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Inlet air cooling control system for gas turbine

An air intake cooling and control system technology, applied in gas turbine devices, mechanical equipment, jet propulsion devices, etc., can solve problems such as increased power consumption, decreased gas turbine output, and reduced mass flow through the compressor and gas turbine. High degree of automation, high safety, and the effect of improving control efficiency

Inactive Publication Date: 2016-10-26
NANJING LEAGUER UNITED TOP HLDG POWER ENERGY SAVING CO LTD
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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
[0003] When the gas turbine unit is at full load, as the ambient temperature rises, the output and thermal efficiency of the gas turbine will decrease

Method used

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  • Inlet air cooling control system for gas turbine

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Embodiment Construction

[0018] In order to deepen the understanding of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. The following examples are only used to illustrate the technical solution of the present invention more clearly, but not to limit the protection scope of the present invention.

[0019] Such as figure 1 As shown, the air intake cooling control system of the gas turbine of the present invention includes a heat exchanger, a hot water circulation pump, an absorption chiller and an air cooler, and the heat exchanger, the hot water circulation pump and the absorption chiller communicate with each other through a hot water supply pipe The connection between the absorption chiller and the air cooler is connected through the chilled water supply pipe, the heat exchanger and the absorption chiller are also connected through the hot water return pipe, and the absorption chiller and the air coo...

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Abstract

The invention discloses an inlet air cooling control system for a gas turbine. The system comprises heat exchangers, hot water circulating pumps, absorption water cooling units and air coolers, wherein the heat exchangers, the hot water circulating pumps and the absorption water cooling units are connected one another through hot water supply pipes; the absorption water cooling units and the air coolers are connected through freeze water supply pipes; the heat exchangers and the absorption water cooling units are further connected through hot water return pipes; and the absorption water cooling units and the coolers are further connected through freeze water return pipes. The system further comprises a control cabinet which is connected to the hot water supply pipes, the hot water return pipes, the freeze water supply pipes and the freeze water return pipes. The inlet air cooling control system for the gas turbine disclosed by the invention is high in safety: once problems or faults happen at a place, the control cabinet sends out a command to cut off the system so as to ensure the integral safety; automatic control is realized through the control cabinet, and to-be-monitored parameters are centralized to a control room, so that the user knows the working state of each part of the system anytime and sends out the control command.

Description

technical field [0001] The invention relates to a combustion engine air intake cooling control system. 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. [0003] When the gas turbine unit is at full load, as the ambient temperature rises, the output and thermal efficiency of the gas turbine will decrease. Therefore, configuring the air intake cooling system in non-winter periods can increase the output of gas turbines or combined cycle units and enhance the peak-shaving performance of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/143F02C9/00
CPCF02C7/143F02C9/00
Inventor 王小鹏李剑斌邵帅仲恒
Owner NANJING LEAGUER UNITED TOP HLDG POWER ENERGY SAVING CO LTD