularities (40) are provided on the outer peripheral surface thereof, and magnetized friction wheels (39) and (39) are provided, respectively, and bar magnets (33) are provided on the upstream side and the downstream side in the rotational direction. ,
A combined steam gas turbine engine comprising a rolling contact magnetic friction power transmission device (14). 164. The magnetic friction power transmitting device (14)
The magnetized friction wheel 37a magnetizes the N and S poles of magnetic poles on the left and right sides in the radial direction of a ring-shaped ferromagnetic material, and fixes both sides thereof with a ring-shaped yoke (47). The power transmission surface (31) is extended and fixed to the outer radial direction power transmission surface (31), and the power transmission surface (31) is provided with a friction increasing and durable means (45) in an annular shape. ) Are provided, and bar magnets (33) are provided on the upstream and downstream sides in the rotational direction as the magnetized friction wheels 37a, 37a, respectively, and the different poles are converted from attracting magnets to the repelling magnets. A steam-gas turbine combined engine, wherein a rolling contact magnetic friction power transmission device (14) is constituted as possible. 165. The magnetic friction power transmitting device (14)
The magnetized friction wheel 37b is configured to magnetize the N and S poles of the magnetic poles on the inner diameter side and the outer diameter side of a ring-shaped ferromagnetic material, and
7) is extended from the inner peripheral side of the magnet to the left and right outer diameter power transmission surfaces (31), and a friction increasing endurance means (45) is annularly provided between the yoke and the magnet to the power transmission surface to enlarge the power transmission surface. Electromagnets (34) are provided on the upstream and downstream sides in the rotational direction as magnetized friction wheels (37b) and (37b), respectively. A combined steam gas turbine engine wherein a magnetic friction power transmission device (14) of rolling contact is constituted by converting a magnet to be attracted to a repelling magnet with the same pole. 166. The magnetic friction power transmission device (14)
Is provided with friction increasing durability means (45) on a power transmission surface (31) having an outer diameter of a ring-shaped ferromagnetic material,
Low irregularities (40) are provided on the outer peripheral surface thereof, and bar magnets (33) are provided on the upstream and downstream sides in the rotational direction as magnetically-attached friction wheels (39) and (39), respectively. A combined steam gas turbine engine, wherein the same pole is convertible into a repelling magnet to constitute a rolling contact magnetic friction power transmission device (14). 167. The magnetic friction power transmission device.
The inner magnetized friction wheel (38a) magnetizes the N and S poles of the magnetic poles on the left and right sides in the radial direction of a ring-shaped ferromagnetic material, and sandwiches both sides thereof with a ring-shaped yoke (47). And protrudingly fixed to the power transmission surface (31) in the radial direction, and a friction increasing and durable means (45) is annularly provided in a concave portion of the internal diameter between the yokes to expand the power transmission surface. (40) is provided,
An integrated steam gas turbine engine comprising an inner magnetized friction wheel (38a) by rolling contact. 168. The magnetic friction power transmission device (14)
The inner magnetized friction wheel device (49a) magnetizes N and S poles of magnetic poles on the left and right sides in the radial direction of a ring-shaped ferromagnetic material, and sandwiches both sides of the ring-shaped yoke (47). Then, it protrudes and is fixed to the inner diameter direction power transmission surface (31), and a friction increasing endurance means (45) is annularly provided in the inner diameter concave portion between the yokes to enlarge the power transmission surface, and the power transmission surface is low. An inner magnetized friction wheel (38a) is provided by providing the unevenness (40), and the magnetized friction wheel (37a) is provided inside the inner magnetized friction wheel (38a) to constitute an inner magnetized friction wheel device (49a) by rolling contact. A combined steam and gas turbine engine. 169. The magnetic friction power transmission device (14)
