JP2001295611A - Steam/gas combined turbine engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide an internal combustion engine for supplying heat, electricity and cryogenic heat by lowering the fuel fee of the internal combustion engine to one half and eliminating the discharge of pollutant including CO2, so as to prevent global warming and restrict the electricity rate. SOLUTION: An outer wall of a combustor-cum-heat exchanger of a steam/gas combined turbine engine is formed into the spiral water cooling outer wall unit assembly structure including a conducting tube, and is arranged as a honeycomb having multiple small-diameter holes by miniaturing and pressurizing. One or more spiral annular conducting tubes are provided in the assembly, and the fuel which is about four times that of the conventional technology is converted to the superheated steam as much as possible with the same quantity of the compressed air with the conventional one by injecting the maximum quantity of the superheated steam in the atmosphere of non-NOx, superheated steam suction thermal lean burn and high pressure, so as to generate the energy to be supplied to the steam turbine 10 times of the latest combined power plant, and the condensate fixed combustion gas is restricted to 0, and the thermal efficiency of the steam/gas combined turbine engine is raised to 80%, including the cryogenic heat supply at 0 deg.C or lower of the exhaust temperature of the gas turbine.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combined engine of a steam gas turbine (fully rotating engine) aiming at zero harmful exhaust gas such as CO2 and NOx and a heat efficiency of 80%. The outer wall of the heat exchanger may be used as a substantially spiral welded structure water-cooled outer wall heat exchanger, or a spiral water-cooled outer wall unit assembly heat exchanger, or a spiral welded structure water-cooled outer wall unit assembled heat exchanger. Shortened and arranged in a honeycomb shape, inside a spiral annular water pipe or steam pipe,
Install one or more as many as possible to suit the application and increase the heat exchanger heat transfer area. Provision of a fuel vapor supply means on the upstream side, after diluting the fuel in superheated supercritical steam or the like, and performing strong stirring and lean low temperature controlled combustion with air to achieve combustion that prevents the generation of harmful gases such as NOx You. The superheated steam (hereinafter, superheated steam is included in the combustion gas), which is the combustion gas of hydrogen, is obtained by performing the combustion control lean cooling combustion at around 900 ° C. or less in the upper limit atmosphere where NOx of high pressure and high temperature is not generated as much as possible. Maximize, complete combustion in a short time, maximize materials that fix water such as global warming gas (CO2). By increasing the superheated steam injection combustion / heat exchange heat transfer area, fuel combustion is made about four times that of the conventional technology, and heat exchange is performed in a high-pressure atmosphere to reduce the amount of heat energy recovered. The amount of thermal energy recovered is more than 10 times that of the gas turbine waste heat recovery heat exchanger, and the amount of cold heat supplied to the gas turbine exhaust increases as the recovered amount increases. will do. In the process of cooling the superheated steam with the adiabatic expanded combustion gas by the gas turbine that obtains the output from the combustion gas, CO2 is fixed to the condensed water in order and drained, and exhausted as no harmful gas exhaust.
The present invention relates to various steam gas turbine combined engines capable of driving a steam turbine or the like with superheated steam obtained by heat exchange and using the outputs of the respective steam turbines.

[0002]

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

[0003] Further, as a prior application, a gas turbine combustor is improved.
No. 5074, Japanese Patent Application No. 7-335595, Japanese Patent Application No. 8-4
1998, Japanese Patent Application No. 8-80407, Japanese Patent Application No. 8-14
No. 3391, Japanese Patent Application No. 8-204049, Japanese Patent Application No. 8-2
No. 72806, Japanese Patent Application No. 9-106925, Japanese Patent Application No. 9-106
There are 181944, Japanese Patent Application No. 10-134720, Japanese Patent Application No. 10-134721, Japanese Patent Application No. 11-69406, and Japanese Patent Application No. 11-77189. The priority claim application based on the above-mentioned prior application generally includes a heat exchanger including a whole rotor blade and / or a plurality of combustors of a gas turbine being lengthened, and a water-cooled outer wall spirally provided as a high-pressure vessel. An apparatus and method that can simultaneously increase the pressure ratio and the specific output to the maximum without exceeding the turbine heat-resistant limit temperature by being able to convert most of the supplied heat into superheated steam, also serving as an exchanger. Thing.

[0004]

[Problems to be Solved by the Invention] An important thing as an internal combustion engine is its mission to reduce harmful exhaust gas to zero. Then, we change the idea of thermodynamics, which thinks that heat does work, heat does not work, and high temperature is considered to be a factor of reduction of work volume = low work volume, heat efficiency × specific output = pressure ratio × combustion gas mass volume = Speed x mass volume, and Tanigawa Mechanics has been established. In the conventional technology, the higher the temperature, the higher the volume and the greater the work load, but the turbine temperature limit temperature is completely meaningless. Therefore, by using the gas turbine combustor also as a heat exchanger, heat is exchanged as much as possible in the high-pressure and high-temperature combustor atmosphere, the superheated steam heat energy is recovered, and the fuel combustion mass with the same amount of compressed air is reduced. When the heat energy recovery is four times that of the state-of-the-art combined cycle gas turbine and the heat energy recovery is ten times or more that of the waste heat recovery heat exchanger, for example, the initial pressure is 1 kg / cm.
2. With an initial temperature of 0 ° C and a pressure ratio of 60, a calculated air temperature of 600 ° C can be obtained. That is, when the gas turbine inlet temperature is set to 600 ° C., it becomes possible to supply cold heat as the exhaust temperature of 0 ° C.
In addition to being able to use four times the total heat energy of the conventional technology as superheated steam, it is also possible to drive the gas turbine by increasing the pressure ratio easily, increasing the combustion gas mass by four times, increasing the combustion gas volume by two times, and enormous heating steam mass volume. You. When the gas turbine inlet temperature is set to 400 ° C., the supply amount of cold heat increases, and the total heat energy of the supplied fuel + the outside air heat energy is used as the superheated steam heat energy, and the cold heat supply at the outside air temperature of 40 ° C. becomes possible. You. The heat-exchanged superheated steam is supplied to a steam turbine side or the like, and the supply amount is increased to increase the amount of cold heat supplied in the gas turbine exhaust, thereby maximizing the gas turbine output and thermal efficiency, and using adiabatic expanded combustion gas. During the process of cooling the superheated steam, there is a problem that CO2 is fixed to the superheated steam condensate and drained, thereby reducing harmful exhaust gas to zero.

[0005] Thermal efficiency and specific output are important as the performance of the gas turbine cycle. Higher thermal efficiency can be obtained as the pressure ratio is higher. If the thermal efficiency (pressure ratio) is constant, the larger the amount of heat supplied to the cycle, the higher the thermal efficiency. A 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, in order to further cool the district by the gas turbine exhaust without exceeding the heat-resistant limit temperature of the gas turbine, the method of increasing the pressure ratio and the supplied heat (fuel combustion mass) to the limit is to reduce the supplied heat (fuel heat). Most of it is converted to superheated steam and used for gas turbines and steam turbines.
Superheated steam in the combustor / heat exchanger by injection and agitation combustion of as much superheated steam as possible, including supercritical fluid, obtained by exchanging heat as much as possible with the combustor / heat exchanger so that the temperature is below 00 ° C CO2, NOx, etc. are fixedly mixed in
Prepare to get closer to. The superheated steam pressure is reduced to a pressure ratio of 10
Fuel dilution agitation NOx which rises to nearly double and burns
The gas turbine is driven to fix the exhaust CO2 to the condensed water, including cooling the superheated steam with the combustion gas. Exhaust, including keeping the temperature below 0 ° C. Drive of various machines by the output of each of them, including driving of rockets and steam turbines that inject the superheated steam,
It is intended to be used for transporting people or luggage, or for supplying heat, electricity or cold.

[0006] That is, the obstacle to increase the pressure ratio and the specific output of the gas turbine is the fuel calorific value of the supplied calorific value. When the fuel calorific value is converted into superheated steam, it is included in various steam turbines. Because there are as many as possible, combustors and heat exchangers are arranged in a short, high pressure arrangement in a large number of small diameter honeycombs,
One or more water pipes or steam pipes are provided in a spiral ring inside as much as possible according to the application, and the combustion gas is supplied from the inside of the inner diameter to the uppermost stream of the gas turbine, and the heat exchange area with a greatly increased heat transfer area The fuel is also used as a heater, and the fuel is supplied by superheated steam in a high-pressure atmosphere by means of a large number of fuel vapor supply means on the uppermost stream side. Increasing / decreasing the fuel suction amount by using the principle of atomization, including superheated steam injection amount control at around 900 ° C or lower, which is the upper limit temperature at which NOx is not generated when the temperature is lowered, the superheated steam cylinder port moving type or fuel port side movement Superheated steam injection agitation cooling combustion such as supercritical
By heat exchange, the harmful combustion gas water is fixed and the harmful exhaust gas is 0 to NOx-free combustion. We will provide an engine that can increase the pressure ratio and the specific output to the maximum by exchanging, increasing the mass volume of superheated steam and increasing the fuel combustion mass by four times.

[0007] For example, the fuel combustion mass is increased up to about four times that of the prior art up to the stoichiometric air-fuel ratio, and the pressure ratio and the fuel combustion mass are increased to reduce the amount of heat used by the gas turbine in the supplied heat to the zero side. Provides a device that significantly reduces and increases the thermal efficiency and specific power of gas turbines. In the process, the outside air heat energy is also converted to superheated steam, the gas turbine is driven by the combustion gas, the exhaust gas temperature is reduced as much as possible, and the cooling gas is supplied. By superheated steam obtained by heat exchange so as to be as low as possible, drive a steam turbine compressor or a steam turbine, for example, to drive various vehicles, or drive various aircraft, respectively, or It is intended to drive various ships and the like, or to drive various machines.

[0008] 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. Compressed air is used for 100% combustion. Includes 4 times the fuel combustion mass. For other applications that require compressed air, a bypass is provided to deal with heat exchange as much as possible in a high pressure atmosphere. Of the heat quantity supplied, including the outside air temperature, due to the increase in the pressure ratio and the fuel combustion mass due to the increase in the combustion gas volume decrease mass including the decrease in the gas turbine inlet temperature to 400 ° C. The amount of used heat is greatly reduced, and the used combustion gas mass volume is greatly increased by superheated steam by controlled combustion of superheated steam injection and stirring of about 900 ° C. or less. Along with the rise, and a large increase in the ratio output. The use of superheated steam, including supercritical steam conditions, in which the gas turbine is driven by the combustion gas and the steam turbine is driven by the superheated steam, and the pressure is greatly increased to nearly 10 times that of air compression. Exhaust gas is fixed water drainage 0
It is another object of the present invention to greatly increase the total thermal efficiency by about two to three times and to greatly increase the specific output.

A gas turbine combustor may be arranged in a short shape in the form of a large number of small diameter honeycombs, and one or more spiral water pipes may be provided inside the combustor to double as a combustor / heat exchanger having a greatly increased heat transfer area. The higher the pressure ratio, the higher the thermal efficiency of the gas turbine. In fuel combustion of the same calorific value, the higher the pressure ratio, the higher the temperature. In addition, the combustion gas temperature of the combustor / heat exchanger reduces NOx. Heat exchange becomes easier as the temperature increases to around 900 C, which is the upper limit at which no heat is generated. Therefore, including the increase in fuel supply amount by a factor of four with the same amount of compressed air, more than ten times as much heat energy recovery as in the waste heat recovery heat exchanger of the advanced steam / gas turbine combined cycle power generation facility The purpose is to double the thermal efficiency. Furthermore, the heat transfer area of the heat exchanger can be reduced and shortened, so that only the uppermost stream side can be used as fuel vapor supply means. Utilizing the principle of spraying with superheated steam, the fuel is mixed and diluted with suction superheated steam, and lean control combustion and cooling control combustion are made possible by maximizing the amount of superheated steam injection. By high-speed injection stirring combustion, complete combustion is completed in the shortest time and NOx is completely eliminated.

[0010] Heat exchange gas turbine inlet combustion gas temperature 40
At 0 ° C., the combustion gas volume is reduced to approximately の of that of the prior art.
The superheated steam injection and agitated combustion at around ℃ is maximized, and the volume of combustion gas containing superheated steam is greatly increased by lean control combustion after suction-mixing dilution with superheated steam of 4 times or more, and cooling by the increase of superheated steam NOx by controlled combustion
I will make it no burning. Furthermore, the pressure ratio rises due to the decrease in the compressed air temperature and the combustion temperature due to the use of a large amount of water, and CO2 is condensed water fixed wastewater by cooling the superheated steam with the combustion gas.
Conversion of exhaust loss to significant exhaust profits, such as supply of cold heat due to a decrease in gas turbine exhaust temperature, heat exchange cooling of fuel heat generation to the limit, cooling loss converted to cooling profit, and effective use of the heat generation to the limit It is an object of the present invention to provide a super-high-performance and ultra-high-efficiency steam-gas-turbine combined engine, and to minimize the power transmission loss by maximizing the use of a magnetic friction power transmission device.

[0011] Although the prevention of global warming has been loudly shouted, the actual situation is quite 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. So, I want to contribute something to humanity for anyone to think about. It has been almost 55 years since I wanted to provide a fully reciprocating engine and a fully rotating engine to contribute to humanity. What I feel most strongly about in the process is that no one will challenge you, as we have agreed, with some difficulties. In other words, there is acid rain as a natural phenomenon, and in the vicinity of humans, there are only substances obtained by dissolving and mixing substances in water such as drinking water, and CO2 such as algae of underwater plants.
Is consumed and needed. If people gather in the nature of water such as natural phenomena, NOx and CO
It is clear that harmful emissions, such as 2, can be eliminated.

In particular, the internal combustion engine has a complete set of conditions, from high-pressure high-temperature reactions to low-pressure low-temperature reactions of 0 ° C. or less, in addition to reducing NOx and increasing thermal efficiency. In order to finish the complete combustion for a short time,
There is a problem that super-high-speed injection stirring combustion of superheated steam, which is the combustion gas of hydrogen, at a supercritical level or less has the best performance without any disadvantages. Therefore, by maximizing the pressure ratio of the combustor and heat exchanger according to the application and exchanging heat in the atmosphere as high as possible, superheated steam with as much high pressure as possible is injected, stirred and burned, and complete combustion is completed in a short time. And NOx and CO2
Toxic substances such as harmful substances are fixedly mixed with superheated steam or water, and the superheated steam and low-temperature combustion gas are further mixed and stirred by a gas turbine. In addition, a substance that promotes fixation of combustion gas water and harmless water is mixed into the exhaust gas and effluent with no harmful exhaust and no pollution to increase the thermal efficiency to about 80%.

