KR101935637B1 - Combined cycle power generation system - Google Patents
Combined cycle power generation system Download PDFInfo
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- KR101935637B1 KR101935637B1 KR1020160154023A KR20160154023A KR101935637B1 KR 101935637 B1 KR101935637 B1 KR 101935637B1 KR 1020160154023 A KR1020160154023 A KR 1020160154023A KR 20160154023 A KR20160154023 A KR 20160154023A KR 101935637 B1 KR101935637 B1 KR 101935637B1
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- South Korea
- Prior art keywords
- pressure
- steam
- low
- turbine
- medium
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- 238000010248 power generation Methods 0.000 title description 20
- 238000001816 cooling Methods 0.000 claims abstract description 86
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 61
- 238000011084 recovery Methods 0.000 claims abstract description 26
- 239000007789 gas Substances 0.000 claims description 101
- 239000012530 fluid Substances 0.000 claims description 65
- 238000003303 reheating Methods 0.000 claims description 9
- 238000007599 discharging Methods 0.000 claims description 7
- 239000000446 fuel Substances 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 7
- 239000000567 combustion gas Substances 0.000 claims description 5
- 230000000694 effects Effects 0.000 abstract description 9
- 238000000034 method Methods 0.000 abstract description 9
- 238000009833 condensation Methods 0.000 description 5
- 230000005494 condensation Effects 0.000 description 5
- 239000007788 liquid Substances 0.000 description 3
- 239000003054 catalyst Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003507 refrigerant Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
- F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
- F01K23/06—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
- F01K23/10—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with exhaust fluid of one cycle heating the fluid in another cycle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K11/00—Plants characterised by the engines being structurally combined with boilers or condensers
- F01K11/02—Plants characterised by the engines being structurally combined with boilers or condensers the engines being turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K17/00—Using steam or condensate extracted or exhausted from steam engine plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
The present invention provides a cooling apparatus for a gas turbine blade, which includes a cooling air generating section separately from a gas turbine section, and supplies compressed air generated in a low-pressure compressor and a high-pressure compressor included in the cooling air generating section to cooling air of a gas turbine blade, Pressure condensed air flowing from the low-pressure compressor to the high-pressure compressor is intermittently cooled using the intermediate heat exchanger in which the condensed water flows and the compressor cooling power is reduced due to the precooling effect of the cooling air and the intermediate cooling effect of the cooling air, The performance of the gas turbine is improved and the heat recovered in the intermediate cooling process is transferred to the arrangement recovery cycle to improve the performance of the arrangement recovery cycle.
Description
The present invention relates to a combined-cycle power generation system, and more particularly, to a combined-cycle power generation system that includes a cooling-air generating unit separately from a gas turbine unit, and compresses compressed air generated in the low-pressure compressor and the high- Pressure compressed air flowing from the low-pressure compressor to the high-pressure compressor is intermittently cooled by using an intermediate heat exchanger provided with cooling air and condensed water generated by condensation of the steam. The cooling effect of the cooling air and the intermediate cooling The present invention relates to a combined-cycle power generation system in which the performance of a gas turbine is improved over the conventional example cooling method, and the heat recovered in the intermediate cooling process is transferred to an arrangement recovery cycle to improve the performance of the arrangement recovery cycle .
Typical examples of the energy conversion apparatus include a gas turbine system or a steam turbine system that generates electricity using energy such as fuel.
Specifically, the gas turbine supplies fuel and air to burn the fuel, thereby driving the turbine using the high-temperature, high-pressure combustion gas generated thereby. The steam turbine uses a steam generator to heat the feed water Thereby generating steam, and then supplying the generated steam to the turbine to drive the steam turbine.
Efforts to improve the energy efficiency of systems have continued since the development of gas turbine power generation systems or steam turbine power generation systems that produce power through such gas turbines or generators connected to steam turbines.
For reference, the liquid circulating through the system can be defined differently depending on the flow position. The liquid, which is condensed by the condenser and supplied to the steam generating means, is supplied to a plurality of condensed water and steam generating means The liquid that is converted into steam can be defined as feed water.
In particular, the combined-cycle power generation system, which uses heat from the exhaust gas produced after producing energy from the gas turbine to heat the steam turbine cycle water using HRSG (Heat Recovery Steam Generator), uses only a steam turbine or only a gas turbine It is a system whose efficiency is remarkably improved as compared with the power generation system used.