The inner magnetized friction wheel device (49a) magnetizes N and S poles of magnetic poles on the left and right sides in the radial direction of a ring-shaped ferromagnetic material, and sandwiches both sides of the ring-shaped yoke (47). Then, it protrudes and is fixed to the inner diameter direction power transmission surface (31), and a friction increasing endurance means (45) is annularly provided in the inner diameter concave portion between the yokes to enlarge the power transmission surface, and the power transmission surface is low. An inner magnetized friction wheel (38a) is formed by providing irregularities (40), and the magnetized friction wheel (37a) is provided inside the inner magnetized friction wheel (38a), and electromagnets (34) are provided upstream and downstream in the rotation direction (35). Wherein the internal combustion friction wheel device (49a) by rolling contact is constituted. 170. The magnetic friction power transmission device (14)
The inner magnetized friction wheel (38b) magnetizes the N and S poles of the magnetic poles on the inner and outer diameter sides of the annular cylindrical ferromagnetic material, and moves the yoke (47) right and left from the outer circumference of the magnet. Internal power transmission surface (3
1), a friction increasing and durable means (45) is annularly provided between the yoke and the magnet up to the power transmission surface, and is expanded and fixed to the entire power transmission surface. ) To form an inner magnetized friction wheel (38b), thereby forming a rolling contact inner magnetized friction wheel (38b). 171. The magnetic friction power transmission device (14)
The inner magnetized friction wheel device (49b) magnetizes the N and S poles of the magnetic poles on the inner and outer diameter sides of the annular cylindrical ferromagnetic material, and moves the yoke (47) from the outer peripheral side of the magnet. A friction increasing and durable means (45) is provided annularly between the yoke and the magnet to the power transmission surface extending to the left and right inner diameter power supply surfaces (31). Low unevenness on the surface (40)
And an inner magnetized friction wheel (38b) is formed, and the magnetized friction wheel (37b) is provided inside the inner magnetized friction wheel (38b) to constitute a rolling contact magnetic friction power transmission device. Turbine united engine. 172. The magnetic friction power transmission device (14)
The inner magnetized friction wheel device (49b) magnetizes the N and S poles of the magnetic poles on the inner and outer diameter sides of the annular cylindrical ferromagnetic material, and moves the yoke (47) from the outer peripheral side of the magnet. A friction increasing and durable means (45) is provided annularly between the yoke and the magnet to the power transmission surface extending to the left and right inner diameter power supply surfaces (31). Low unevenness on the surface (40)
Is provided to form an inner magnetized friction wheel (38b), and the magnetized friction wheel (37b) is provided inside the inner magnetized friction wheel (38b).
5) comprising an electromagnet (34) upstream and downstream of
A combined steam and gas turbine engine comprising a rolling contact magnetic friction power transmission device. 173. The magnetic friction power transmission device (14)
The magnetized friction wheel (37c) is formed by magnetizing N and S poles of magnetic poles on the left and right sides in the radial direction of a plurality of annular cylindrical ferromagnetic materials, alternately arranging them, and forming both sides thereof into annular plate-like shapes. The yoke (47) is alternately sandwiched between the power transmission surfaces (31) so as to protrude from the power transmission surface (31) in the outer diameter direction, and is fixed to the power transmission surface (31). And a magnetic friction power transmission device (14) including a magnetized friction wheel (37c) provided with low irregularities (40) on the outer peripheral surface thereof. 174. The magnetic friction power transmission device (14)
The magnetized friction wheel device (51c) includes a plurality of ring-shaped ferromagnetic materials which are magnetized on the left and right sides in the radial direction of magnetic poles, respectively, and are arranged alternately, and both sides thereof are ring plates. Shaped yoke (4
7) alternately sandwiching them, protruding and fixing to the outer diameter power transmission surface (31), and providing a friction increasing and durable means (45) in the outer diameter concave portion between the yokes in an annular shape and extending to the power transmission surface. A combination of rolling contact magnetic friction power transmission devices (14), each of which is provided with low irregularities (40) on the outer peripheral surface thereof, as magnetized friction wheels 37c, 37c, respectively. . 175. The magnetic friction power transmission device (14)
The magnetized friction wheel device (51c) includes a plurality of ring-shaped ferromagnetic materials which are magnetized on the left and right sides in the radial direction of magnetic poles, respectively, and are arranged alternately, and both sides thereof are ring plates. Shaped yoke (4