[0013]

[Means for Solving the Problems] 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, the present invention reduces pollutants such as CO2 and NOx and suspended particulate matter to an upper limit temperature of 90% at which NOx is not first generated.
In the process of injecting superheated steam from the fuel steam supply means on the most upstream side in a combustor / heat exchanger with an increased heat transfer area at around 0 ° C or less, the fuel is suction-diluted using the principle of atomization. Then, by superheated steam and agitated lean combustion,
Disperse heat generation and transfer generated heat to superheated steam side to make cooling and combustion control easier, and eliminate superheated steam cylinder opening or fuel Sliding the nozzle side, increasing or decreasing the number of fuel nozzles, controlling the fuel injection amount using the principle of spraying,
By maximizing the volumetric mass of the combustion gas containing a huge amount of superheated steam,
Complete combustion short time end ・ No NOx combustion and only combustion gas generation of CO2.

By using a combustor / heat exchanger to perform combustion and heat exchange in a high pressure atmosphere as much as possible and converting it into superheated steam, the fuel combustion mass with the same amount of compressed air can be reduced. As a technology four times that of the state-of-the-art combined cycle gas turbine, the heat loss of the combustion gas is cooled as much as possible and converted into enormous superheated steam including the outside heat energy, thereby reversing the cooling loss to the cooling profit. Supplying a large amount of superheated steam, including outside heat energy, to a steam turbine or the like, with the heat energy recovery amount including the gas turbine inlet temperature of 400 ° C. or less and the heat energy recovery amount being 10 times or more of that of the conventional gas turbine waste heat recovery heat exchanger. At the same time, it supplies cold heat at an exhaust temperature of 0 ° C or less to reverse exhaust loss to exhaust profit. The superheated steam and the combustion gas are always in contact from high to low temperatures, including low temperatures below the stratosphere, to maintain an environment in which all harmful combustion gases adhere and dissolve, and adhere and dissolve harmful combustion gases sequentially to the condensate of superheated steam. Discharge. By exchanging heat with the exhaust heat exchanger depending on the application, harmful combustion gas adheres to the superheated steam condensate and is dissolved and discharged. In the process of cooling the superheated steam with the combustion gas according to the application, a substance that promotes fixing of harmful combustion gas water and harmless wastewater is mixed into the water supply, etc. to make harmless exhaust and harmless wastewater.

Infinite heat exchange between the compressor and the combustor / heat exchanger maximizes the pressure ratio of the compressor by reducing the temperature of the compressed air to the minimum, and reduces the dilution of the superheated steam injection fuel in the atmosphere as high as possible. Combustion and heat exchange, injection of superheated steam below supercritical as much as possible, complete stirring, complete combustion in a short time, and control combustion at around 900 ° C, which is extremely difficult, with NOx
Increases superheated steam, which is important for water fixation, as no combustion. Depending on the application, the generation of harmful combustion gases other than CO2 can be considered. Water easily dissolves and mixes any substance.However, in order to select a pollutant and dissolve and mix it in water, depending on the application, fix combustion gas water and harmless wastewater to feed water in the process of becoming superheated steam. Mixing chemicals and substances of the promoting substances, polluting substances by high pressure and high temperature chemical reaction or 0 ℃
It is fixed to water and discharged by low-temperature chemical reaction and mixing below the stratosphere and below the stratosphere, and the emission of pollutants approaches zero. The advantage of combustion and heat exchange in the atmosphere of high pressure and high temperature as possible
For example, at an initial pressure of 1 kg / cm2, an initial temperature of 0 ° C, and a pressure ratio of 60,
Since a calculated air temperature of 600 ° C. is obtained, the outside air temperature 30
Considering summertime around ℃, outside air heat energy can be obtained that exceeds the heat recovery of the waste heat recovery heat exchanger of the gas turbine of the advanced steam gas turbine combined cycle power generation equipment. If the supply fuel is further increased by four times, the thermal energy that can be supplied to the steam turbine side will be more than 10 times that of the state-of-the-art power generation equipment gas turbine and waste heat recovery, and the exhaust temperature of the gas turbine will be 0 ° C or less. It is possible to supply cold heat. Therefore, the thermal efficiency of the gas turbine rises inconceivably, enabling a total thermal efficiency of 80% or more.

The combustion gas as the working gas of the prior art gas turbine generally has a very high proportion of air, and contains about 4 times the stoichiometric mixture. That is, a large amount of heat energy is consumed, and about 80% of the compressed air is wasted, and in addition, it is used to reduce the combustion temperature, resulting in a large loss. Spiral welding structure including water cooling outer wall or spiral welding structure water cooling outer wall unit assembly structure, or
As a spiral water-cooled outer wall unit assembling structure, shortening and high pressure are arranged in a large number of small diameter honeycombs, and as many as possible one or more sets of spiral water pipes are provided in the inside to increase the heat exchange heat transfer area. By converting superheated steam by heat exchange, approximately 100% of air compressed for combustion is involved in combustion and made available for effective use. It is easy to increase the pressure and increase the fuel vapor supply means on the most upstream side, and the maximum fuel supply is about four times that of the conventional technology, thereby increasing the volume of combustion gas.

The heat transfer area of the combustor / heat exchanger is greatly increased,
Converting the combustion gas temperature to superheated steam without limit,
Controlled combustion around 900 ° C in an atmosphere where it is difficult to reduce Ox, including supercritical superheated steam injection and agitation combustion, ensures an increase in combustion gas volume mass and no NOx. From the superheated steam injection combustion gas turbine inlet heat-resistant limit temperature to 4 more
Up to 00 ° C. or less, the unit volume is about half that of the prior art, and high-pressure low-temperature combustion gas is supplied from the upstream and inside of the gas turbine. Combustion gas is mixed and discharged into water, stratified atmosphere water is fixed in contact with water, superheated steam and fuel are quadrupled to increase the volume of combustion gas, and waste heat is recovered by an exhaust heat exchanger to produce condensed water. Fix, harmless water and drain. Uses the output of gas turbines and steam turbines for various purposes, including rockets that inject superheated steam such as supercritical heat obtained by heat exchange.

The design items of the combustor / heat exchanger include:
When used for the smallest size, as shown in FIGS. 17 and 18 of the fifth and sixth special embodiments, as a combustor and heat exchanger for a large-diameter one-water-cooled outer-wall water-cooled inner-wall conduit, the diameter of the water-cooled outer wall depends on the inner diameter. In it, as many as possible spiral spiral water pipes and steam pipes are installed and used. In the normal high pressure type shown in FIGS. 1 to 4, since a cylindrical combustor / heat exchanger is provided in a honeycomb shape,
Although an empty space can be created, the empty space may be used as a space type combustor / heat exchanger not shown in the figure. In that case, FIG.
Use a water-cooled external wall combustor and heat exchanger. By this heat exchange, the gas turbine inlet temperature is reduced from the turbine heat-resistant limit temperature or lower to 400 ° C. or lower as much as possible according to the application, and the total compressed air compressed for combustion is brought close to stoichiometric air-fuel ratio combustion, The combustion mass can be increased up to about 4 times, and most of the fuel calorific value is converted to superheated steam, including supercritical steam conditions, a pressure increase of about 5 to 10 times that of air compression, and a pressure increase. A large amount of superheated steam heat energy including external air heat energy is recovered by heat exchange in an atmosphere with a high ratio and supplied to a steam turbine, etc.

Heat exchange in a high-pressure atmosphere, including air cooling in the compressor and quadrupling the fuel combustion mass, enables waste heat recovery of the gas turbine with the same compressed air amount of the advanced steam / gas turbine combined cycle power generation equipment. By using heat energy more than 10 times when recovering with a heat exchanger, the total thermal efficiency is around 80% and the specific output is greatly increased. By driving the gas turbine with the combustion gas, the superheated steam obtained by exchanging heat so that the combustion gas temperature becomes 400 ° C. or less from the turbine heat-resistant limit temperature or less, drives the steam turbine or the steam turbine compressor, etc. The rotating power and thrust rotate propellers, wheels, generators, machines, and the like to drive various aircraft, automobiles, ships, machines, and the like, and depending on the application, thrust of superheated steam exhaust, combustion gas exhaust, or compressed air. Will provide equipment for levitating and propelling various aircraft and ships, including a control device for controlling each other.

Further, when comparing the case where air is compressed and the case where water is compressed, it is much more advantageous to compress water in which water vapor is condensed to about 1/700. In addition to being able to increase the amount of heat (the amount of retained heat energy), if superheated steam is released at a pressure close to 5 to 10 times that of air compression, a large increase in thermal efficiency can be obtained as a large volume and a large speed far exceeding 1700 times. The best way to utilize substantially all of the compressed air for combustion is to convert and use superheated steam with the highest efficiency, including substantially all of the thermal energy of the increased fuel supply. Therefore, in order to obtain an ultra-high performance combustor / heat exchanger, control combustion at around 900 ° C, which does not generate as high pressure and high temperature NOx as possible, and heat exchange to an infinitely low temperature combustion gas are most efficient. In addition to heat exchange, it is best to inject superheated steam, such as supercritical hydrogen, which is the combustion gas of hydrogen, to complete the complete combustion in a short period of time without stirring and to increase the output.

The amount of heat (superheated steam) extracted from the fuel having the same heat value is maximized including the outside air heat energy including the gas turbine inlet temperature of 400 ° C. or less, so that a huge amount of superheated steam can be obtained most efficiently. By maximizing the mass of the combustion gas that drives the gas turbine, minimizing the driving combustion gas calorie by the heat exchange, and driving the gas turbine with the highest thermal efficiency, the combustion gas exhaust gas is cooled at 0 ° C. or less as a low-temperature exhaust calorie, The harmful combustion gas exhaust is fixed to the condensed water and reduced to zero, the amount of thermal energy used in the gas turbine is reduced, and the nitrogen gas is exhausted to reduce the combustion gas exhaust to zero and recover the cold heat by the exhaust heat exchanger. And supply, also used as heat, electricity and cold supply equipment, with exhaust losses reversed to exhaust profits. For other applications that require compressed air, use a bypass and use it instead of a normally used gear unit.
By using the magnetic friction power transmission device of the prior application appropriately or entirely, as a drive device that transmits power most efficiently, including all auxiliary machines, a steam gas turbine combined engine including all blades The maximum thermal efficiency of the cycle is greatly increased by about 2 to 3 times.

[0022]

DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiments and embodiments of the present invention will be described with reference to the drawings. The reference numerals are used to omit duplicate explanations, and the characteristic parts and the parts that are not explained are added and explained sequentially. In addition, some parts are described with numbers in order to specifically and clearly explain the intended and expected aspects of the invention, but are not limited to numbers.
Further, the combustor / heat exchanger 4 used in the present invention is arranged in a short shape in the form of a large number of small diameter honeycombs, and one or more water guide pipes 1 to steam pipes 6 are formed in a spiral ring inside in accordance with as many as possible. To expand the heat transfer area of the heat exchanger and supply the combustion gas from the most upstream side of the gas turbine. FIG.
As shown in FIGS. 4, 13, and 14, the water-cooled outer wall 26 has a spiral welded structure including one or more water guide tubes 1 or a water-cooled outer wall unit 52 assembly structure including a spiral welded structure. As the heat exchanger 4, a relatively large pressure ratio is set, and the fuel vapor supply means 27 is provided at the most upstream side of each of the heat exchangers. Construct a gas turbine that aims to greatly increase the heat exchange speed, configure a steam turbine etc. driven by superheated steam obtained by heat exchange, for example, provide a generator and electric motor not shown in the figure,
It is also used as a heat / electricity / cold heat supply system and as a starting device, and is also used for various purposes such as driving various transportation devices and driving machinery.

Referring to FIG. 1 and FIG. 2, an embodiment of a core portion of a combined blade / steam gas turbine engine will be described. The idea of the whole rotor blade is that when you move a car by hand, you can be very tired if you push it with the brake applied, but the workload is 0, and you can move easily by releasing the brake and pushing. Therefore, if there is a stationary blade in a compressor or a turbine, a large loss of energy will occur.
The displacement rotor blades are connected to the outer shaft device, and the conventional rotor blades are connected to the inner shaft device, and the inner shaft device and the outer shaft device rotating in opposite directions are connected to each other by magnetic friction having a cooling device such as a water pipe 1. The power transmission device 14 couples the two shafts with the most efficient double reversal drive, and at the same time, divides the peripheral speed by approximately half, makes the outer diameter approximately twice, and makes the fluid passage approximately four times, thereby increasing the specific output. And the thermal efficiency is greatly increased. Alternatively, the peripheral speed is made substantially the same as that of the prior art, and the relative speed between the moving blades is made about twice, so that the specific output and the thermal efficiency are greatly increased. Alternatively, the permissible stress is reduced to approximately one-fourth by reducing the peripheral speed by approximately half of that of the prior art.
It allows for a variety of designs (combined use of heat, electricity and cold for business or home use), such as low-cost, quiet, etc., while greatly increasing thermal efficiency. Or, in order to make the exhaust gas 0 of the harmful combustion gas containing CO2, the superheated steam is cooled in the process of adiabatic expansion in the gas turbine by the low-temperature combustion gas, and the harmful combustion gas is fixed to the condensed water. Hazardous exhaust gas is reduced to zero using centrifugal force from the capillary discharge means (57) provided in the outer turbine blade group.

The first embodiment of the core portion of the combined steam gas turbine engine shown in FIG. 1, the embodiment of the steam turbine compressor shown in FIGS. 5 to 8, and the embodiment of the combined steam gas turbine engine shown in FIGS. See and explain. As shown in FIG. 1, air is sucked in as usual from the first stage 16 of the replaced outer compressor blade group at the right end of the full blade compressor, and the inner compressor blade group 17 of the even-numbered stage is sucked.
And the odd-numbered outer compressor blade groups 16 cooperate to efficiently compress the air by all the rotor blades and provide the compressed air 15 to the inner compressor blade group 17 including the inner shaft device. Each of them is cooled by cooling water by means 55, and the cooling water is jetted from water jetting means 56 for direct contact air cooling, and the capillary discharge means 57 provided in the outer compressor blade group 16 including the outer shaft device. The condensed cooling water is discharged using the centrifugal force and the capillary phenomenon to supply compressed air 15 of high pressure and low temperature by air cooling. The high-pressure / low-temperature compressed air 15 is shortened from the outer compressor rotor blade group final stage 16 through the annular outlet 21 through the annular receiving port 22 and the annular compressed air reservoir 8 into a small-diameter multi-honeycomb arrangement. A combustor / heat exchanger 4 in which one or more water guide pipes 1 to steam pipes 6 are provided as many as possible in a helical ring in accordance with the application to increase the heat transfer area.
Supply.