The prior art is disclosed in Japanese Patent Registration No. 10-1531931 (Jun. 22, 2015).
Conventional turbine cooling technology reduces the surface temperature of turbine blades by injecting a portion of the compressed air from the compressor into the turbine blades. The higher the performance of the gas turbine, the higher the compression ratio and the higher turbine inlet temperature Hereinafter, the temperature of the compressed air is high to provide a technique for cooling the compressed air.
To solve this problem, conventionally, cooling air added to the compressor is cooled by a separate cooler in order to pre-cool the cooling air for cooling the turbine blades. However, pre-cooling of the cooling air is necessary for increasing the pressure ratio and turbine inlet temperature , The energy is discarded as it is in the process of cooling the compressed air.
Accordingly, in order to solve the above-described problem, the present invention provides a cooling air generator separately from the gas turbine, and the compressed air generated in the low-pressure compressor and the high-pressure compressor included in the cooling air generator is supplied as cooling air for the gas turbine blade Pressure compressing air flowing from the low-pressure compressor to the high-pressure compressor is intermittently cooled using the intermediate heat exchanger in which the condensed water generated by the condensation of the steam flows, and the pre-cooling effect of the cooling air and the intermediate- The present invention provides a combined-cycle power generation system in which the performance of a gas turbine is improved as compared with the conventional pre-cooling method due to a decrease in power, and the heat recovered in the intermediate cooling process is transferred to an arrangement recovery cycle to improve the performance of the arrangement recovery cycle.
A combined-cycle power generation system according to the present invention includes a compressor for introducing outside air into a high pressure by a rotational force, a compressor connected to an outlet of the compressor, for introducing compressed air compressed by the compressor, A gas turbine section that is connected to the compressor and includes a gas turbine in which a high temperature and high pressure combustion gas discharged from the combustor generates a rotational force corresponding to the turbine blade; A steam turbine section driven by the steam generated in the batch recovery boiler section, and a steam turbine section driven by steam generated by the steam turbine section, A condenser for condensing the steam through the steam turbine section, Wherein the condenser includes a condenser connected to a line through which the fluid flows with the steam turbine portion and which condenses the fluid discharged from the steam turbine portion to discharge condensed water, A low pressure pump connected to the condensing water line and connected to the condensing water line at a low pressure, and a low pressure pump connected to the condensing water line at a low pressure to discharge the condensed water from the condensing water line at a low pressure; A medium pressure pump connected to a line through which the fluid flows to the deaeration device and to discharge the fluid deaerated through the deaeration device under a medium pressure; And a high-pressure pump for sending the fluid sent out under a medium pressure to a high pressure. And a cooling air generating unit for cooling the gas turbine by providing the generated cooling air to the gas turbine of the gas turbine unit, wherein the cooling air generator is driven by the rotational force of an electric motor using an external power source, A low pressure compressor for compressing and discharging outside air to a low pressure and a high pressure compressor driven by the torque of an electric motor using an external power source to compress the low pressure air discharged from the low pressure compressor to a high pressure and discharge the low pressure air, And an intermediate cooling heat exchanger for intermediate cooling the cooling air by heat exchange with low-pressure air discharged from the condenser and condensed water generated by condensing the steam in the condenser, wherein the steam turbine includes a low-pressure turbine generating a rotational force by low-pressure steam, An intermediate-pressure turbine generating a rotational force by the steam of the high-pressure steam, Pressure boiler is connected to a line through which the fluid flows with the low-pressure pump inside the exhaust passage, and a hot-water tank for heating the low-pressure condensate flowing through the inside by heat exchange with the exhaust gas, (Condensed water) is introduced through the deaerator into the exhaust pipe, and the fluid (condensed water) is heated by the heat exchange between the fluid (condensate) and the exhaust gas inside the exhaust pipe, Pressure condenser, which is connected to a line through which the fluid flows in the exhaust passage, and which is a fluid flowing along the inside of the exhaust passage, A first high pressure economizer for heating by heat exchange with the first high pressure economizer and for supplying the heated condensed water to the second high pressure economizer, A low pressure and hot air which is connected to a line through which the fluid flows with the low pressure evaporator and heats the low pressure steam flowing along the inside by heat exchange with the exhaust gas to supply the heated low pressure steam to the steam turbine section, Pressure condensate, which is a degassed fluid flowing along the inside of the furnace, is heated by heat exchange with the exhaust gas to generate steam, and the generated steam is supplied to the intermediate-pressure evaporator Pressure economizer