7) alternately sandwiching them, protruding and fixing to the outer diameter power transmission surface (31), and providing a friction increasing and durable means (45) in the outer diameter concave portion between the yokes in an annular shape and extending to the power transmission surface. The magnets are provided on the upstream side and the downstream side in the rotational direction as the magnetized friction wheels 37c, 37c, respectively, so that the different poles are repelled by the attracted magnet. A combined steam and gas turbine engine comprising a rolling contact magnetic friction power transmission device (14) that can be converted to a magnet. 176. The magnetic friction power transmitting device (14)
The magnetized friction wheel (37d) magnetizes the N and S poles of the magnetic poles on the inner and outer diameter sides of a plurality of annular ferromagnetic materials, respectively, and connects the yokes (47) to the inside of the magnet. It extends from the peripheral side to the left and right outer diameter power transmission surfaces (31), and is provided with annular friction increasing and durable means (45) between the yoke and the magnet to the power transmission surfaces, and is expanded and fixed to the power transmission surfaces, A combined steam and gas turbine engine, wherein a low irregularity (40) is provided on an outer peripheral surface thereof, and a rolling contact magnetic friction power transmission device (14) can be configured as a magnetized friction wheel (37d). 177. The magnetic friction power transmission device (14)
The magnetized friction wheel device (51d) magnetizes the N and S poles of the magnetic poles on the inner and outer diameter sides of a plurality of annular ferromagnetic materials, respectively, and connects the yokes (47) to the magnets. The inner peripheral side extends to the left and right outer diameter power transmission surfaces (31), and friction increasing and durable means (45) are provided annularly between the yoke and the magnet to the power transmission surfaces, and are expanded and fixed at the power transmission surfaces. , Low irregularities (40) are provided on the outer peripheral surface thereof so that each magnetized friction wheel (37d) (37
d) a rolling contact magnetic friction power transmission device (1)
4) A combined steam gas turbine engine comprising: 178. The magnetic friction power transmission device (14)
The magnetized friction wheel device (51d) magnetizes the N and S poles of the magnetic poles on the inner and outer diameter sides of a plurality of annular ferromagnetic materials, respectively, and connects the yokes (47) to the magnets. The inner peripheral side extends to the left and right outer diameter power transmission surfaces (31), and friction increasing and durable means (45) are provided annularly between the yoke and the magnet to the power transmission surfaces, and are expanded and fixed at the power transmission surfaces. , Low irregularities (40) are provided on the outer peripheral surface thereof so that each magnetized friction wheel (37d) (37
As d), magnets are provided on the upstream side and the downstream side in the rotation direction so that different poles can be converted from magnets to be attracted to magnets that repel the same poles.
4) A combined steam gas turbine engine comprising: 179. The magnetic friction power transmission device (14)
Is a combined steam gas turbine engine using water as cooling means. 180. The magnetic friction power transmission device (14)
The low irregularities (40) of the gears are designed to reduce the meshing height of the gears as much as possible to obtain low irregularities for rolling contact power transmission, and have the same type of flat irregularities (41), helical irregularities (42), 43) A combined steam gas turbine engine using any one of the above (43). 181. A heating blade (7) heated by the steam.
9) A combined steam gas turbine engine wherein annular casting is performed for each blade stage and steam having a supercritical pressure or less is used. 182. The heating blade (7) heated by the steam
9) A combined steam gas turbine engine wherein annular casting is performed for each blade stage, and steam containing superheated steam having a supercritical pressure or less is supplied to turbine blades for use. 183. A heating blade (7) heated by the steam.
9) A steam gas characterized in that annular casting is performed for each blade stage, and steam containing superheated steam having a supercritical pressure or less is supplied to substantially all turbine blades including nozzles, stationary blades, and moving blades for use. Turbine united engine. 184. A heating blade (7) heated by the steam.
9) A combined steam gas turbine engine wherein annular casting is performed for each blade stage, and steam having a supercritical pressure or less is heated to 1000 ° C or less for use. 185. A heating blade (7) heated by the steam.