The supplied high-pressure / low-temperature compressed air 15 is supplied to a fuel injection port 60 of the fuel vapor supply means 27 shown in FIG.
The fuel supplied at a maximum of four times that of the prior art is suction-diluted by a large amount of superheated steam including the supercritical gas at the superheated steam cylinder port 59 using the principle of spraying, and diffused into the superheated steam. Then, the mixture is agitated and lean-burned with the air diluted with suction, and the combustion control is completed at a temperature around 900 ° C., which is the upper limit temperature at which NOx is not generated by the injection-stirred cooling combustion.
With very difficult NOx-free combustion in high pressure atmosphere,
Only the combustion gas CO2 succeeds. Combustion is performed including substantially stoichiometric air-fuel ratio combustion, and a needle valve 61 is provided at the center of the tip of the superheated steam cylinder port 59 so that it can be fully opened and closed, and a screw or a reciprocating piston is provided. The combustion temperature is controlled by controlling the flow rate of superheated steam as electric drive control, pneumatic drive control, or hydraulic drive control to set the maximum to 0. Fuel nozzle 6 of fuel vapor supply means 27
The fuel supplied up to 0 times the maximum of four times that of the prior art is rotated or reciprocated by a screw or a reciprocating piston provided in the fuel injection port 60, and a large number of fuel small holes 62 on the inner diameter side are formed. It is opened and closed by the superheated steam cylinder port 59, and the combustion temperature is controlled by controlling the fuel flow rate.

The combustion gas temperature is 800 ° C. at the gas turbine inlet.
From the following, while exchanging heat as much as possible in the combustor / heat exchanger 4 so as to be 400 ° C. or less depending on the application, heat exchange is performed according to the application, and the water cooling outer wall 26 of each of the water guide pipes 1 is used.
Alternatively, the combustion gas 10 is cooled and exchanged by the steam pipe 6,
The combustion gas 10 obtained by Ox-free combustion or the like was rotatably inserted into the annular receiving port 23 from the respective combustor / heat exchanger 4 via the annular combustion gas reservoir 9 and was airtightly maintained. Outer turbine blade group 1 stage 1
9 and the inner turbine blade group 2 stage 20, which are sequentially injected to the downstream side to generate rotational power and to cool the superheated steam 5 by the combustion gas 10 in the process of adiabatic expansion, and to convert CO 2 into condensed water. Is fixed to approach the harmful exhaust gas 0, and the heat exchange by the exhaust heat exchanger 58 further reduces CO to the condensed water.
Fix 2 to make harmful exhaust gas 0. Depending on the application, the exhaust temperature is kept at 0 ° C or less, and CO2 is fixed to the condensed water to make no harmful exhaust gas while maintaining the profit of the exhaust gas.

Reversing the idea of thermodynamics, which considers that heat does work, heat does not work, and high temperature means that unit volume mass is small = unit volume work is reduced. Therefore, thermal efficiency X specific output = pressure ratio X Combustion gas mass volume = velocity X mass volume,
At the same mass, the higher the temperature, the larger the volume and the larger the work, but it is meaningless due to the turbine heat-resistant limit temperature. Therefore, when the gas turbine combustor is also used as a heat exchanger, heat is exchanged as much as possible in a high-pressure and high-temperature atmosphere, and superheated steam heat energy including outside air heat energy is recovered. 4 of the prior art advanced combined cycle gas turbine
Twice as much as the heat energy recovery amount of the waste heat recovery heat exchanger.
It is possible to increase the output of the gas turbine to 0 times or more, to reverse the exhaust loss to the exhaust profit, and to greatly increase the thermal efficiency.
All or most of the supplied heat energy, including the outside air heat energy, is converted into superheated steam 5 to be supplied to the respective combustor / heat exchanger 4.
Of the steam turbine including all the moving blades shown in FIGS. 5 to 8 and FIGS. 9 to 12 through a steam control valve 7 including a steam pipe 6 and a control device. Cars and other vehicles are driven by the output of gas turbines including moving blades. FIG.
8 to the outer turbine moving blade group 1 stage 19 or the inner turbine stationary blade or the prior art stationary blade from the most upstream side of the steam turbine of the steam turbine compressor including all the rotating blades of FIG.
Drives the downstream side sequentially as usual to generate a large rotation output, and uses it as a steam turbine depending on the application, or strongly drives the various compressors in the figure to obtain thrust or pressure gas. .

The superheated steam, which is supplied to the downstream side and becomes wet steam or water droplets, is ejected from the outer turbine blade group 19 to the rear of the outer periphery from the capillary discharge means 57 by centrifugal force to generate thrust, or Capillary discharge means 57 by pressure + gravity
More emissions, enabling a great reduction in exhaust loss such as stratospheric flight,
Drive the steam turbine. Spout the husband's exhaust,
Use to inject air in the front right strongly to the rear left and use it in various applications that require rotational force and levitation propulsion, such as helicopters and jet aircraft, and jet propulsion of various ships, or aircraft And intermediate use of a ship, etc., is used for levitation injection propulsion, or FIG. 9 is provided with a superheated steam reservoir 32 and an injection port 29 to be used also as a rocket for jetting superheated steam, or a propeller or a wheel. Various types of known control for increasing the thermal efficiency, propulsion efficiency and levitation propulsion efficiency by using superheated steam whose pressure is about 5 to 10 times that of conventional air compressors, for use in rotating and driving generators, machines, etc. It is a steam gas turbine combined engine including various moving blades with the equipment.

Another explanation will be given with reference to FIG. The heat transfer area of the combustor / heat exchanger 4 can be easily increased and shortened in the form of a large number of small diameter honeycombs.
As many as one or more can be provided according to the application to facilitate a lightweight high-pressure vessel, and the fuel vapor supply means 27 can be easily added and installed at the most upstream side, up to about four times that of the conventional technology. Easy to increase. A magnetic friction power transmission device 14 is provided on each of the left and right sides of the center, and each is fixed to the inner shaft device, and is provided annularly on the outer periphery.
An outer shaft device, to which the outer turbine blade group one stage 19 is fixed, is rotatably fitted to the outer shaft device, and the two shafts rotating in opposite directions to each other are respectively moved by the magnetic friction power transmission device 14. At the optimum rotational ratio, the final stage 17 of the inner compressor blade group and the second stage 20 of the inner turbine blade group are fixed to the inner shaft device, and thereafter the odd-numbered final stage 16 of the outer compressor blade group of the outer shaft device is fixed.
The outer compressor rotor blade group odd-numbered stage 16 is fixed to the outer compressor blade group, and the inner compressor rotor blade group even-numbered stage 17 is fixed to the inner compressor blade group final stage 17, so that power is transmitted most efficiently. For this purpose, a drive unit including a magnetic friction power transmission device is used to configure an all-blade compressor. The outer turbine blade group odd stage 19 is fixed to the outer turbine blade group first stage 19 of the outer shaft device, and the inner turbine blade group second stage 20 is fixed.
The inner turbine blade group even-numbered stage 20 is alternately fixed to the inner turbine blade group even-number
0 is fixed to the inner shaft device, and the outer turbine blade group odd-numbered final stage 19 is fixed to the outer shaft device, and is rotatably fitted to the inner shaft device so as to be rotatably fitted on the inner shaft device. Configure
The core part of the combined rotor / steam gas turbine engine.

With reference to FIG. 2, a second embodiment of the core portion of the combined engine with all the moving blades and the steam gas turbine added to the bypass will be described. In the prior art, a large amount of heat energy is consumed and wasteful (reversely lowering the combustion temperature) is discharged without using nearly 80% of the compressed air for combustion, resulting in a large loss. Air compressed for combustion is used for combustion.
The compressed air 15 used for purposes other than combustion is provided with a bypass 28 and used separately to increase the specific output to the utmost limit and greatly increase the thermal efficiency. That is, the combustion gas as the working gas of the prior art gas turbine generally has a very high air ratio and contains air that is about four times the stoichiometric air-fuel ratio, so that the compressed air for combustion is used for 100% combustion. Requires that most of the supplied heat be converted to superheated steam. Therefore, the present invention provides a heat exchanger 4 in which the combustor / heat exchanger 4 is shortened and arranged in a small number of honeycombs and one or more spiral water pipes or steam pipes 6 are provided inside as much as possible. In order to increase the area, to easily increase the pressure and to easily increase the supply of fuel vapor, all or most of the supplied heat can be converted to superheated steam, and the water-cooled outer wall 26 has at least one
A spiral welding structure including a plurality of water pipes 1 or more, or
The water-cooled outer wall unit 52 of the spiral water pipe 1 includes an assembly structure including a welding structure, which enables a large increase in the pressure ratio and injection of superheated steam including supercritical fluid, thereby greatly increasing the specific output and increasing the combustion efficiency. Approximately all of the compressed air can be used effectively for combustion. For other uses requiring compressed air, a bypass is provided for separate use. For uses requiring rotational force, the output shaft 12 is provided. By taking out the rotating power, the waste of air compression is completely eliminated and the thermal efficiency is greatly increased.

Another explanation will be given with reference to FIGS. 2 and 5 to 12. Air is sucked in as usual from the replaced outer compressor blade group 1 stage 16 of the rightmost full blade compressor including the bypass 28, and the even-numbered inner compressor blade group 17 and the odd-numbered outer compressor The moving blade group 16 cooperates to efficiently compress the air by all the moving blades, and for other applications requiring compressed air, optimally supplies compressed air from a bypass 28 passage provided appropriately according to the application. The compressed air 15 is cooled by cooling water provided by the cooling means 55 provided on the inner compressor blade group 17 including the inner shaft device, and the cooling water is jetted from the water jetting means 56 for direct contact. The condensed cooling water is discharged from a capillary discharge means 57 provided on the outer shaft device including the outer compressor rotor blade group 16 using centrifugal force and capillary phenomenon. Supply compressed air 15. The high-pressure and low-temperature compressed air 15 is arranged from the outer compressor rotor blade group final stage 16 through the annular outlet 21 to the annular receiving port 22 and the annular compressed air reservoir 8 so as to be pressurized and arranged in a large number of small-diameter honeycombs. A water pipe or steam pipe 6 with a spiral ring inside
Is provided as many as possible in accordance with the application, and is supplied to the combustor / heat exchanger 4 with an increased heat transfer area.

The supplied high-pressure / low-temperature compressed air 15 is supplied from fuel vapor supply means 27 upstream of the respective combustor / heat exchanger 4 in accordance with a command from a known control device (not shown). By using superheated steam, a maximum of about four times the fuel supply compared to the prior art can be supplied, and the short-time dilution-mixing-lean combustion complete combustion + superheated steam injection-stirring cooling combustion can be performed at a stoichiometric air-fuel ratio of 900.
Performs control combustion around ℃, and enables NOx-free combustion in a very difficult high-pressure and high-temperature atmosphere, including heat exchange. Depending on the application, the only harmful combustion gas is CO2. In the combustor / heat exchanger 4 having an enlarged heat exchange heat transfer area, heat exchange is performed as combustion at around 900 ° C. in the combustion control, and heat exchange is performed by the water cooling outer wall 26 and the steam pipe 6 of each of the water guide tubes 1. Cools down and burns NOx and reduces combustion gas temperature.
Gas turbine combustion gas inlet temperature 800 ° C or less or 40
Combustion gas 10 obtained by heat exchange so as to be 0 ° C. or less
Is replaced by a group of annular nozzles 24 rotatably inserted into the annular receiving port 23 from the respective combustor / heat exchanger 4 via the annular combustion gas reservoir 9 and held in an airtight manner. Turbine blade group 1 stage 19 and inner turbine blade group 2 stage 2
0, and sequentially injects to the downstream side to generate rotational force, cools the superheated steam with the combustion gas 10, fixes CO2 in the condensed water to make harmful exhaust gas 0, and the exhaust temperature is 0 ° C depending on the application. Exhaust including the supply of cold heat by the following heat exchange.

Most of the superheated steam 5 obtained by heat exchange so that the gas turbine inlet temperature is 800 ° C. or lower or 400 ° C. or lower is supplied to the respective combustor / heat exchanger 4 depending on the application.
5 to 8 and FIGS. 10 and 1 through the steam control valve 7.
As shown in 1, the superheated steam 5 is supplied to the steam turbine compressor including all the moving blades by the steam pipe 6 to the most upstream side of the steam turbine, and the downstream side is sequentially driven to generate a large torque.
Also used as a steam turbine. The compressor including the entire moving blades is driven by the steam turbine including the entire moving blades to generate thrust or rotational force, and a turboshaft engine, a turboprop engine, and Used as a turbojet engine, turbofan engine, ship levitation propulsion device, etc., with various core parts, various aircraft and various ships. Similarly, in FIG. 9, the core portion of the combined engine of the steam gas turbine including all the moving blades, the superheated steam reservoir 32 and the injection port 29 in which the water pipes 1 are densely provided in a spiral cylindrical shape are connected to the stop valves 13 and 1.
A rocket is constructed by making it possible to separate between the three. Similarly, in FIG. 12, the steam turbine (compressor removed) including all the moving blades of FIGS. 5 to 8 is driven, and the propeller, the wheels, the generator, the machine, and the like are mainly driven by the torque and the core torque. , Used for driving, may use thrust and levitation force at the same time, aim at heat utilization of exhaust, etc., also used as combined heat, electricity and cold heat equipment, and have various known control devices. It is a combined blade and steam gas turbine engine, and is used for many applications as in the seventh embodiment.

Another explanation will be given with reference to FIG. The water pipes 1 are arranged in a short shape in the shape of a large number of small diameter honeycombs, and are spirally annular inside.
And at least one steam pipe 6 as many as possible according to the application, the combustor / heat exchanger 4 is provided. By connecting the inner shaft device, the left and right inner shaft devices,
A two-shaft, to which an outer shaft device is rotatably fitted and externally rotatably fitted with an outer compressor rotor blade group final stage 16 and an outer turbine rotor blade group first stage 19, which are provided in an annular shape. Are connected at the optimum rotational ratio by the magnetic friction power transmission device 14, and the inner compressor rotor blade group final stage 17 and the inner turbine rotor blade group second stage 20 are fixed to the respective inner shaft devices. Thereafter, the odd-numbered stage 16 of the outer compressor blade group and the even-numbered stage 17 of the inner compressor blade group are alternately fixed, and alternately including the one having an enlarged outer diameter as a compressed air bypass used for purposes other than combustion. The outer shaft device is fixed to the first stage 16 of the outer compressor rotor blade group, and the outer shaft device is rotatably fitted to the inner shaft device so as to be rotatably fitted to the inner shaft device. Combined to form a full blade compressor that drives the two shafts most efficiently. It is. Outer turbine blade group 1
The outer turbine blade group odd number stage 19 is fixed to the stage 19,
The even-numbered stage 20 of the inner turbine blade group is alternately fixed to the second stage 20 of the inner turbine blade group, and the even final stage 20 of the inner turbine blade group is fixed to the inner shaft device. The outer turbine blade group odd-numbered final stage 19 is fixed to the outer shaft device, and rotatably fitted to the inner shaft device so as to be rotatably fitted to the outer shaft device. By configuring the turbine, the core part of the combined engine with bypass and all blades and steam gas turbine is configured.