and a medium pressure evaporator connected to a line through which the fluid flows with the medium pressure economizer in the exhaust passage to introduce steam generated through the medium pressure economizer and generate and supply a medium pressure steam using exhaust gas, And is connected to a line through which the fluid flows with the intermediate-pressure evaporator in the exhaust passage, Pressure steam is heated by heat exchange with the exhaust gas to mix the steam with the steam discharged from the high-pressure turbine to provide the first reheater, A second high pressure economizer connected to a line through which the fluid flows with the intermediate cooling heat exchanger and the first high pressure economizer and for heating the condensed water as a fluid flowing along the inside thereof by heat exchange with the exhaust gas and providing the condensed water to the high pressure evaporator; Pressure economizer and a second high-pressure economizer connected to the second high-pressure economizer through a line through which the fluid flows, the high-pressure steam is generated by heat exchange with the exhaust gas by flowing the fluid heated through the second high-pressure economizer, Pressure evaporator and a line through which the fluid flows with the medium pressure and the heat inside the exhaust passage, A first reheater for introducing a medium pressure steam heated by pressure and heat to reheat the medium pressure steam by heat exchange with the exhaust gas to provide reheated medium pressure steam to the second reheater, Pressure evaporator and a second high-pressure reheater for reheating the high-pressure steam flowing through the interior of the high-pressure evaporator by heat exchange with the exhaust gas to provide reheated high-pressure steam to the second high- Pressure reheating line and a line through which the fluid flows in the exhaust gas recirculation passage in the exhaust passage so as to introduce the intermediate-pressure steam reheated by the first reheater to heat-exchange the exhaust gas with the intermediate- A second reheater for reheating the second high-pressure reheater to provide reheated steam of a medium pressure to the steam turbine, and a second reheater for reheating the second high- It is connected to, and re-heating the high pressure of the steam that flows along the inside of the heat exchange with the exhaust gas, and a second high-pressure reboiler to provide vapor of the re-heated high-pressure parts of the steam turbine.
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The combined-cycle power generation system according to an embodiment of the present invention provides compressed air generated at a low pressure and a high pressure separately from the gas turbine as cooling air for a gas turbine blade, so that the consuming power of the compressor in the gas turbine is reduced, The performance of the gas turbine is improved.
Pressure refrigerant flowing from the low-pressure compressor to the high-pressure compressor is intermittently cooled using the intermediate heat exchanger in which the condensed water generated by the condensation of the steam flows, the cooling effect of the cooling air and the heat recovered in the intermediate cooling process So that the performance of the array recovery cycle is improved.
FIG. 1 is a schematic view illustrating a combined-cycle thermal power generation system according to an embodiment of the present invention.
Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. Prior to this, terms and words used in the present specification and claims should not be construed as limited to ordinary or dictionary terms, and the inventor should appropriately interpret the concepts of the terms appropriately The present invention should be construed in accordance with the meaning and concept consistent with the technical idea of the present invention.
Therefore, the embodiments described in the present specification and the configurations shown in the drawings are merely the most preferred embodiments of the present invention, and are not intended to represent all of the technical ideas of the present invention. Therefore, It should be understood that there may be variations.
The present invention provides a cooling apparatus for a gas turbine blade, which includes a cooling air generating unit separately from a gas turbine unit, and supplies compressed air generated in a low-pressure compressor and a high-pressure compressor included in the cooling air generating unit to cooling air of a gas turbine blade, Pressure condensed air flowing from the low-pressure compressor to the high-pressure compressor is intermittently cooled using the intermediate heat exchanger in which the condensed water flows and the compressor cooling power is reduced due to the precooling effect of the cooling air and the intermediate cooling effect of the cooling air, The present invention relates to a combined-cycle power generation system in which the performance of a gas turbine is improved and a heat recovery cycle is performed in an intermediate cooling process to improve the performance of an arrangement recovery cycle.
The combined thermal power generation system according to an embodiment of the present invention includes a
The
The compressed air compressed by the
The
The high temperature and high pressure exhaust gas discharged from the
As the
At this time, the
Also, the combined-cycle power generation system according to an embodiment of the present invention includes a
The low-
The
Accordingly, the cooling
The intermediate cooling heat exchanger 430 is connected to the
Therefore, the power consumption of the compressor is reduced due to the intermediate cooling effect of the cooling air, thereby improving the performance of the gas turbine over the conventional cooling method.