9) A steam gas turbine wherein annular casting is performed for each blade stage, steam at a supercritical pressure or lower is heated to 1000 ° C. or lower, and supplied to turbine blades in the same manner as a conventional cooling blade. Coalition organization. 186. The heating blade (7) heated by the steam
9) Annular casting is performed for each blade stage, and steam at supercritical pressure or lower is heated to 1000 ° C or lower, and supplied to almost all turbine blades including nozzles, stationary blades, and moving blades in the same manner as conventional cooling blades. A steam gas turbine combined engine characterized by being used as a steam engine. 187. The combined steam gas turbine engine, wherein the heating blade (79) heated by the combustion gas is annularly cast for each blade stage and uses the combustion gas from the combustor / heat exchanger. 188. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage, and the combustion gas from the combustor / heat exchanger is supplied to the turbine blade for use. Steam gas turbine combined engine. 189. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage, and the combustion gas from the combustor / heat exchanger is supplied to substantially all turbines including an injection port, a stationary blade, and a moving blade. A steam gas turbine combined engine characterized by being supplied to blades for use. 190. A combined steam gas turbine engine, wherein the heating blade (79) heated by the combustion gas is annularly cast for each blade stage and combustion gas of a dedicated combustor is used. 191. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage, and the combustion gas of a dedicated combustor is supplied to the turbine blade and used like the conventional cooling blade. A combined steam and gas turbine engine. 192. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage, and the combustion gas of a dedicated combustor is supplied to the nozzle, the stationary blade, and the moving blade in the same manner as the conventional cooling blade. A combined steam gas turbine engine for supplying and using substantially all of the turbine blades including the turbine blade. 193. The heating blade (7) heated by the electricity
9) An integrated steam gas turbine engine wherein annular casting is performed for each blade stage, and turbine blades are heated by electric resistance. 194. The heating blade (7) heated by electricity.
9) An integrated steam gas turbine engine wherein annular casting is performed for each blade stage, and the turbine blades are heated by heat generated by electric resistance. 195. The heating blade (7) heated by the electricity.
9) An integrated steam gas turbine engine wherein annular casting is performed for each blade stage, and substantially all of the turbine blades including the nozzle, the stationary blade, and the moving blade are heated by heat generated by electric resistance. 196. The heating blade (7) heated by the electricity
9) A combined steam gas turbine engine in which an annular casting is performed for each blade stage and the turbine blades are heated by electric resistance in substantially the same manner as a conventional electric cushion. 197. The heating blade (7) heated by the electricity.
9) An integrated steam gas turbine engine in which an annular casting is performed for each blade stage, and the turbine blades are heated by heat generated by electrical resistance in substantially the same manner as a conventional electric cushion. 198. The heating blade (7) heated by electricity.
9) A steam gas turbine, wherein an annular casting is performed for each blade stage, and substantially all turbine blades including nozzles, stationary blades, and moving blades are heated by heat generated by electric resistance in substantially the same manner as a conventional electric cushion. Coalition organization. 199. The heating blade (79) is annularly cast for each blade stage to heat a heating blade (81) for heating the turbine blade, a heating blade (82) for heating the turbine blade, and a nozzle. A combined steam and gas turbine engine comprising: a heating nozzle (83) for heating by electric and steam. 200. The heating blade (79) is annularly cast for each blade stage to heat a turbine blade (81), a heating blade (82) to heat a turbine blade, and a nozzle. A combined steam and gas turbine engine comprising: a heating nozzle (83) for heating by electricity and combustion gas. 201. The heating blade (79) is annularly cast for each blade stage to heat a turbine blade (81), a heating blade (82) for heating a turbine blade, and a nozzle. A steam gas turbine combined engine characterized by heating by steam and combustion gas as a heating nozzle (83). 202. The heating blade (7) heated by the steam
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
A steam engine having a supercritical pressure or less. 203. A heating blade (7) heated by the steam
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
And a steam turbine containing superheated steam having a supercritical pressure or less is supplied to the turbine blades for use. 204. The heating blade (7) heated by the steam
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
A steam turbine including superheated steam having a supercritical pressure or less and supplying the steam to substantially all turbine blades including nozzles, stationary blades, and moving blades for use. 205. The heating blade (7) heated by the steam
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
A steam gas turbine having a supercritical pressure or lower and heated to 1000 ° C. or lower. 206. A heating blade (7) heated by the steam
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
A steam turbine having a supercritical pressure or less, and heating the steam to a temperature of 1000 ° C. or less and supplying the steam to a turbine blade in the same manner as a conventional cooling blade. 207. The heating blade (7) heated by the steam
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
It is characterized in that the steam is heated to 1000 ° C. or less and supplied to almost all the turbine blades including the nozzles, the stationary blades and the moving blades in the same manner as the conventional cooling blades. Steam gas turbine combined engine. 208. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an outer diameter assembly annular portion (8).
