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Integrated system for heating and cooling inflow air of gas turbine

A gas turbine and integrated system technology, applied in the field of integrated systems, can solve the problems of reducing the mass flow rate, air density, and output of the gas turbine flowing through the compressor and the gas turbine, etc.

Active Publication Date: 2014-04-02
ZHEJIANG ELECTRIC POWER DESIGN INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the ambient temperature rises, the air density decreases, resulting in a decrease in the mass flow through the compressor and gas turbine, resulting in a decrease in the output of the gas turbine
The increase in ambient temperature will also reduce the compression ratio of the compressor and increase the power consumption, resulting in a further decrease in the output of the gas turbine
For simple cycle or combined cycle, as the ambient temperature increases, the output and thermal efficiency of the gas turbine will decrease

Method used

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  • Integrated system for heating and cooling inflow air of gas turbine

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Embodiment

[0024] Embodiment: The gas turbine intake air heating (anti-freezing) and cooling integrated system according to the present invention mainly includes a gas turbine 3, a compressor 4, a waste heat boiler 1, a steam turbine 2, a condenser 5, a cooling tower 6, a circulation Water pump 7 , lithium bromide refrigerator 9 , expansion tank 10 , chilled water pump 11 , air heat exchanger 12 , water-water heat exchanger 13 , booster pump 8 , pipeline pump 14 and first valve 101 to fifteenth valve 115 .

[0025] The driving heat source of the lithium bromide refrigerator 9 in the gas turbine inlet cooling system adopts the heating and extraction steam of the steam turbine 2 or the low-pressure main steam, which is drawn from the steam turbine 2 and connected with the lithium bromide refrigerator 9 through the fourteenth valve 114, and the driving steam is condensed The final condensed water passes through the fifteenth valve 115, and is connected to the condensed water pipeline behind ...

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Abstract

The invention discloses an integrated system for heating and cooling inflow air of a gas turbine. The integrated system comprises a lithium bromide refrigerator, wherein the inlet of a driving heat source of the lithium bromide refrigerator is connected with a heat supply steam bleeding or low pressure main steam leading-out port of a steam turbine; condensed water formed by the heat supply steam bleeding or low pressure main steam after being condensed through the lithium bromide refrigerator is lead out from a condensed water leading-out port of the lithium bromide refrigerator, and then is connected to a condensed water pipeline behind a shaft sealing heater through a pipeline pump; a cooling water inlet of the lithium bromide refrigerator is connected with an outlet of a circulating water pump in a power plant circulating water pipeline, and a cooling water outlet of the lithium bromide refrigerator is connected with a backwater pipeline in the circulating water pipeline; a refrigerant water outlet of the lithium bromide refrigerator is connected with the inlet of a refrigerant water heat exchange channel in an air cooler through a chilled water pump, and the outlet of the refrigerant water heat exchange channel is connected back to a refrigerant water inlet of the lithium bromide refrigerator; the air cooler is also internally provided with an air heat exchange channel, and the hot air sucked into the air heat exchange channel carries out heat exchange with the refrigerant water of a refrigerant water heat exchange channel.

Description

technical field [0001] The invention relates to an integrated system for gas turbine inlet heating or anti-freezing and cooling, which belongs to the field of energy technology. Background technique [0002] The gas turbine is a constant-capacity power machine, and its performance is closely related to the ambient temperature. When the ambient temperature rises, the air density decreases, resulting in a decrease in the mass flow through the compressor and gas turbine, resulting in a decrease in the output of the gas turbine. The increase in ambient temperature will also reduce the compression ratio of the compressor and increase the power consumption, resulting in a further decrease in the output of the gas turbine. For simple cycle or combined cycle, as the ambient temperature increases, the output and thermal efficiency of the gas turbine will decrease. Therefore, configuring the air intake cooling system during the high temperature period in summer can increase the out...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/141
Inventor 林俊光沈又幸光旭张卫灵费雄军徐红波任渊源陈金耀吴骅鸣
Owner ZHEJIANG ELECTRIC POWER DESIGN INST
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