In addition, the arrangement of the exhaust gas generated in the
Here, the
The detailed description of the power generation process of the
The
The
The
In addition, the
The low pressure condensate supplied through the
At this time, the
The condensed water heated by the
Here, the
The fluid with the air removed by the
Here, the exhaust
The
At this time, the generated low-pressure steam is diverged and supplied to the
The low-pressure and high-
The low pressure steam supplied to the
The condensed water, which is a fluid branched from the
The
The medium pressure steam generated by the
The
The
The medium-pressure steam supplied to the
The condensed water sent out from the
At this time, the condensed water through the intermediate cooling heat exchanger 430 is supplied to the second
The first high-
The second
In addition, the high-
The high pressure steam generated in the
The second high-
The high pressure steam supplied to the
Therefore, the combined-cycle power generation system according to an embodiment of the present invention includes a cooling air generator separately from the gas turbine, and the compressed air generated in the low-pressure compressor and the high-pressure compressor included in the cooling air generator is cooled Pressure compressed air flowing from the low-pressure compressor to the high-pressure compressor is intermittently cooled by using an intermediate heat exchanger in which condensed water generated by the condensation of the steam flows and is supplied to the air and the intermediate cooling effect of the cooling air The performance of the gas turbine is improved more than that of the conventional example cooling method, and the heat recovered in the intermediate cooling process is transferred to the arrangement recovery cycle to improve the performance of the arrangement recovery cycle.
While the present invention has been described with reference to exemplary embodiments, it is to be understood that the invention is not limited to the disclosed exemplary embodiments, but, on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims. Accordingly, the true scope of the present invention should be determined by the technical idea of the appended claims.
100: gas turbine section
110: compressor
120: Combustor
130: Turbine
200: Sequence recovery boiler section
210: hot water machine
220: Low pressure evaporator
221: Medium pressure evaporator
222: High-pressure evaporator
230: Low pressure and heat
231: Heavy pressure and heat
232: First High Pressure Reheater
233: Second High Pressure Reheating
240: First High Pressure Economizer
241: Medium pressure economizer
242: second high pressure economizer
250: 1st reheating
251: Second reheating
300: steam turbine section
310: Low pressure turbine
320: Medium pressure turbine
330: High pressure turbine
340: second generator
400: cooling air generating unit
410: Low pressure compressor
420: High pressure compressor
430: Intermediate cooling heat exchanger
500: condenser
510: condenser
520: Low pressure pump
530: Deaerator
540: Medium pressure pump
550: High pressure pump
Claims (5)
A combustor connected to an outlet of the compressor for introducing the compressed air compressed by the compressor to mix fuel supplied from the outside and discharging compressed high-temperature high-pressure combustion gas;
A gas turbine section that is connected to the compressor and includes a gas turbine in which a high-temperature, high-pressure combustion gas discharged from the combustor generates rotational force corresponding to the turbine blade;
An arrangement recovery boiler unit for generating steam using the arrangement of the exhaust gas generated in the gas turbine unit;
A steam turbine section driven by steam generated in the batch recovery boiler section;
A first generator and a second generator that generate power by the power of the gas turbine section and the steam turbine section;
And a condensing portion for condensing the steam through the steam turbine portion and re-supplying the steam to the batch recovery boiler portion,
A condenser connected to a line through which the fluid flows with the steam turbine section and discharging condensed water by condensing the fluid discharged from the steam turbine section;
A low pressure pump connected to a line through which the fluid flows with the condenser and to discharge the condensed water discharged from the condenser to a low pressure;
A deaerator connected to a line through which the fluid flows with the batch recovery boiler portion and removes air from the condensate through the batch recovery boiler portion;
A medium pressure pump connected to the deaerator through a line through which the fluid flows, and delivering the deaerated fluid through the deaerator at a medium pressure;
And a high-pressure pump connected to the medium-pressure pump through a line through which the fluid flows, and for sending out the medium-pressure fluid to the high pressure,
And a cooling air generator for cooling the gas turbine by supplying outside air to generate air by compressing the air to generate cooling air and supplying the generated cooling air to the gas turbine of the gas turbine portion,
The cooling air generator includes a low-pressure compressor driven by a rotational force of an electric motor using an external power source and compressing and discharging the introduced external air to a low pressure;