Referring to FIG. 3, a description will be given of a third embodiment of the core portion of the combined steam and gas turbine engine. The difference from the first embodiment of FIG. 1 is that the core of the combined rotor / steam gas turbine engine is the core of the steam gas turbine combined engine.
The replacement blade is reduced to a prior art stationary blade, and the means for discharging the condensed cooling water by direct contact air cooling and the means for discharging the superheated steam condensed water of the capillary discharge means 57 of the respective outer blades are provided. The use of centrifugal force has been converted to the use of dynamic pressure and gravity, and it has just been replaced with conventional compressors and gas turbines. In other respects, in a similar manner, air is normally sucked from the rightmost compressor stationary blade, and the even-stage inner compressor blade group 17 and the odd-numbered stationary blades cooperate to compress the air. The cooling means 55 provided in the inner compressor rotor blade group 17 cools each of them with cooling water, and the cooling water is jetted from the water jetting means 56 for direct contact air cooling. It supplies high-pressure and low-temperature compressed air 15 compressed by air cooling and released using capillary action and dynamic pressure + gravity from the capillary discharge means 57 provided near the lower part.

The high-pressure and low-temperature compressed air 15 is shortened from the inner compressor rotor blade group final stage 17 through the annular outlet 21 to the annular receiving port 22 and the air reservoir 8 into a small-diameter multi-honeycomb arrangement. , And a spiral annular water pipe 1 to a steam pipe 6 therein.
Is supplied to the combustor / heat exchanger 4 provided as many as possible, depending on the application. Mass volume X speed (pressure ratio) works, high temperature is considered to be unit volume mass small = unit volume work decrease, and combustion gas heat energy including outside air heat energy is infinitely reduced by combustor and heat exchanger. Converted into superheated steam and used, and superheated steam containing supercritical fluid, 4 times the fuel of the prior art, suction dilution injection agitation lean combustion complete combustion short-term completion, and NOx non-cooling combustion, a large amount of superheated steam injection Increasing the combustion gas volume mass while halving the combustion gas cooling volume below 800 ° C to 400 ° C, including outside air heat energy (exhaust temperature 0 ° C at 6MPa 600 ° C), and supplying heat energy as much as possible to superheated steam By converting, for example, a gas turbine or a steam turbine with an exhaust temperature of 0 ° C or less and no harmful exhaust gas can be driven. Therefore, the elements from the first embodiment to the third embodiment shown in FIG. 1 are appropriately replaced with each other, and similarly to the first embodiment, for various purposes, for example, for moving a vehicle and for propulsion of a ship or an aircraft, or for power generation. Used for

Referring to FIG. 3 and FIG. 12, which are close to the prior art, a combined steam and gas turbine combined cycle thermal power plant, the case of using it as a state-of-the-art thermal power plant will be described in comparison with the prior art. In the third embodiment using the gas turbine of FIG. 3, when the generator is driven, the combustor / heat exchanger 4 is shortened and arranged in a large number of small-diameter honeycombs, and the spiral annular water pipes 1 to 3 are provided inside. In the heat exchange in a high-pressure and high-temperature atmosphere in which one or more steam pipes 6 are provided to increase the heat exchange area, an air temperature of 600 ° C is obtained at a pressure ratio of 60, a compression ratio of 18, and an outside air temperature of 0 ° C. If the inlet temperature is around 400 ° C, 3
The superheated steam heat energy that can be recovered from the outside air temperature of around 0 ° C also becomes very large.
Up to about four times the fuel combustion of the conventional technology, the heat energy recovered by the conventional gas turbine waste heat recovery heat exchanger,
The heat energy amount is much more than 10 times, and the exhaust profits, which have reversed the exhaust loss due to the significant decrease of the exhaust temperature below 0 ° C, are also incredibly large, including the large supply of heat, electricity and cold heat. Great increase in thermal efficiency.

Furthermore, in addition to obtaining a small and large-output gas turbine with a greatly increased combustion gas mass volume including superheated steam, the amount of heat energy used and a large-output gas turbine using only outside air heat C in steam condensate
O2 is melted and drained, and nitrogen gas exhaust temperature of 0 ° C or less enables the supply of cold heat by converting the exhaust gas profit to zero combustion gas exhaust and exhaust loss. In steam turbines and gas turbines that use all generated superheated steam,
It is possible to reduce the size of an automobile or the like, and the exhaust heat exchanger 58 dissolves and fixes the CO2 of the combustion gas to the condensed water of the superheated steam of the steam turbine exhaust gas and discharges it. Steam turbine exhaust gas can supply relatively hot water 3. As for the comparison of pressure ratios, the use of large amounts of water makes it easier to lower the compressed air temperature, so the pressure ratio can be raised to the limit and thermal efficiency can be increased. That is, the more heat exchanged in an atmosphere having a large pressure ratio, the higher the thermal efficiency of the steam gas turbine combined engine becomes, and the larger the unit mass of combustion gas becomes, the smaller the gas turbine becomes, and the larger the output becomes. The lower the temperature, the higher the thermal efficiency of the gas turbine, and the greater the amount of thermal energy extracted from the same amount of compressed air, the higher the output of the steam turbine. As a result, the overall thermal efficiency can be increased to about 80%.

Referring to FIG. 4, a fourth embodiment of the core portion of the combined steam-gas turbine engine with bypass will be described. The difference from the third embodiment of FIG. 3 is that a bypass is added to the compressor in the core part of the steam gas turbine combined engine of the third embodiment to make it the core part of the combined steam gas turbine combined engine. . Otherwise, as in the third embodiment, the replacement blade is reduced to a stationary blade of the prior art, and the capillary discharge means 57 of each of the blades discharges condensed cooling water by direct contact air cooling. The means for discharging superheated steam condensate has been converted from the use of centrifugal force to the use of dynamic pressure and gravity to form a compressor with bypass and a gas turbine. Similarly, the combustor / heat exchanger 4 is similarly arranged in a short shape in the form of a large number of small-diameter honeycombs, and one or more water guide pipes 1 to steam pipes 6 are provided in a spiral ring inside the combustor / heat exchanger 4 so that the amount of supplied heat is infinite. By converting to superheated steam, the superheated steam injection fuel suction dilution dilution stirring and lean combustion complete combustion including supercritical energy is completed in a short time, the combustion gas unit volume is reduced by half, the NOx is completely cooled, and the combustion gas mass volume including superheated steam is reduced. The gas turbines and steam turbines can be driven while increasing, and the exhaust temperature of the gas turbine is 0 ° C or less and the combustion gas exhaust is 0. Therefore,
The elements from the first embodiment to the fourth embodiment in FIG. 1 are replaced as appropriate, and are used for various purposes, for example, for moving a vehicle and propelling a ship or an aircraft as in the first embodiment. To do.

Referring to FIG. 5, a first embodiment of the all blade / steam turbine compressor will be described. Superheated steam 5 obtained by heat exchange at the core of various steam gas turbine combined engines
The rotor blade steam turbine is driven to generate rotational force, which is used as rotational power by the output shaft 12 at the left end.
Also used as a steam turbine. In addition, the rotating blade is equipped with the full-blade compressor shown in FIG. 5 and rotated to obtain a high compressed air or a high-speed airflow. The rotating force, the thrust and the levitation force are obtained. Therefore, the superheated steam 5 obtained by heat exchange in the core portion is conveyed from the steam control valve 7 to the most upstream side of the all-blade steam turbine by the steam pipe 6 to drive the most upstream side and sequentially downstream. To generate large rotational power, and in the process, condensed water of superheated steam is discharged from the capillary discharge means 57 of the outer turbine bucket group 19, and mutually separated by the magnetic friction power transmission device 14 at the left end. The outer turbine blade group 19 and the outer shaft device, which rotate in opposite directions, are connected with the inner turbine blade group 20 and the inner shaft device at the optimum rotation ratio. Further, the right end compressor-side magnetic friction power transmission device 14 optimally reverses the inner compressor blade group 17 and the inner shaft device also serving as the turbine outer shaft device, and the outer compressor blade group 16 and the outer shaft device. The first embodiment of the all-blade steam turbine and the all-blade steam turbine compressor is constructed by combining them by the ratio.

Referring to FIG. 6, a description will be given of a second embodiment of the all-blade / steam turbine compressor. Superheated steam 5 obtained by heat exchange at the core of various steam gas turbine combined engines is supplied from a center of the right end of the inner shaft device to the upstream side of the all-blade steam turbine by a steam pipe 6, and the all-blade steam The turbine is driven to generate a rotational force, and in the process, the condensed water of the superheated steam is discharged from the capillary discharge means 57 of the outer turbine bucket group 19 and is used as the rotational power by the output shaft 12 at the left end. Also used as all blades / steam turbine. Further, by using the rotating force, the whole blade compressor shown in FIG. 6 is provided and rotated.
It obtains high compressed air or high-speed airflow, and obtains rotational force, thrust, levitation, etc. Therefore, the superheated steam 5 obtained by heat exchange is conveyed from the steam control valve 7 to the most upstream side of the all-blade steam turbine by the steam pipe 6 to drive the most upstream side and sequentially drive the downstream side. The outer turbine rotor blade group 1 generates a large rotational power and rotates in opposite directions by the magnetic friction power transmission device 14 at the left end.
9 and the outer shaft unit, and the inner turbine blade group 20 and the inner shaft unit are combined at an optimum rotation ratio to form a full blade steam turbine. Further, the inner compressor rotor blade group 17 and the inner shaft device, and the outer compressor rotor blade group 16 and the outer shaft device are connected by the right-most compressor-side magnetic friction power transmission device 14 at an optimum counter-rotating rotation ratio. By composing a full-blade compressor,
It is the second embodiment of the all blade steam turbine and the all blade steam turbine compressor.

Referring to FIG. 7, a third embodiment of the steam turbine compressor will be described. At the core of various steam gas turbine combined engines, the superheated steam 5 obtained by heat exchange drives the steam turbine to generate torque, which is used by the output shaft 12 and used as a steam turbine. In addition, the compressor shown in Fig. 7 is rotated by the rotational force to obtain high compressed air or high-speed airflow, and to obtain rotational force, thrust, levitation, and the like. Therefore, the superheated steam 5 obtained by heat exchange is conveyed from the center of the right end of the inner fixed shaft device to the most upstream side of the steam turbine by the steam pipe 6 through the steam control valve 7 to drive the most upstream side. And the downstream side is sequentially driven to generate a large rotational power, and by rotating the outer turbine blade group 19 and the outer shaft device, which are opposite to the usual, the condensed water of the superheated steam 5 is removed by centrifugal force. As in the first and second embodiments of the full-blade gas turbine and the full-blade steam turbine, the fuel is injected outward and rearward to cope with a decrease in exhaust temperature and a decrease in exhaust pressure such as a stratospheric flight, and the mass of the compressed air flow. As the increase, the propulsion force is increased, the outer shaft device is externally pivoted to the inner fixed shaft device on the left end, and the left end of the outer shaft device is used as the output shaft 12 to constitute a steam turbine. The right end of the inner turbine stationary blade shaft and inner fixed shaft device is fixed by a horizontal joint of a casing, and the casing is externally fitted to the inner shaft device also serving as the turbine outer shaft device and the inner compressor blade group 17. Then, the compressor is constituted, and the third of the steam turbine compressor is
An example.

Referring to FIG. 8, a fourth embodiment of the steam turbine compressor will be described. A steam turbine is driven by superheated steam 5 obtained by heat exchange in a core portion of various steam gas turbine combined engines to generate a rotational force and is used by an output shaft 12 to be used as a conventional steam turbine. Use In addition, a compressor is provided on the right side and rotated by the rotational force to obtain high compressed air or high-speed airflow, and to obtain rotational force, thrust and levitation force. Therefore, the superheated steam 5 obtained by the heat exchange is conveyed to the most upstream side of the known steam turbine by the steam pipe 6 from the steam control valve 7 to drive the most upstream side as usual, and sequentially. By driving the downstream side to generate a large rotational power, in the process, the condensed water of the superheated steam is released by dynamic pressure and gravity from the capillary discharge means 57 provided at the lower part of the casing, and the left end of the inner shaft device Is used as an output shaft 12 to constitute a steam turbine that extracts rotational force. That is, a stationary turbine is fixed to a casing that can be disassembled and assembled with a horizontal joint on the outer side of the inner turbine moving blade group 20 and the inner shaft device, and is externally fitted and pivoted to constitute a steam turbine. Similarly, outside the inner compressor rotor blade group 17 and the inner shaft device, a casing to which the stationary vane is fixed is externally fitted and pivoted to form a compressor, which is a fourth embodiment of the steam turbine compressor. .

Referring to FIG. 13, a description will be given of the welding structure of the means for increasing the heat exchange heat transfer area, in which the combustor / heat exchanger 4 is arranged in a small number of honeycombs to reduce the size thereof. )
(C) As shown in (d), the water-cooling outer wall 26 including at least one or more spiral water pipes 1 is formed into a spiral welding structure with a small number of diameters, thereby setting a large pressure ratio and increasing heat transfer. Acceleration of the heat exchange rate due to the increase in the area and easy addition of the fuel vapor supply means 27 at the most upstream side are facilitated, and the core of the entire steam gas turbine engine is formed into a reasonable cylindrical shape. That is, as in the embodiments shown in (a) and (b), the combustor outer box part 25 is provided a little outward in the radial direction of the spirally provided water guide pipe 1, and one or more water guide pipes 1 are pivoted. Direction T-shaped, etc.
Spiral welding makes it possible to greatly increase the heat transfer area of the combustor / heat exchanger 4 as well as the high pressure vessel. Further, as in the embodiment shown in (c), a combustor outer box 25 to a water-cooled outer wall 26 are provided radially outward of the spirally provided water guide tube 1 so that one or more water guide tubes 1 are provided. Axial helical welding makes it possible to increase the heat transfer area of the combustor / heat exchanger 4 at a significantly higher pressure than supercritical steam conditions. Further, as in the embodiment shown in (d), a combustor outer box part 25 is provided substantially at the center in the radial direction of the water guide pipe 1 provided in a spiral shape, and one or more water guide pipes 1 are axially spiraled. It enables the heat exchange heat transfer area of the combustor / heat exchanger 4 to be increased below the supercritical steam condition and at a relatively high pressure ratio.