5. A combined steam gas turbine engine according to 5), wherein the combustion gas from the combustor / heat exchanger is used in contact with the steam gas turbine. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an outer diameter assembly annular portion (8).
5) A combined steam gas turbine engine characterized in that the combustion gas from the combustor / heat exchanger is supplied to the turbine blades for use by being contacted according to (5). 210. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an outer diameter assembly annular portion (8).
5) A combined steam gas turbine engine wherein the combustion gas from the combustor / heat exchanger is supplied to substantially all of the turbine blades including the nozzles, the stationary blades, and the moving blades in communication with each other according to 5). 211. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an outer diameter assembly annular portion (8).
5) A combined steam gas turbine engine wherein the combustion gas of a dedicated combustor is used in contact with the engine according to 5). 212. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an outer diameter assembly annular portion (8).
5) A combined steam gas turbine engine wherein a combustion gas of a dedicated combustor is supplied to a turbine blade for use in the same manner as a conventional cooling blade. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an outer diameter assembly annular portion (8).
5) A steam gas turbine characterized in that the combustion gas of the dedicated combustor is supplied to almost all of the turbine blades including the nozzles, the stationary blades, and the moving blades in the same manner as the conventional cooling blades. Coalition organization. 214. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
And a turbine blade is heated by electric resistance. 215. The heating blade (7) heated by electricity.
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
A steam gas turbine combined engine, wherein the turbine blades are heated by heat generated by electrical resistance. 216. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
A steam gas turbine combined engine characterized by heating substantially all turbine blades including nozzles, stationary blades, and moving blades by heat generated by electric resistance. 217. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
A steam gas turbine combined engine characterized by heating turbine blades in substantially the same manner as a conventional electric cushion by contacting with an electric cushion. 218. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
A steam gas turbine combined engine characterized in that the turbine blades are heated substantially in the same manner as a conventional electric cushion by heat generated by electric resistance. 219. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an outer diameter assembling annular portion (85)
A steam gas turbine combined engine characterized by heating substantially all turbine blades including nozzles, stationary blades, and moving blades in substantially the same manner as a conventional electric cushion by heat generated by electrical resistance. 220. The heating blade (79) is annularly cast for each blade stage, and the heating blade (81) and the turbine stationary blade are connected by an outer diameter assembly annular portion (85) to heat the turbine blade. A combined steam and gas turbine engine comprising: a heating stationary blade (82) for heating; and a heating nozzle (83) for heating an injection nozzle, which are heated by electricity and steam. 221. The heating blade (79) is annularly cast for each blade stage, and is connected by an outer diameter assembly annular portion (85) to heat the turbine blade and heat the turbine blade (81). A combined steam and gas turbine engine comprising: a heating stationary blade (82) for heating; and a heating nozzle (83) for heating an injection nozzle, which are heated by electricity and combustion gas. 222. The heating blade (79) is annularly cast for each blade stage, and is connected by an outer diameter assembly annular portion (85) to heat the turbine blade and heat the turbine blade (81). A combined steam gas turbine engine comprising: a heating stationary vane (82) for heating; and a heating nozzle (83) for heating an injection nozzle, which are heated by steam and combustion gas. 223. A heating blade (7) heated by the steam.