A high pressure compressor driven by a rotational force of an electric motor using an external power source and compressing and discharging the low pressure air discharged from the low pressure compressor to a high pressure;
And an intermediate cooling heat exchanger for intermediate-cooling the low-pressure air discharged from the low-pressure compressor and the condensed water generated by condensing the steam in the condenser,
Wherein the steam turbine comprises: a low pressure turbine generating a rotational force with low pressure steam; A medium pressure turbine generating a torque by means of steam of medium pressure; And a high-pressure turbine generating a rotating force by high-pressure steam,
The boiler comprising: a hot water tank connected to a line through which the fluid flows with the low pressure pump in the exhaust passage to heat low-pressure condensed water flowing through the inside of the exhaust pipe by heat exchange with the exhaust gas;
(Condensed water) is introduced through the deaerator to flow the fluid (condensed water) through the heat exchange between the fluid (condensate) and the exhaust gas inside the exhaust passage, A low-pressure evaporator for generating low-pressure steam by heating to discharge the fluid as low-pressure steam;
Pressure condenser which is connected to a line through which the fluid flows with the high-pressure pump in the exhaust passage and which heats the high-pressure condensate, which is a fluid flowing along the inside, through heat exchange with the exhaust gas, and supplies the heated condensate to the second high-pressure economizer 1 high pressure economizer;
Pressure steam is supplied to the steam turbine section by heating the low-pressure steam flowing through the inside thereof by heat exchange with the exhaust gas and supplying the heated low-pressure steam to the steam turbine section, With heat;
Pressure condensate, which is a degassed fluid flowing along the inside of the exhaust passage, is heated by heat exchange with the exhaust gas to generate steam, and the generated steam is supplied to the intermediate-pressure evaporator Pressure economizer;
A middle pressure evaporator connected to a line through which the fluid flows with the medium pressure economizer in the exhaust passage to introduce steam generated through the intermediate pressure economizer and generate and supply a medium pressure steam using exhaust gas;
Pressure steam which flows in the inside of the exhaust passage through a line through which the fluid flows with the medium-pressure evaporator, heats the medium-pressure steam flowing through the inside of the exhaust passage by heat exchange with the exhaust gas, Medium pressure and hot air to provide a first reheater by mixing;
A second high-pressure evaporator that is connected to the intermediate cooling heat exchanger and the first high-pressure economizer through a line through which the fluid flows, inside the exhaust passage, for heating the condensed water, which is a fluid flowing along the interior thereof, An economizer;
And a second high pressure economizer connected to the second high pressure economizer through a line through which the fluid flows, the fluid heated by the second high pressure economizer is introduced into the exhaust passage to generate high pressure steam by heat exchange with the exhaust gas, A high pressure evaporator provided with heat;
Pressure steam is introduced into the exhaust passage through a line through which the fluid flows with the medium pressure and the heat, the medium-pressure steam heated by the medium pressure and the heat is introduced into the exhaust passage, the medium-pressure steam is primarily reheated by heat exchange with the exhaust gas, A first reheater for supplying the steam of the intermediate pressure to the second reheater;
Pressure steam to the second high-pressure reheater, the second high-pressure reheater being connected to the high-pressure evaporator through a line through which the fluid flows, and reheating the high-pressure steam flowing through the inside of the exhaust passage by heat exchange with the exhaust gas, A first high-pressure reheater;
Pressure steam which is reheated by the first reheater to flow into the exhaust pipe and is reheated by reheating the intermediate-pressure steam by heat exchange with the exhaust gas, A second reheater for providing reheated steam of a medium pressure to the steam turbine section;
Pressure steam that flows through the inside of the exhaust passage and is connected to a line through which the fluid flows, and reheats the high-pressure steam flowing through the inside of the exhaust passage by heat exchange with the exhaust gas to supply reheated high-pressure steam to the steam turbine section And a second high-pressure reheater operatively connected to the second high pressure reheater.
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JP2014009606A (en) * | 2012-06-28 | 2014-01-20 | Mitsubishi Heavy Ind Ltd | Cooling system of turbine blade and gas turbine |
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JP2014009606A (en) * | 2012-06-28 | 2014-01-20 | Mitsubishi Heavy Ind Ltd | Cooling system of turbine blade and gas turbine |
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