Referring to FIGS. 13 and 14, the water-cooled outer wall unit 52 of the means for increasing the heat transfer area, which has a small number of combustor / heat exchangers 4 having a large number of small diameters and arranged in a honeycomb shape, will be described. . As shown in FIGS. 14A, 14B and 14C, a water-cooled outer wall unit 52 including at least one or more spiral water pipes 1
Is provided with flanges 53 at both ends, and as a unit that can be assembled, a plurality of water-cooled outer wall units 52 are connected to form a main part of the combustor / heat exchanger 4 that can be significantly increased in pressure and shortened. . That is, as in the embodiments shown in FIGS. 13 and 14 (a), (b), (a), and (b), at least one or more spirally provided water pipes 1 are slightly separated radially outward. A combustor outer box part 25 including a welding structure is provided, and flanges 53 are provided at both ends of the combustor outer part 25. The water pipe 1 is opened in the flange 53, and a water-cooled outer wall unit 52 including the water pipe 1 is provided. To be concatenable.
Further, as in the embodiments shown in (c), (d), and (c), at least one or more spirally provided water pipes 1 includes a welding structure at a position radially outward or substantially at the center in the radial direction. An outer box part 25 is provided, and flanges 53 are provided at both ends thereof.
3 and a water-cooled outer wall unit 52 including the water pipe 1 is configured to be connectable, and a combustor / heat unit having a supercritical steam condition or lower and a relatively high pressure ratio is used. Exchanger 4
The heat exchange heat transfer area can be increased. Therefore, FIG.
The water-cooled outer wall shown in FIG. 14 is used as the inner wall (FIGS. 17 and 18). The water-cooled inner wall 54 is provided inside and cooled from the outside by the water pipe 1.

Referring to FIGS. 15 and 16, the magnetic friction power transmission device 14 will be described. Various power transmission devices including normal speed change and reverse rotation mainly use a gear device. For this reason, in order to require a sliding tooth surface including a large load on the tooth surface, in addition to requiring lubricating oil, friction heat loss is also very large, and transmission equipment for large power including high speed rotation is required. ,
There is a problem that it cannot be used. For this reason, in order to commercialize an all-blade / steam gas turbine combined engine, an ultra-high-speed and large-power transmission device by rolling contact is indispensable. In order to do so, a power transmission device by rolling contact is required, in which the sliding tooth surfaces of the gear device are almost zero. For this reason,
As shown in FIG. 15, a bar magnet 33 or an electromagnet 34 is provided on the upstream and downstream sides in the rotation direction 35 or on the upstream or downstream side in the rotational direction 35, as shown in FIG. Using the strong attractive force of the magnet, for example, FIG.
It is preferable to use the entire magnetic friction power transmission device 14 including various combinations of the magnetized friction wheels 37, 37 and the magnetic friction wheels 39, 39 shown in FIG. That is, by approaching rolling contact,
This is an ultra-high-speed large-power transmission device that reduces frictional heat loss to almost zero, and enables pollution-free water cooling in place of lubricating oil.

Referring to FIG. 16, the magnetic friction power transmission device 14 will be described. Instead of various gears, various magnetized friction wheels 3
7 and 37, and various magnetically attached friction wheels 39, 39, etc., the power transmission surface 31 is provided with a low unevenness 40, for example, a flat unevenness 41 wheel instead of a spur gear, and a boss unevenness 4 instead of a helical gear.
The two wheels are replaced with Yamaba gears, and 43 Yamaba irregularities are provided. 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.

Referring to FIG. 17, a fifth special embodiment having a simple structure and an inexpensive structure at the core of the all-blade steam gas turbine combined engine will be described. The difference from the first embodiment shown in FIG. 1 is that the combustor / heat exchanger 4 which is the core part of the combined rotor blade steam gas turbine engine is a single large-diameter cylindrical hollow combustor / heat exchanger. 4
The water-cooled outer wall in FIGS.
A combustor / heat exchanger in which the water-cooled inner wall 54 of FIG. 18 is provided in a cylindrical hollow portion, and one or more water guide tubes 1 to steam tubes 6 are provided in a helically annular shape inside the hollow portion according to the application. 4
It is a place to use as. Otherwise, the mass-volume X speed (pressure ratio) works similarly, and the high temperature is smaller than the mass per unit mass =
Considering that the unit work volume is reduced, the combustor / heat exchanger 4 converts the combustion gas heat energy including the outside air temperature into infinitely superheated steam, and superheated steam injection fuel suction dilution and stirring including supercritical, lean, Combustion complete combustion short time end and combustion gas volume halved mass doubling NOx no-cooling combustion heat exchange, while increasing combustion gas volume mass including superheated steam, supply heat energy including outside air heat energy to superheated steam without limit By converting, for example, a gas turbine or a steam turbine that is simple and inexpensive and can be driven, the exhaust temperature of the gas turbine is 0 ° C or less, and the combustion gas exhaust is 0. Therefore, the elements from the first embodiment to the fifth special embodiment in FIG. 1 are appropriately replaced with each other to supply various kinds of applications like the first embodiment, for example, supply of heat, electricity, cold heat, and vehicle. Used for moving and propulsion of ships and aircraft.

Referring to FIG. 18, a sixth special embodiment having a simple structure and an inexpensive structure at the core of the combined steam and gas turbine engine will be described. The difference from the fifth special embodiment shown in FIG. 17 is that the replacement blade is reduced to the stationary blade of the prior art by using the core part of the all-blade steam gas turbine combined engine as the core part of the steam gas turbine combined engine. And a conventional compressor and gas turbine. Otherwise, as in the fifth special embodiment, the combustor / heat exchanger 4 is formed as one large-diameter cylindrical hollow combustor / heat exchanger, and the water-cooled outer wall in FIGS. 1
7. A water-cooling inner wall 54 shown in FIG. 18 is provided in a cylindrical hollow portion, and as many as one or more water guide pipes 1 to steam pipes 6 are provided in a helically annular shape therein according to the application. Superheated steam injection including supercritical by combustor / heat exchanger, using mass volume X velocity (pressure ratio) to work, high temperature is considered to be smaller per unit mass per unit volume = reduced work per unit volume Supply heat including outside air heat energy while increasing combustion gas volume mass including superheated steam by fuel suction dilution agitation, lean combustion complete combustion short-term completion, combustion gas unit volume halving unit mass doubling, and NOx non-cooling combustion It converts energy into superheated steam without limit, and makes it possible to drive, for example, gas turbines and steam turbines that are simple and inexpensive,
The exhaust temperature of the gas turbine shall be 0 ° C or less and the exhaust gas of the combustion gas shall be 0. Therefore, the elements from the first embodiment to the sixth special embodiment in FIG. 1 are appropriately replaced with each other to supply various applications such as supply of heat, electricity and cold heat, and movement of the vehicle as in the case of the first embodiment. Used for propulsion of ships and aircraft.

Referring to FIG. 19, fuel vapor supply means 27
Will be described. Since the conventional NOx reduction combustor dilutes the fuel with air, it tends to generate black smoke due to a local high-temperature region or insufficient fuel-deficient air-deficient combustion in the combustion region.
It causes pollution due to the generation of x and suspended particulate matter. Therefore, in order to eliminate the generation of NOx and suspended particulate matter, the present invention injects superheated steam, which is the combustion gas of hydrogen, at the highest possible temperature and injects fuel using the principle of atomization. By diluting and agitating and gasifying, and after a moment's delay, aspirating and diluting the air to agitate and combust with the fuel, the optimal lean combustion with no local high-temperature region in the combustion region is achieved, producing NOx and suspended particulate matter. It's all about nothing. Therefore, in the early stage of combustion such as ignition, priority is given to ignition combustion with the minimum amount of superheated steam injection, and with the rise in combustion ambient temperature, the amount of superheated steam injection is increased to prevent the generation of NOx and suspended particulate matter. To do. In high-pressure and high-temperature atmospheres, use high-pressure and high-temperature superheated steam in accordance with the application. For those used at atmospheric pressure such as boilers, use high-temperature and low-pressure superheated steam as much as possible to generate NOx and suspended particulate matter. Block.

The superheated steam 5 in the superheated steam cylinder opening 59 shown in FIG. 19A is rotated by rotating the needle valve 61 by electric control or the like, thereby rotating the threaded portion to open and close the needle valve 61, thereby obtaining the superheated steam. The amount of superheated steam is increased or decreased by increasing or decreasing the injection amount. The fuel 11 in the fuel vapor supply means 27 is preheated and supplied to the small fuel hole 62 of the fuel injection port 60, and in the process of suction dilution stirring injection into the superheated steam, agitated and lean combustion is performed with the air, and the fuel injection port 60 is electrically driven. By rotating by control, the screw part is rotated to open and close a large number of small holes 62, and the number of small holes is increased / decreased, and the flow rate of fuel is increased / decreased. Therefore, in this case, another cylindrical part for reciprocatingly opening and closing a large number of small fuel holes 62 is provided, and the screw part of the cylindrical part is rotated to reciprocate the cylindrical part to increase or decrease the fuel flow rate. You can In other words, the combustion temperature is maintained at the set value by controlling the flow rate of superheated steam and the fuel flow rate.

The superheated steam 5 in the superheated steam cylinder port 59 in FIG. 19B reciprocates the piston portion of the needle valve 61 by hydraulic or pneumatic control or the like, thereby reciprocating the piston portion to open and close the needle valve 61. Then, the flow rate of superheated steam is increased or decreased by increasing or decreasing the injection amount of superheated steam. The fuel 11 in the fuel vapor supply means 27 is preheated and supplied to the fuel small hole 62 of the fuel nozzle 60, and in the process of suction dilution stirring stirring injection to the superheated steam, agitated and lean burn with the air, and the fuel nozzle 60 By reciprocating the piston part by control or air pressure control, the piston part is reciprocated to open and close a number of fuel small holes 62, and the number of fuel small holes is increased or decreased, and the flow rate of fuel is increased or decreased. . Therefore, in this case, another cylindrical component for reciprocatingly opening and closing a large number of small fuel holes 62 is provided, and the piston of the cylindrical component is reciprocated by hydraulic control or pneumatic control to increase or decrease the fuel flow rate. All right In other words, the combustion temperature is maintained at the set value by controlling the flow rate of superheated steam and the fuel flow rate.

[0053]

According to the present invention, the outer wall of a combustor / heat exchanger is provided with a spiral welding structure or a welding structure including a water pipe as a core part of various steam gas turbine combined engines including all rotor blades. As a helical water-cooled outer wall unit assembling structure, a small-diameter multiple-honeycomb-shaped short arrangement is provided, and as many as one or more helically annular water-conducting pipes or steam pipes are provided therein, so that the core part of the steam-gas-turbine united engine There is a big effect that can make the external shape compact. Furthermore, as a combustor and heat exchanger for the high-pressure vessel with an increased heat transfer area, the fuel vapor supply means is also easily added to the most upstream side up to four times that of the conventional technology, and uses the principle of spraying fuel. It adopts a configuration in which it is diluted with superheated steam and then agitated and burns with air. This has a great effect of reducing NOx and suspended particulate matter to almost zero. In addition, the effect of converting a large part of the supplied heat including the outside air temperature into superheated steam is great, and the exhaust temperature is greatly reduced by reducing the exhaust temperature to 0 ° C or less by setting the inlet temperature of the gas turbine to 400 ° C or less by heat exchange. It has a great effect on profit.

A large rotating power is obtained by the combustion gas and a huge amount of superheated steam obtained by the heat exchange, the cooling water amount of the compressed air for combustion is maximized, the temperature of the compressed air is reduced, and the high pressure and low temperature compression is performed. It has a great effect of getting air.
When the amount of compressed air for combustion is the same as that of the conventional technology, the amount of heat to be supplied is greatly increased up to the stoichiometric air-fuel ratio combustion with a fuel approximately four times as large as that of the conventional gas turbine, and the upper limit is approximately 900 ° C. at which NOx is not generated. The combustion control has the effect of injecting a huge amount of superheated steam at high speed and completes the combustion in a short time. In addition, the effect of maximizing the material that fixes CO2 in water and the best environment from high pressure and high temperature to low pressure and low temperature is achieved. There is
It also has the effect of reducing the emission of combustion gas such as CO2 to zero. Heat exchange also increases the combustion gas mass volume, which has the effect of increasing the specific output. The amount of air compressed for combustion is used for 100% combustion, and superheated steam at a pressure close to the supercritical pressure, which is 5 to 10 times the normal pressure ratio, can be injected at a high speed in large quantities. The controllable effect is large, NOx is completely non-cooled combustion, and the harmful exhaust gas is limited to CO2.
It has a great effect on a large increase in thermal efficiency.

The infinite cooling of the gas turbine pressure ratio by heat exchange combustion gas has the effect of increasing the heat efficiency of the gas turbine to the limit by raising it to the limit. Furthermore, to exchange heat with the pressure ratio raised to the limit, maximize the amount of superheated steam energy including supercritical steam conditions, minimize the exhaust temperature, and increase the total specific output and thermal efficiency to the limit There is an effect that can be done. Furthermore, in order to exchange heat in a state where the pressure ratio is raised to the limit, the combustion gas gas turbine inlet temperature is set to 400 ° C. or less, the heat consumption of the gas turbine by a large amount of superheated steam injection is minimized, and the combustion gas mass volume is maximized. It has the effect of increasing the thermal efficiency to the limit. Furthermore, the use of combustion gas that has undergone heat exchange as much as possible with the pressure ratio raised to the limit has the effect of significantly reducing the exhaust temperature of the gas turbine to 0 ° C or less, and allowing thermal energy to be used to the limit. . or,
By fully developing and using various magnetic friction power transmission devices, the friction loss of the various power transmission devices of the prior art is greatly reduced, and there is the effect of further increasing the thermal efficiency.
Therefore, it can be used as a variety of transportation equipment and co-supply equipment of heat, electricity and cold, etc., and has a great effect to reduce CO2 on a global scale.