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
A steam engine having a supercritical pressure or less. 224. A heating blade (7) heated by the steam.
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
And a steam turbine containing superheated steam having a supercritical pressure or less is supplied to the turbine blades for use. 225. The heating blade (7) heated by the steam
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
A steam turbine including superheated steam having a supercritical pressure or less and supplying the steam to substantially all turbine blades including nozzles, stationary blades, and moving blades for use. 226. A heating blade (7) heated by the steam.
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
A steam gas turbine having a supercritical pressure or lower and heated to 1000 ° C. or lower. 227. A heating blade (7) heated by the steam.
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
A steam turbine having a supercritical pressure or less, and heating the steam to a temperature of 1000 ° C. or less and supplying the steam to a turbine blade in the same manner as a conventional cooling blade. 228. A heating blade (7) heated by the steam.
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
It is characterized in that the steam is heated to 1000 ° C. or less and supplied to almost all the turbine blades including the nozzles, the stationary blades and the moving blades in the same manner as the conventional cooling blades. Steam gas turbine combined engine. 229. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an inner diameter annular portion (8).
6. A combined steam gas turbine engine according to 6), wherein the combustion gas from the combustor / heat exchanger is used. 230. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an inner-diameter assembly annular portion (8).
6. A combined steam gas turbine engine according to 6), wherein the combustion gas from the combustor / heat exchanger is supplied to the turbine blades for use. 231. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an inner diameter assembly annular portion (8).
6) A combined steam gas turbine engine wherein the combustion gas from the combustor / heat exchanger is supplied to almost all of the turbine blades including the nozzles, the stationary blades, and the moving blades to be used in accordance with 6). The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an inner diameter assembly annular portion (8).
6. A combined steam gas turbine engine according to 6), wherein the combustion gas of a dedicated combustor is used. 233. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an inner diameter assembly annular portion (8).
6) A combined steam gas turbine engine wherein the combustion gas of a dedicated combustor is supplied to a turbine blade and used in the same manner as a conventional cooling blade. 234. The heating blade (79) heated by the combustion gas is annularly cast for each blade stage to form an inner-diameter assembly annular portion (8).
6) A steam gas turbine in which the combustion gas of a dedicated combustor is supplied to substantially all of the turbine blades, including the nozzles, the stationary blades, and the moving blades, in the same manner as the conventional cooling blades. Coalition organization. 235. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
And a turbine blade is heated by electric resistance. 236. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
A steam gas turbine combined engine, wherein the turbine blades are heated by heat generated by electrical resistance. 237. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
A steam gas turbine combined engine characterized by heating substantially all turbine blades including nozzles, stationary blades, and moving blades by heat generated by electric resistance. 238. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
A steam gas turbine combined engine characterized by heating turbine blades in substantially the same manner as a conventional electric cushion by contacting with an electric cushion. 239. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
A steam gas turbine combined engine characterized in that the turbine blades are heated substantially in the same manner as a conventional electric cushion by heat generated by electric resistance. 240. The heating blade (7) heated by the electricity
9) Casts annularly for each blade stage to form an inner diameter annular portion (86).