The most significant feature of the present invention is that since the gas turbine and the steam turbine can be separated, the thermal efficiency of the most advanced thermal power generation equipment, which is most commonly spread around the world, can be maximized. In other words, in a state-of-the-art steam / gas turbine combined cycle power generation facility, the waste heat of the gas turbine is recovered and the steam turbine cycle is driven, so the amount of heat supplied to the steam turbine cycle becomes small and the exhaust loss increases. Therefore, in order to perform combustion and heat exchange in a high pressure atmosphere as much as possible as a combustor / heat exchanger, the present invention employs, for example, an outside air temperature of 0 ° C., a pressure ratio of 60 and an air temperature of 600 ° C.
In addition to recovering a large amount of outside air heat energy by setting the outside air temperature to about 30 ° C., the supply heat energy by fuel combustion with the same amount of compressed air is also quadrupled. In order to significantly increase the temperature before and after, the superheated steam heat energy supplied to the steam turbine cycle is increased by 10 times or more, and the exhaust temperature is significantly reduced to 0 ° C or less.
Using the exhaust loss as the exhaust profit, the amount of heat used by the gas turbine is minimized, and the overall thermal efficiency is greatly increased to around 80%.

[Brief description of the drawings]

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

FIG. 19 is a partial cross-sectional view showing a fuel vapor supply means of the combustor / heat exchanger.

[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 52: water cooling outer wall unit 53: flange 54: water cooling inner wall
55: cooling means 56: water injection means 57: capillary discharge means 58:
Exhaust heat exchanger 59: Superheated steam cylinder mouth 60: Fuel nozzle 61: Needle valve 62: Fuel small hole

──────────────────────────────────────────────────続 き Continued on the front page (51) Int.Cl. ⁷ Identification symbol FI Theme coat ゛ (Reference) F02C 3/30 F02C 7/16 Z 7/16 7/224 7/224 F04D 19/02 F04D 19/02 F22B 1/18 R F22B 1/18 F23R 3/28 A F23R 3/28 B60K 9/00 C

Claims (171)