A steam gas turbine combined engine characterized by heating substantially all turbine blades including nozzles, stationary blades, and moving blades in substantially the same manner as a conventional electric cushion by heat generated by electrical resistance. 241. The heating blade (79) is annularly cast for each blade stage, and is connected by an inner diameter assembling annular part (86) to heat the turbine blade and heat the turbine blade. A steam gas turbine combined engine characterized by heating by electricity and steam as a heating vane (82) to be heated and a heating nozzle (83) to heat the nozzle. 242. The heating blade (79) is annularly cast for each blade stage, and is connected by an inner diameter assembly annular portion (86) to heat the turbine blade and heat the turbine blade and the turbine stationary blade. A combined steam and gas turbine engine comprising: a heating vane (82) to be heated; and a heating nozzle (83) for heating the nozzle. 243. The heating blade (79) is annularly cast for each blade stage, and is connected by an inner diameter assembly annular portion (86) to heat the turbine blade and heat the turbine stationary blade. A steam gas turbine combined engine characterized by heating by steam and combustion gas as a heating vane (82) for heating and a heating nozzle (83) for heating the nozzle. 244. A steam gas turbine combined engine, wherein the apparatus driven by the output of the all-blade gas turbine is various large, medium and small power generation facilities. 245. An integrated steam gas turbine engine, wherein the apparatus driven by the output of the full blade gas turbine is a facility for supplying various types of heat, electricity and cold heat of large, medium and small sizes. 246. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full blade gas turbine is a facility for supplying various types of heat and electricity. 247. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full blade gas turbine is a variety of large, medium and small vessels. 248. A steam gas turbine combined engine, wherein the apparatus driven by the output of the full-blade gas turbine is various large, medium and small aircraft. 249. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full blade gas turbine is a variety of large, medium and small vehicles. 250. A combined steam gas turbine engine, wherein the apparatus driven by the output of the all-blade gas turbine is a large, medium or small machine. 251. A steam gas turbine combined engine, wherein the apparatus driven by the output of the all-blade gas turbine is a large, medium or small ship. 252. A combined steam gas turbine engine, wherein the apparatus driven by the output of the all-blade gas turbine is a variety of large, medium and small tanks. 253. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade gas turbine is a variety of large, medium and small fighters. 254. A combined steam gas turbine engine, wherein the apparatus driven by the output of the all-blade steam gas turbine is a large, medium or small power generation facility. 255. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam gas turbine is a large, medium and small heat, electricity and cold heat supply facility. 256. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam gas turbine is a large-, medium-, and small-sized heat and electricity supply facility. 257. A combined steam gas turbine engine, wherein a device driven by the output of the full-blade steam gas turbine is a large, medium, or small vessel. 258. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam gas turbine is a variety of large, medium and small aircraft. 259. A steam gas turbine combined engine, wherein a device driven by the output of the full-blade steam gas turbine is a large, medium, or small vehicle. 260. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam gas turbine is a large, medium or small machine. 261. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam gas turbine is a large, medium or small ship. 262. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam gas turbine is a variety of large, medium and small tanks. 263. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam gas turbine is a variety of large, medium and small fighters. 264. A combined steam gas turbine engine, wherein the device driven by the output of the gas turbine is a large, medium or small power generation facility. 265. A steam gas turbine combined engine, wherein the device driven by the output of the gas turbine is a facility for supplying large, medium and small heat, electricity and cold heat. 266. A steam gas turbine combined engine, wherein the apparatus driven by the output of the gas turbine is a facility for supplying various types of heat and electricity of large, medium and small sizes. 267. A combined steam gas turbine engine, wherein the apparatus driven by the output of the gas turbine is a variety of large, medium and small vessels. 268. A combined steam gas turbine engine, wherein the device driven by the output of the gas turbine is various large, medium and small aircraft. 269. A combined steam gas turbine engine, wherein the apparatus driven by the output of the gas turbine is various large, medium and small vehicles. 270. A combined steam gas turbine engine, wherein the apparatus driven by the output of the gas turbine is a large, medium or small machine. 271. A combined steam gas turbine engine, wherein the apparatus driven by the output of the gas turbine is a large, medium or small ship. 272. A combined steam gas turbine engine, wherein the device driven by the output of the gas turbine is a large, medium or small tank. 273. A combined steam gas turbine engine, wherein the device driven by the output of the gas turbine is a variety of large, medium and small fighters. 274. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam turbine is a large, medium or small power generation facility. 275. A combined steam gas turbine engine, wherein the device driven by the output of the full-blade steam turbine is a facility for supplying various types of heat, electricity and cold heat of large, medium and small sizes. 276. A combined steam gas turbine engine, wherein the device driven by the output of the full-blade steam turbine is a large-, medium-, and small-sized heat and electricity supply facility. 277. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam turbine is a variety of large, medium and small vessels. 278. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam turbine is various large, medium and small aircraft. 279. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam turbine is a variety of large, medium and small vehicles. 280. A combined steam gas turbine engine, wherein the device driven by the output of the full-blade steam turbine is a large, medium or small machine. 281. A combined steam gas turbine engine, wherein the apparatus driven by the output of the full-blade steam turbine is a large, medium or small ship. 282. A combined steam gas turbine engine, wherein a device driven by the output of the full-blade steam turbine is a variety of large, medium and small tanks. 283. A combined steam gas turbine engine, wherein a device driven by the output of the full-blade steam turbine is a variety of large, medium and small fighters. 284. A combined steam gas turbine engine, wherein the device driven by the output of the steam turbine is a large, medium or small power generation facility. 285. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam turbine is a facility for supplying various types of heat, electricity and cold heat of large, medium and small sizes. 286. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam turbine is a large and medium and small heat and electricity supply facility. 287. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam turbine is a variety of large, medium and small vessels. 288. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam turbine is various large, medium and small aircraft. 289. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam turbine is a variety of large, medium and small vehicles. 290. A combined steam gas turbine engine, wherein the device driven by the output of the steam turbine is a variety of large, medium and small machines. 291. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam turbine is a large, medium or small ship. 292. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam turbine is a variety of large, medium and small tanks. 293. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam turbine is a large, medium or small fighter. 294. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam gas turbine is a large, medium or small power generation facility. 295. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam gas turbine is a facility for supplying various types of heat, electricity and cold heat of large, medium and small sizes. 296. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam gas turbine is a facility for supplying various types of heat and electricity of large, medium and small sizes. 297. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam gas turbine is a variety of large, medium and small vessels. 298. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam gas turbine is a large, medium or small aircraft. 299. A combined steam gas turbine engine, wherein the device driven by the output of the steam gas turbine is a variety of large, medium and small vehicles. 300. A combined steam gas turbine engine wherein the apparatus driven by the output of the steam gas turbine is a large, medium or small machine. 301. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam gas turbine is a large, medium or small ship. 302. A combined steam gas turbine engine wherein the apparatus driven by the output of the steam gas turbine is a large, medium or small tank. 303. A combined steam gas turbine engine, wherein the apparatus driven by the output of the steam gas turbine is a large, medium or small fighter. 304. The fuel burned by the combined steam gas turbine engine is gasoline, natural gas, propane gas,
Alcohol, methanol, methane, hydrogen, light oil, heavy oil,
A combined steam gas turbine engine wherein any one of pulverized coal is used. 305. The fuel burned by the combined steam gas turbine engine is gasoline, natural gas, propane gas,
Alcohol, methanol, methane, hydrogen, light oil, heavy oil,
A combined steam gas turbine engine comprising two types of pulverized coal. 306. The fuel burned by the combined steam gas turbine engine is gasoline, natural gas, propane gas,
Alcohol, methanol, methane, hydrogen, light oil, heavy oil,
A steam gas turbine combined engine, wherein any one of three types of pulverized coal is used. 307. A combined steam gas turbine engine, wherein the type of fuel burned in the combined steam gas turbine engine is not limited. 308. A combined steam gas turbine engine, wherein the type of the device driven by the output of the combined steam gas turbine engine is not limited. 309. The water used in the combined steam gas turbine engine is characterized by mixing a substance and easily dissolving a pollutant gas such as CO2 into water in order to reduce pollution and prevent global warming. Steam gas turbine combined engine. 310. A water used in the combined steam gas turbine engine is mixed with a chemical substance to easily synthesize and dissolve a pollutant gas such as CO2 into water in order to reduce pollution and prevent global warming. Steam gas turbine combined engine. [311] The water used in the steam gas turbine combined engine is characterized by mixing a substance and mixing and dissolving a pollutant gas such as CO2 into water in order to reduce pollution and prevent global warming. Steam gas turbine combined engine. [312] In order to reduce pollution and prevent global warming, water used in the combined steam gas turbine engine is mixed with a chemical substance to synthesize and dissolve a pollutant gas such as CO2 into water and discharge the water. A combined steam gas turbine engine.