[Claims] 1. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure and one or more spiral annular water pipes are provided therein, and the combustor / heat exchanger has a small diameter and a large number of honeycombs. A combined steam gas turbine engine having an all-blade compressor for supplying heat to a heat exchanger and an all-blade gas turbine for obtaining output from combustion gas. 2. A water-cooled outer wall is formed as a spiral welded structural unit assembly structure, and one or more spiral annular water pipes are provided therein,
A combustor / heat exchanger, which is arranged in a short shape in the form of a large number of small-diameter honeycombs, an all-blade compressor that supplies compressed air to the combustor / heat exchanger, and a whole-blade gas turbine that obtains output using combustion gas. Steam gas turbine united engine. 3. A spiral water-cooled outer wall unit assembling structure,
A combustor / heat exchanger in which at least one water guide pipe is provided in a helical ring inside and shortened and arranged in a small number of honeycombs, and a full blade compressor for supplying compressed air to the combustor / heat exchanger, A combined steam gas turbine engine having a full blade gas turbine that obtains output with combustion gas. 4. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure, one or more water guide tubes are provided in a spiral annular shape inside, and the combustor / heat exchanger is shortened and arranged in a large number of small diameter honeycombs. A combined steam and gas turbine engine having a compressor for supplying heat to a heat exchanger and a gas turbine for obtaining output from combustion gas. 5. A water-cooled outer wall is formed as a spiral welding unit assembly structure, and one or more water guide tubes are provided in a spiral ring inside thereof.
A combined steam / gas turbine engine having a combustor / heat exchanger, which is shortened and arranged in the shape of a large number of small-diameter honeycombs, a compressor that supplies compressed air to the combustor / heat exchanger, and a gas turbine that obtains output using combustion gas. . 6. A spiral water-cooled outer wall unit assembly structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside and are arranged in a short shape in a small number of honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A combined gas and gas turbine engine having a gas turbine for obtaining output. 7. The combined steam and gas turbine engine according to claim 4, wherein one of the compressor and the gas turbine is a full moving blade. 8. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welded structure and one or more spiral annular water pipes are provided therein, and the combustor / heat exchanger is arranged in a short shape in a small-diameter multi-honeycomb form. Blade compressor that supplies the heat and heat to the heat exchanger. A combined steam gas turbine engine having an all-blade steam turbine for obtaining output. 9. A water-cooled outer wall is formed as a spiral welding structure unit assembling structure, and one or more spiral annular water pipes are provided therein,
A combustor / heat exchanger which is arranged in a short shape in the form of a large number of small diameter honeycombs, a full blade compressor for supplying compressed air to the combustor / heat exchanger, a full blade gas turbine which obtains output with combustion gas,
A combined steam gas turbine engine comprising: a full-rotor blade steam turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than a turbine heat-resistant limit temperature. 10. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided as a spiral water-cooled outer wall unit assembling structure and are arranged in a small number of small honeycombs, and the compressed air is burned. Rotor blade compressor to supply heat to the heat exchanger and heat exchanger, and all blade rotor gas turbine that obtains output with combustion gas, and superheated steam obtained by performing heat exchange so that the combustion gas temperature is lower than the turbine heat resistance limit temperature. A combined steam gas turbine engine having an all-blade steam turbine for obtaining output. 11. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and arranged in a small number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas A combined steam gas turbine engine having a gas turbine for obtaining output, and a steam turbine for obtaining output with superheated steam obtained by performing heat exchange so that a combustion gas temperature is equal to or lower than a turbine heat resistant limit temperature. 12. A combustor / heat exchanger having a water-cooled outer wall formed as a spiral welded unit assembling structure and one or more spirally-arranged water pipes provided inside and shortened and arranged in a small-diameter multiple-honeycomb form, and compressed air. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam gas turbine engine having a steam turbine. 13. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided inside as a spiral water-cooled outer wall unit assembling structure, and are arranged in a short shape in a plurality of small diameter honeycombs; A compressor that supplies heat to the heat exchanger and a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. A steam gas turbine combined engine having 14. A compressor, a gas turbine, or a steam turbine according to claim 11, wherein
The following is a combined steam gas turbine engine with all blades. 15. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine for obtaining an output, an orifice (29) for obtaining an output with superheated steam obtained by performing heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat-resistant limit temperature, and a superheated steam reservoir for supplying the superheated steam to the orifice ( 30) a combined steam gas turbine engine having: 16. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welding structure unit assembling structure and one or more water pipes are provided inside in a spiral ring shape and are arranged in a small-diameter multiple-honeycomb shape, and compressed air. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature. A combined steam gas turbine engine having an injection port (29) and a superheated steam reservoir (30) for supplying superheated steam to the injection port. 17. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided inside as a spiral water-cooled outer wall unit assembly structure, and are arranged in a small-diameter multi-honey structure, and the compressed air is burned. A compressor for supplying heat to the heat exchanger, a gas turbine for obtaining output from combustion gas, and an injection port for obtaining output from superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature (29 ) And a superheated steam reservoir (30) for supplying superheated steam to the injection port. 18. The combined steam and gas turbine engine according to claim 15, wherein at least one of the compressor and the gas turbine are all blades. 19. The method according to claim 15, wherein the compressor, gas turbine, combustor and heat exchanger and the superheated steam reservoir (30) are provided with stop valves (13), (13) and (1).
3) A combined steam gas turbine engine wherein the two are separated from each other. 20. A combined steam gas turbine engine wherein the superheated steam reservoir (30) is formed by densely packing a water guide pipe (1) in a cylindrical spiral shape with a honeycomb structure. 21. A steam-gas turbine combined engine, wherein the superheated steam reservoir (30) is densely packed in a cylindrical spiral annular shape including a welded water pipe (1) in a honeycomb shape. 22. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and arranged in a small number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas A steam turbine that combines a gas turbine that obtains output and a steam turbine that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. organ. 23. A combustor / heat exchanger having a water-cooled outer wall formed as a spiral welded unit assembling structure, one or more spirally-circulated water pipes provided inside and shortened and arranged in a small-diameter multi-honey structure, and compressed air. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine comprising a steam turbine and a single shaft. 24. A combustor / heat exchanger in which at least one water pipe is provided in a spiral ring shape as a spiral water-cooled outer wall unit assembling structure and which is arranged in a small number of small diameter honeycombs, and the compressed air is burned. A compressor that supplies heat to the heat exchanger and a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A steam gas turbine united engine provided on a single shaft. 25. The method according to claim 22, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 26. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and arranged in a small number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas A gas turbine that obtains output, a steam turbine compressor that obtains output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature,
An apparatus for levitating and moving an aircraft body. 27. A combustor / heat exchanger having a water-cooled outer wall formed as a unitary structure of a helical welding structure unit and having at least one helically annular water guide tube therein, and arranged in a small-diameter multi-honey-comb shape, and a compressed air. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature. A combined steam and gas turbine engine having a steam turbine compressor and a device for levitating and moving an aircraft body by the thrust of the steam turbine compressor. 28. As a spiral water-cooled outer wall unit assembly structure, a combustor / heat exchanger in which one or more spirally-arranged water pipes are provided inside and short-circuited in a small-diameter multi-honey structure, and the compressed air is burned. Compressor that supplies heat to a heat exchanger and a gas turbine that obtains output with combustion gas, and steam turbine compression that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature And a device for levitating and moving the aircraft body by the thrust of the husband and the wife. 29. The combined steam and gas turbine engine according to claim 26, wherein at least three of the compressor, the steam turbine compressor, and the gas turbine are all blades. 30. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and arranged in a small number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas A gas turbine that obtains output, a steam turbine that obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature, a steam turbine compressor that obtains output with the superheated steam, A combined steam and gas turbine engine having a device for levitating and moving an aircraft body with the use of husband and wife. 31. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and one or more spirally-circulated water pipes are provided inside thereof, and the combustor / heat exchanger is shortened and arranged in a small-diameter multi-honey structure. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam gas turbine engine having a steam turbine, a steam turbine compressor that obtains an output with the superheated steam, and a device for levitating and moving the aircraft body by the thrust of the steam turbine and the compressor. 32. As a helical water-cooled outer wall unit assembly structure, a combustor / heat exchanger in which one or more helically annular water guide pipes are provided inside, and which are arranged in a short shape in a small number of honeycombs, and the compressed air is burned. A compressor that supplies heat to the heat exchanger, a gas turbine that obtains output with combustion gas, and a steam turbine that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A combined steam and gas turbine engine comprising: a steam turbine compressor that obtains an output with the superheated steam; and a device that levitates and moves the aircraft body by the thrust of the steam turbine compressor. 33. The combined steam / gas turbine engine according to claim 30, wherein at least four of the compressor, the steam turbine, the steam turbine compressor, and the gas turbine are all blades. 34. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine that obtains output, a steam turbine compressor that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and the ship is levitated and moved by the force of each of them. Steam turbine combined engine having a device for 35. A combustor / heat exchanger in which a water-cooled outer wall is formed as a unitary structure of a welding structure having a spiral shape, and one or more water pipes are provided in a spiral ring shape inside thereof, and the combustor / heat exchanger is shortened and arranged in a small-diameter multi-honey structure. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine having a steam turbine compressor and a device for levitating and moving a ship by their respective forces. 36. As a helical water-cooled outer wall unit assembly structure, one or more helical annular water pipes are provided inside, and a combustor / heat exchanger in which a plurality of small-diameter, honeycomb-shaped tubes are arranged and shortened. Compressor that supplies heat to a heat exchanger and a gas turbine that obtains output with combustion gas, and steam turbine compression that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature And a device for levitating and moving a ship by the power of the couple. 37. The combined steam and gas turbine engine according to claim 34, wherein at least three of the compressor, the steam turbine compressor, and the gas turbine are all blades. 38. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and arranged in a small number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas A gas turbine that obtains output, a steam turbine that obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat resistant limit temperature, a steam turbine compressor that obtains output with the superheated steam, A combined steam and gas turbine engine having a device for levitating and moving a ship under the influence of husband and wife. 39. A combustor / heat exchanger having a water-cooled outer wall formed as a spiral welded unit assembly structure and one or more spirally-circulated water pipes provided inside and shortened and arranged in a small-diameter multi-honey structure, and compressed air. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam gas turbine engine having a steam turbine, a steam turbine compressor that obtains an output with the superheated steam, and a device for levitating and moving a ship by the respective forces. 40. A combustor / heat exchanger in which one or more spiral water pipes are provided inside as a spiral water-cooled outer wall unit assembling structure, and the combustor / heat exchanger is arranged in a short shape in a number of small diameter honeycombs, and the compressed air is burned. A compressor that supplies heat to the heat exchanger and a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A steam gas turbine combined engine comprising: a steam turbine compressor that obtains an output using the superheated steam; and a device that levitates and moves a ship by the power of the steam turbine compressor. 41. The combined steam and gas turbine engine according to claim 38, wherein at least four of the compressor, the steam turbine, the steam turbine compressor, and the gas turbine are all blades. 42. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and arranged in a small number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas A gas turbine that obtains output, a steam turbine that obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature becomes equal to or lower than the turbine heat resistant limit temperature, and a steam turbine compressor that obtains output with the superheated steam. A combined steam gas turbine engine having a device for lifting and moving an airframe by rotating a propeller by an output and a thrust of a husband. 43. A combustor / heat exchanger in which a water-cooled outer wall is formed as a unitary structure of a welding structure in a spiral shape, and one or more water guide tubes are provided in a spiral ring shape inside, and are arranged in a short shape in a honeycomb shape with a plurality of small diameters. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine comprising: a steam turbine; a steam turbine compressor that obtains an output from the superheated steam; and a device for rotating a propeller to levitate and move the fuselage by using the output and thrust of each. 44. As a helical water-cooled outer wall unit assembly structure, one or more helically annular water pipes are provided inside, and a combustor / heat exchanger in which a plurality of small-diameter honeycomb structures are arranged, and the compressed air is burned. A compressor that supplies heat to the heat exchanger and a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. A steam turbine combined engine having a steam turbine compressor for obtaining an output with the superheated steam, and a device for rotating a propeller to levitate and move the airframe by using the output and the thrust of each of them. 45. The combined steam and gas turbine engine according to claim 42, wherein at least four of the compressor, the steam turbine, the steam turbine compressor, and the gas turbine are all blades. 46. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and arranged in a small number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas A gas turbine that obtains output, a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature, and a fuselage that rotates a propeller with the output and thrust of each And a device for levitating the gas. 47. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure, one or more water pipes are provided in a spiral annular shape inside, and a small-diameter multiple-honeycomb is arranged and shortened. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine having a steam turbine and a device for rotating a propeller to levitate and move the airframe by using the output and thrust of each of them. 48. As a helical water-cooled outer wall unit assembly structure, a combustor / heat exchanger in which one or more helically annular water pipes are provided inside, and which are arranged in a short shape in a number of small diameter honeycombs, and the compressed air is burned. A compressor that supplies heat to the heat exchanger and a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. And a device for rotating the propeller to levitate and move the fuselage by the output and thrust of the husband and wife. 49. The method according to claim 46, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 50. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and arranged in a small number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas A gas turbine that obtains output, a steam turbine compressor that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. And a device for causing the combined gas and gas turbine to have an engine. 51. A combustor / heat exchanger having a water-cooled outer wall formed as a unitary structure of a helical welding structure and having at least one helically annular water-conducting pipe therein and arranged in a small-diameter multiple-honeycomb shape, and a compressed air. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam gas turbine engine having a steam turbine compressor and a device for levitating and moving the airframe by the output and thrust of each of them. 52. As a spiral water-cooled outer wall unit assembly structure, a combustor / heat exchanger in which one or more spirally-arranged water pipes are provided inside and shortened and arranged in a honeycomb shape with a small diameter, and the compressed air is burned. Compressor that supplies heat to the heat exchanger and a gas turbine that obtains output with combustion gas, and steam turbine compression that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature A combined steam and gas turbine engine having a power unit and a device for levitating and moving the vehicle using the power and thrust of each of the power units. 53. The combined steam and gas turbine engine according to claim 50, wherein at least three of the compressor, the steam turbine compressor, and the gas turbine are all blades. 54. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine that obtains output, a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature, and a hull that rotates a propeller by using the output and thrust of each. And a device for levitating and moving the steam turbine. 55. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure and one or more spirally-circulated water pipes are provided inside thereof, and the combustor / heat exchanger is shortened and arranged in a small-diameter multi-honey structure. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine having a steam turbine and a device for rotating a propeller to levitate and move a hull by the output and thrust of each of them. 56. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided as a spiral water-cooled outer wall unit assembling structure and which are arranged in a short shape in a plurality of small diameter honeycombs, and the compressed air is burned. A compressor that supplies heat to the heat exchanger and a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. And a device for rotating a propeller to levitate and move the hull by the output and thrust of the husband and wife. 57. The method according to claim 54, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 58. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine that obtains output, a steam turbine compressor that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. And a device for causing the combined gas and gas turbine to have an engine. 59. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welding unit assembly structure, one or more water pipes are provided in a spiral annular shape inside, and are arranged to be short and arranged in a small number of honeycombs; And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine having a steam turbine compressor and a device for levitating and moving a hull by the output and thrust of each. 60. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided inside as a spiral water-cooled outer wall unit assembling structure, and the combustor / heat exchanger is arranged in a small-diameter multiple honeycomb shape, and the compressed air is burned. Compressor that supplies heat to the heat exchanger and a gas turbine that obtains output with combustion gas, and steam turbine compression that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature And a device for lifting and moving the hull by the output and thrust of the husband and wife. 61. A combined steam gas turbine engine according to claim 58, wherein at least three of the compressor, the steam turbine compressor, and the gas turbine are all blades. 62. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine that obtains output, a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. Steam turbine combined engine having a power transmission device. 63. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine that obtains output, a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature. And a power transmission device for generating and charging the output and rotating the wheels by an electric motor so as to be movable. 64. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure and one or more water pipes are provided in a spiral ring inside, and are arranged in a small-diameter multiple-honeycomb shape, and compressed air is provided. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine having a steam turbine and a power transmission device for rotating and moving wheels according to outputs of the steam turbine and the steam turbine. 65. A combustor / heat exchanger in which a water-cooled outer wall is formed as a unitary structure of a helical welding structure and one or more helical annular water pipes are provided therein, and the unit is compactly arranged in a small-diameter multi-honey structure, and compressed air. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A steam gas having a steam turbine and a power transmission device for rotating and moving wheels by means of their respective outputs, and for generating and charging the output to rotate the wheels with an electric motor so as to be movable. Turbine united engine. 66. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided internally as a spiral water-cooled outer wall unit assembly structure and arranged in a small-diameter multi-honey structure, and the compressed air is burned. A compressor that supplies heat to the heat exchanger and a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. And a power transmission device for rotating and moving wheels according to the outputs of the steam and gas turbine. 67. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided inside as a spiral water-cooled outer wall unit assembly structure, and are arranged in a small-diameter multi-honey structure, and the compressed air is burned. A compressor for supplying heat to a heat exchanger and a heat exchanger, a steam gas turbine for obtaining output using superheated steam obtained by exchanging heat so that a combustion gas and a combustion gas temperature are equal to or lower than a turbine heat-resistant limit temperature, and an output using the superheated steam. With the steam turbine that obtains and the output of each husband and wife, the wheels are rotated and movable,
A power transmission device for generating and charging the output and rotating the wheels by an electric motor so as to be movable. 68. The method according to claim 62, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 69. The method according to claim 62, wherein the power transmission surface (31) of the rail (54) and the wheel (55) is provided with low irregularities (40), respectively. A combined steam gas turbine engine wherein a bar magnet (33) or an electromagnet (34) is provided between the front and rear rails (54) in the traveling direction to apply a suction force. 70. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine that obtains output, a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature, and a propeller is rotated to move the hull by the output of each. And a device for causing the combined gas and gas turbine to have an engine. 71. A combustor / heat exchanger in which a water-cooled outer wall is formed as a unitary structure of a helical welding structure and one or more helically annular water pipes are provided therein, and the combustor / heat exchanger is shortened and arranged in a small-diameter multi-honey structure. And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. An integrated steam gas turbine engine having a steam turbine and a device for rotating a propeller by rotating the propeller according to the output of the steam turbine. 72. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided internally as a spiral water-cooled outer wall unit assembly structure, and are arranged in a small-diameter multi-honey structure, and the compressed air is burned. A compressor that supplies heat to the heat exchanger and a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. And a device for moving a hull by rotating a propeller according to the outputs of the husband and wife. 73. The method according to claim 70, wherein any one of a compressor, a steam turbine, and a gas turbine is selected.
The following is a combined steam gas turbine engine with all blades. 74. The combined steam and gas turbine engine according to claim 70, wherein an exhaust orifice containing the superheated steam is opened at the bottom of the ship. 75. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine that obtains output, a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and rotates the machine to work according to the output of each. And a combined apparatus for a steam gas turbine. 76. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welded unit assembling structure and one or more water pipes are provided in a spiral annular shape inside thereof, and the combustor / heat exchanger is shortened and arranged in a small number of honeycombs; And a gas turbine that obtains output with combustion gas, and obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam gas turbine engine having a steam turbine and a device for rotating a machine to perform work according to the output of the steam turbine. 77. A combustor / heat exchanger in which one or more spiral water pipes are provided inside as a spiral water-cooled outer wall unit assembling structure, and the combustor / heat exchanger is shortened and arranged in a small number of honeycombs, and the compressed air is burned. A compressor that supplies heat to the heat exchanger and a gas turbine that obtains output using combustion gas, and a steam turbine that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is below the turbine heat resistance limit temperature. And a device for rotating the machine according to the output of the husband and the wife to perform work. 78. The method according to claim 75, wherein any one of a compressor, a steam turbine, and a gas turbine is selected.
The following is a combined steam gas turbine engine with all blades. 79. The water-cooled outer wall has a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine generator that obtains output, a steam turbine generator that obtains output using superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature, and heat supply from either of the two. And a device for supplying electricity from the couple. 80. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine generator that obtains output, a steam turbine generator that obtains output with superheated steam obtained by performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and heat and heat from either one of the two. A combined steam gas turbine engine having a cold heat supply and a device for supplying electricity from the couple. 81. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine generator for obtaining an output, a steam turbine generator for obtaining an output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, and for supplying electricity from each of them. And a combined steam gas turbine engine having the apparatus. 82. A combustor / heat exchanger in which a water-cooled outer wall is formed as a spiral welding structure unit assembly structure and one or more spirally-circulated water pipes are provided inside thereof, and the combustor / heat exchanger is shortened and arranged in a small-diameter multi-honey structure. And a gas turbine generator that obtains output with combustion gas, and outputs with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A steam gas turbine united engine comprising: a steam turbine generator for obtaining the above; a heat supply from any of the husband and the husband; and a device for supplying electricity from the husband and the husband. 83. A combustor / heat exchanger having a water-cooled outer wall formed as a unitary structure of a helical welding structure and having at least one helically annular water-conducting pipe therein and arranged to be short and arranged in a small-diameter multi-honey structure, and compressed air. And a gas turbine generator that obtains output with combustion gas, and outputs with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A steam turbine combined engine comprising: a steam turbine generator for obtaining the above; a device for supplying heat and cold from one of the couple; and a device for supplying electricity from the couple. 84. A combustor / heat exchanger in which a water-cooled outer wall has a spiral welding structure unit assembly structure and one or more spirally-circulated water pipes are provided inside thereof, and the combustor / heat exchanger is short and arranged in a small-diameter multi-honey structure. And a gas turbine generator that obtains output with combustion gas, and outputs with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam and gas turbine engine having a steam turbine generator for obtaining the above and a device for supplying electricity from the couple. 85. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided inside as a spiral water-cooled outer wall unit assembly structure, and the combustor / heat exchanger is shortened and arranged in a large number of small diameter honeycombs. A compressor that supplies the heat to the heat exchanger, a gas turbine generator that obtains output with combustion gas, and a steam that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature A combined steam and gas turbine engine having a turbine generator, heat supply from either of them, and a device for supplying electricity from the couple. 86. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided inside as a spiral water-cooled outer wall unit assembling structure, and the combustor / heat exchanger is shortened and arranged in a large number of small diameter honeycombs, and the compressed air is burned. A compressor that supplies the heat to the heat exchanger, a gas turbine generator that obtains output with combustion gas, and a steam that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature A combined steam and gas turbine engine comprising: a turbine generator; heat and cold heat supply from any one of the two; and a device for supplying electricity from the couple. 87. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided as a spiral water-cooled outer wall unit assembling structure and which are arranged in a short shape in a plurality of small diameter honeycombs, and the compressed air is burned. A compressor that supplies the heat to the heat exchanger, a gas turbine generator that obtains output with combustion gas, and a steam that obtains output with superheated steam obtained by exchanging heat so that the combustion gas temperature is equal to or lower than the turbine heat resistance limit temperature A combined steam gas turbine engine having a turbine generator and a device for supplying electricity from the couple. 88. The method according to claim 79, wherein any one of a compressor, a steam turbine, and a gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 89. A water-cooled outer wall having a spiral welding structure,
A combustor / heat exchanger in which one or more water pipes are provided in a spiral ring inside, and are arranged in a short shape like a large number of small diameter honeycombs, a compressor for supplying compressed air to the combustor / heat exchanger, and a combustion gas. A gas turbine generator having an exhaust temperature of 0 ° C. or less for obtaining an output, and a steam turbine generator with a condenser for obtaining an output with superheated steam obtained by heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature, And a device for supplying electricity from the couple. 90. A combustor / heat exchanger having a water-cooled outer wall formed as a unitary structure of a helical welding structure and having at least one helically annular water-conducting pipe therein and arranged in a small-diameter multi-honey structure, and a compressed air. And a gas turbine generator having an exhaust temperature of 0 ° C. or lower for obtaining an output from the combustion gas, and performing heat exchange so that the combustion gas temperature is equal to or lower than the turbine heat-resistant limit temperature. A combined steam gas turbine engine having a steam turbine generator with a condenser that obtains an output with the obtained superheated steam, and a device for supplying electricity from the couple. 91. A combustor / heat exchanger in which one or more spirally-circulated water pipes are provided internally as a spiral water-cooled outer wall unit assembly structure, and are arranged in a small-diameter multi-honey structure, and the compressed air is burned. Compressor to supply to the heat exchanger and heat exchanger, gas turbine generator with exhaust temperature of 0 ° C or less to obtain output from combustion gas, and superheat obtained by heat exchange so that combustion gas temperature is below the turbine heat resistance limit temperature A combined steam gas turbine engine having a steam turbine generator with a condenser for obtaining output with steam, and a device for supplying electricity from the couple. 92. The method according to claim 89, wherein any one of the compressor, the steam turbine, and the gas turbine is used.
The following is a combined steam gas turbine engine with all blades. 93. A combined steam gas turbine engine, wherein the combustor / heat exchanger of the all-blade gas turbine injects supercritical steam or superheated steam to reduce NOx by agitated combustion. 94. A combined steam gas turbine engine, wherein the combustor and heat exchanger of the gas turbine injects supercritical or superheated steam to reduce NOx by agitated combustion. 95. The combined steam gas turbine engine, wherein the exhaust gas temperature of the all blade gas turbine is set to 0 ° C. or lower. 96. The gas turbine has an exhaust gas temperature of 0 ° C.
A steam gas turbine combined engine characterized by the following. 97. A steam gas characterized in that the combustor / heat exchanger having one or more water pipes arranged in a helical ring inside is arranged as a single unit having a large diameter, wherein the small diameter is arranged so as to be a large number of honeycombs. Turbine united engine. 98. The steam turbine uses superheated steam under supercritical steam conditions.
A combined steam gas turbine engine according to any one of claims 97 to 97. 99. A combined steam gas turbine engine comprising: a magnetic friction power transmission device (14) in which an inner shaft device and an outer shaft device of the full blade gas turbine are connected at an optimum rotation ratio. 100. A combined steam gas turbine engine comprising a magnetic friction power transmission device (14) in which an inner shaft device and an outer shaft device of the full blade compressor are connected at an optimum rotation ratio. 101. The magnetic friction power transmission device (14)
Is a steam gas turbine combined engine having a cooling device. 102. A combined steam gas turbine engine, wherein a bypass is provided in an all-blade compressor that supplies the compressed air to a combustor / heat exchanger. 103. A steam gas turbine combined engine, wherein a bypass is provided in a compressor for supplying the compressed air to a combustor / heat exchanger. 104. A combined steam gas turbine engine, wherein a cooling device is provided in a magnetic friction power transmission device 14 for reversing an inner shaft device and an outer shaft device of the full blade gas turbine. 105. A combined steam gas turbine engine, wherein a cooling device is provided in a magnetic friction power transmission device 14 for reversing an inner shaft device and an outer shaft device of the all-blade compressor. 106. The full-blade steam turbine comprises an inner shaft device provided with an inner turbine blade group (20), and an outer shaft device provided with an outer turbine blade group (19). A steam turbine comprising: a rotor blade steam turbine which is combined with a magnetic friction power transmission device to supply superheated steam (5) from a center of an inner shaft device to drive the rotor blade steam turbine; Gas turbine combined engine. 107. The all-blade steam turbine compressor,
The inner shaft device is provided with an inner turbine blade group (20), and the outer shaft device is provided with an outer turbine blade group (19) and an inner compressor blade group (17). The two shafts are connected by a magnetic friction power transmission device to form a full-blade steam turbine, and an outer shaft device and an outer compressor blade group (16) are provided outside the inner compressor blade group (17), and are mutually inverted. The outer shaft device and the inner shaft device are combined by a magnetic friction power transmission device to form a full blade compressor, and superheated steam (5) is supplied from the center of the inner shaft device.
A combined steam gas turbine engine comprising a device for driving the all-blade steam turbine compressor. 108. The all-blade steam turbine compressor comprising:
An inner shaft unit is provided with an inner turbine blade group (20), and an outer shaft unit is provided with an outer turbine blade group (19). The front inner shaft device is provided with an inner compressor blade group (17), and the outer shaft device and the outer compressor blade group (16) are provided on the outer side, so that the outer shaft device and the inner shaft which are mutually inverted are provided. A device that is combined with a magnetic friction power transmission device to form a full blade compressor, supplies superheated steam (5) from the center of the inner shaft device, and drives the device as the full blade steam turbine compressor. A combined steam gas turbine engine, comprising: 109. The steam turbine, wherein an inner turbine stationary blade is provided on an inner fixed shaft device, and an outer turbine rotor blade group (19) is provided on an outer shaft device, and superheated steam (5) is provided from the center of the inner shaft device. A combined steam gas turbine engine comprising a steam turbine configured to be supplied and driven. 110. The steam turbine compressor, wherein an inner turbine stationary blade is provided on an inner fixed shaft device, and an outer turbine rotor blade group (19) is provided on an outer shaft device, and superheated steam (5) is provided from the center of the inner shaft device. The steam turbine is configured to be drivable by supplying the inner compressor rotor blade group (17) to the outer shaft device, and the inner compressor device blade group (17) is also used as the inner shaft device.
A combined steam and gas turbine engine comprising a compressor and a compressor provided by providing a casing and a stationary vane outside of the steam turbine. 111. The steam turbine compressor is provided with an inner turbine blade group (20) on an inner shaft device and a stationary blade on an outer shaft device, and injects and supplies superheated steam (5) from the upstream side. A steam turbine is configured so as to be drivable, a compressor is provided by providing an inner compressor moving blade group (17) in a front inner shaft device, and a casing and a stator blade provided outside the inner compressor moving blade group (17). A combined steam gas turbine engine provided as a steam turbine compressor. 112. The all-blade steam turbine compressor comprises:
A combined steam and gas turbine engine, wherein an all-blade compressor is removed to provide a full-blade steam turbine. 113. A combined steam gas turbine engine, wherein the steam turbine compressor is provided as a steam turbine by removing the compressor. 114. A water-cooled outer wall having a spiral welded structure and one or more spiral annular water pipes provided therein and having a combustor / heat exchanger in which a plurality of small-diameter multiple honeycombs are arranged and shortened. A combined steam and gas turbine engine comprising a combustor and a heat exchanger in which an outer wall and a water-cooled inner wall (54) are formed in a spiral welding structure and one or more spiral annular water pipes are provided therein. 115. A combustor / heat exchanger in which the water-cooled outer wall is formed as a spiral welding structure unit assembly structure and one or more spiral annular water pipes are provided therein and are arranged in a small-diameter multi-honey compact arrangement. Water-cooled outer wall and water-cooled inner wall (5
(4) A combined steam gas turbine engine, wherein (1) is a helical welding structure unit assembly structure, and a single combustor / heat exchanger having at least one helical annular water pipe therein. 116. A helical water cooling outer wall unit assembling structure in which one or more helical annular water pipes are provided inside and a combustor / heat exchanger which is arranged in a small number of small-diameter honeycombs is arranged. A steam-cooled gas turbine having a unitary structure of a water-cooled outer wall (26) and a unitary structure of a water-cooled inner wall (54), each of which is provided with one or more spiral annular water pipes therein. Coalition organization. 117. A combined steam gas turbine engine, wherein the all-blade gas turbine injects superheated steam (5) that has become water droplets outward and rearward by centrifugal force. 118. The combined steam gas turbine engine, wherein the all-blade steam turbine injects superheated steam (5) that has become water droplets outward and rearward by centrifugal force. 119. A steam gas turbine combined engine, wherein the steam turbine provided with the rotor blades on the outside injects superheated steam (5) as water droplets outward and rearward by centrifugal force. 120. A combined steam gas turbine engine wherein the combustor / heat exchanger injects superheated steam from fuel vapor injection means (27) to fix combustion gas to superheated steam. 121. The combustor / heat exchanger injects any one of supercritical superheated steam or water from a fuel vapor injection means (27) to fix the combustion gas to the superheated steam. Steam gas turbine combined engine. 122. The combined steam gas turbine engine, wherein the combustor / heat exchanger injects any one of supercritical superheated steam and water to fix the combustion gas to the superheated steam. 123. The combustor / heat exchanger injects any one of supercritical superheated steam or water containing a substance which promotes fixation of combustion gas water from a fuel vapor injection means (27), and A steam gas turbine combined engine, wherein the steam turbine is fixed to superheated steam. 124. The combustor / heat exchanger injects any one of supercritical superheated steam or water containing a substance that promotes fixation of combustion gas water to fix the combustion gas to the superheated steam. A combined steam gas turbine engine. 125. A combined steam gas turbine engine, wherein the combustion gas fixed to the superheated steam is mainly CO2. 126. A combined steam gas turbine engine, wherein the combustion gas fixed to the superheated steam is mainly a harmful combustion gas. 127. The combined steam gas turbine engine, wherein the all blade gas turbine cools the superheated steam with the low-temperature combustion gas and discharges the harmful combustion gas by fixed-water mixing and discharge. 128. A steam gas turbine combined engine, wherein the gas turbine cools superheated steam with a low-temperature combustion gas and discharges harmful combustion gas into a fixed water mixture. 129. The combined steam / gas turbine engine, wherein the all-blade gas turbine cools superheated steam and combustion gas by an exhaust heat exchanger (58), and discharges harmful combustion gas into a fixed water mixture. . 130. The combined steam gas turbine engine according to claim 130, wherein the gas turbine cools the superheated steam and the combustion gas by an exhaust heat exchanger (58), and discharges the harmful combustion gas in a fixed water mixture. 131. A steam gas turbine combined engine, wherein the combustion gas fixed to the water is drained by approaching harmlessly. 132. A steam gas turbine combined engine, wherein the gas turbine supplies cold heat. 133. A full blade compressor of the gas turbine includes a cooling means (5) provided on an inner compressor blade group including an inner shaft device.
5) A combined steam and gas turbine engine comprising: 134. A combined steam gas turbine engine according to claim 134, wherein the compressor of the gas turbine is provided with cooling means (55) in an inner compressor rotor group including an inner shaft device. 135. The full-blade compressor of the gas turbine includes a cooling means (5) provided on an inner compressor blade group including an inner shaft device.
5) and a steam gas turbine combined engine, comprising: a water injection means (56). 136. The steam gas turbine combined engine of the compressor of the gas turbine, wherein a cooling means (55) and a water injection means (56) are provided in an inner compressor blade group including an inner shaft device. . 137. The combined steam and gas turbine engine according to claim 137, wherein the full blade compressor of the gas turbine is provided with a capillary discharge means (57) in an outer compressor blade group including an outer shaft device. 138. The steam gas turbine combined engine, wherein the compressor of the gas turbine is provided with a capillary discharge means (57) in a casing including a compressor stationary blade. 139. The all-blade gas turbine includes a capillary discharge means (5) provided on an outer shaft device including an outer turbine blade group.
7) A combined steam gas turbine engine comprising: 140. The combined steam and gas turbine engine according to claim 140, wherein the gas turbine is provided with a capillary discharge means (57) in a casing including an outer turbine stationary blade. 141. The full blade gas turbine includes a capillary discharge means (5) provided on an outer shaft device including an outer turbine blade group.
7. A combined steam gas turbine engine according to 7), wherein water containing combustion gas is discharged. 142. A combined steam gas turbine engine according to claim 142, wherein the gas turbine is provided with a capillary discharge means (57) in a casing including an outer turbine stationary blade to discharge water containing combustion gas. 143. The gas turbine, wherein the exhaust gas temperature is set to 0.
A combined steam and gas turbine engine having a temperature of ℃ or lower. 144. A combined steam gas turbine engine according to claim 144, wherein said gas turbine has an inlet combustion gas temperature of 600 ° C. or lower. 145. The steam gas turbine combined engine, wherein the gas turbine has an inlet combustion gas temperature of 400 ° C or lower. 146. The combustor / heat exchanger is characterized in that in order to promote fixation of combustion gas water, heat exchange is performed to lower the temperature of the combustion gas as much as possible, thereby making the combustion gas a relative of superheated steam. Steam gas turbine combined engine. 147. In the combustor / heat exchanger, in order to promote fixation of the combustion gas water, superheated steam agitated combustion lowers the combustion gas temperature as much as possible, and makes the combustion gas a relative of the superheated steam. Steam gas turbine combined engine. 148. The gas turbine including the combustor / heat exchanger, in order to promote fixing of the combustion gas water, lowers the combustion gas temperature by contacting at a high temperature and a high pressure including a superheated steam agitated combustion to a low temperature and a low pressure. A steam gas turbine combined engine, wherein combustion gas is made relative to superheated steam. 149. A fuel vapor supply means (2) for heating and diluting fuel with superheated steam for injection.
7) A combined steam gas turbine engine comprising: 150. The steam combustor / heat exchanger further comprising a fuel vapor supply means (27) for suctioning and diluting fuel with superheated vapor and injecting it by utilizing the principle of spraying. Gas turbine combined engine. 151. The combustor / heat exchanger further comprises a fuel vapor supply means (27) for reducing NOx to 0 by diluting fuel with superheated steam and agitating and burning it with air. Steam gas turbine combined engine. 152. The combustor / heat exchanger includes a fuel vapor supply means (27) for reducing NOx to 0 by diluting fuel with superheated steam and agitating combustion with air in a high-pressure atmosphere. A combined steam gas turbine engine comprising: 153. The combustor / heat exchanger, in a high-pressure atmosphere, dilutes fuel with supercritical superheated steam and agitates and combusts with air to reduce NOx to 0, thereby providing fuel vapor supply means ( 27) A combined steam gas turbine engine comprising: 154. The fuel vapor supply means (27)
A combined steam gas turbine engine comprising a fuel injection port (60). 155. The fuel vapor supply means (27)
A combined steam gas turbine engine comprising a plurality of small fuel holes (62) inside a fuel injection port (60). 156. The fuel vapor supply means (27)
A combined steam gas turbine engine comprising a plurality of small fuel holes (62) inside a fuel injection port (60) and slidably fitted over a superheated steam cylinder port (59). 157. The fuel vapor supply means (27)
A number of small fuel holes (62) are provided inside the fuel nozzle (60) so that the fuel nozzle (60) can be slidably fitted on the superheated steam cylinder port (59). A steam gas turbine combined engine characterized by increasing or decreasing the numerical aperture of a steam turbine. 158. The fuel vapor supply means (27)
A number of small fuel holes (62) are provided inside the fuel nozzle (60) so that the fuel nozzle (60) can be externally slidably fitted to the superheated steam cylinder port (59). 62) A combined steam gas turbine engine, characterized in that the numerical aperture is increased / decreased and the fuel injection amount is increased / decreased. 159. The fuel vapor supply means (27)
A large number of small fuel holes (62) are provided inside the fuel nozzle (60) so that the fuel nozzle (60) can be externally slidably fitted to the superheated steam cylinder port (59). 62) A combined steam gas turbine engine wherein the numerical aperture is increased or decreased to control the fuel injection amount. 160. The fuel vapor supply means (27)
A number of small fuel holes (62) are provided inside the fuel nozzle (60) so that the fuel nozzle (60) can be externally slidably fitted to the superheated steam cylinder port (59). 62) A combined steam gas turbine engine wherein the numerical aperture is increased or decreased to control the fuel injection amount. 161. The fuel vapor supply means (27)
A steam characterized in that a plurality of small fuel holes (62) are provided inside the fuel injection port (60), and another cylindrical part is provided inside the superheated steam cylinder port (59) so as to be slidably reciprocated. Gas turbine combined engine. 162. The fuel vapor supply means (27)
A plurality of small fuel holes (62) are provided inside the fuel injection port (60), and inside the superheated steam cylinder port (59), another cylindrical component is provided so as to be slidable and reciprocated, and the cylindrical component is rotated. Thereby increasing or decreasing the numerical aperture of the fuel small hole (62). 163. The fuel vapor supply means (27)
A number of small fuel holes (62) are provided inside the fuel injection port (60), and inside the superheated steam cylinder port (59), another cylindrical component is provided so as to be able to slide around and reciprocate, and the cylindrical component is electrically operated. A combined steam gas turbine engine wherein the driving rotation increases or decreases the numerical aperture of the fuel small hole (62) and controls the fuel injection amount. 164. The fuel vapor supply means (27)
A number of small fuel holes (62) are provided inside the fuel injection port (60), and inside the superheated steam cylinder port (59), another cylindrical component is provided so as to be slidable and reciprocally fitted to the superheated steam cylinder port (59). A steam gas turbine combined engine characterized by increasing and decreasing the numerical aperture of the small fuel hole (62) by reciprocating the fuel gas and controlling the increase and decrease of the fuel injection amount. 165. The fuel vapor supply means (27)
A number of small fuel holes (62) are provided inside the fuel injection port (60), and inside the superheated steam cylinder port (59), another cylindrical component is provided so as to slide around and reciprocate, and the cylindrical component is hydraulically driven. A steam gas turbine combined engine characterized by increasing and decreasing the numerical aperture of the fuel small hole (62) by reciprocating the fuel gas and controlling the increase and decrease of the fuel injection amount. 166. The fuel vapor supply means (27)
A combined steam gas turbine engine comprising a superheated steam cylinder port (59). 167. The fuel vapor supply means (27)
A combined steam gas turbine engine comprising a superheated steam cylinder port (59) and a needle valve (61). 168. The fuel vapor supply means (27)
A combined steam and gas turbine engine comprising a needle valve (61) provided at a superheated steam cylinder port (59) and rotating the needle valve (61) to increase or decrease the injection amount of superheated steam. 169. The fuel vapor supply means (27)
A combined steam gas turbine engine comprising a needle valve (61) at a superheated steam cylinder opening (59), and electrically controlling the needle valve (61) to increase or decrease the injection amount of superheated steam. 170. The fuel vapor supply means (27)
A combined steam gas turbine engine comprising a needle valve (61) provided at a superheated steam cylinder port (59) and controlling the needle valve (61) by pneumatic drive to increase or decrease the injection amount of superheated steam. 171. The fuel vapor supply means (27),
A combined steam gas turbine engine comprising a needle valve (61) at a superheated steam cylinder opening (59), and hydraulically controlling the needle valve (61) to increase or decrease the injection amount of superheated steam.