Combined type energy-saving gas turbine inlet air cooling system

A gas turbine and intake air cooling technology, which is applied to gas turbine devices, jet propulsion devices, mechanical equipment, etc., can solve the problems that the air temperature cannot reach the ambient wet bulb temperature, the limited effect in high temperature and high humidity areas, and the low operation and maintenance costs. Achieve the effect of reducing one-time investment and operating costs, reducing installed capacity and reducing energy consumption

Active Publication Date: 2013-12-25
无锡金龙石化冶金设备制造有限公司
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, there are two main ways to cool the intake air of gas turbines: first, spray direct evaporative cooling, that is, in the intake passage of gas turbines, high-pressure desalted water passes through atomizing nozzles to form sprays and mixes with air, evaporates and absorbs heat, thereby To remove the sensible heat of the air, the system structure is as figure 1 As shown in the figure, 1 is a compressor, 2 is a combustion chamber, 3 is a gas turbine, 4 is a waste heat boiler, and 5 is a chimney. The air inlet of device 6 is connected with the air outlet of air filter 7, and high-pressure pipe 100 leads into air cooler 6, is provided with atomizing nozzle 200 on the high-pressure pipe 100 that stretches into air cooler 6, stretches out air cooler The high-pressure pipe 100 of 6 is connected to the water outlet of the desalinated water tank 300, and the end of the air cooler 6 is provided with a demister 8, and the water outlet of the air cooler 6 is connected to the water inlet pipe of the desalinated water tank 300, and in this The pipeline is provided with a return water pump 400 and a demineralized water filter device 500. The method of spraying direct evaporative cooling is simple, requires less investment, and is low in operation and maintenance costs. Ambient humidity and water temperature have a great influence, and need to consume a certain amount of desalted water. It is generally suitable for high temperature and dry areas, and has limited effect on high temperature and high humidity areas; second, indirect contact heat exchange, through a refrigerator (such as lithium bromide Absorption unit or electric refrigeration chiller) to produce chilled water, t

Method used

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  • Combined type energy-saving gas turbine inlet air cooling system
  • Combined type energy-saving gas turbine inlet air cooling system
  • Combined type energy-saving gas turbine inlet air cooling system

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Embodiment Construction

[0016] The specific embodiments of the present invention will be described below in conjunction with the drawings.

[0017] see image 3 , The present invention includes a compressor 1, the outlet end of the compressor 1 is connected to the inlet end of the combustion chamber 2, the outlet end of the combustion chamber 2 is connected to the inlet end of the gas turbine 3, and the inlet end of the compressor 1 is connected to the air cooler 6 The air outlet pipe is connected, the air inlet of the air cooler 6 is connected with the air outlet of the air filter 7, the air cooler 6 is provided with a demister 8, and the first surface heat exchanger 9 is provided in the air cooler 6, The water inlet of the first surface heat exchanger 9 is connected to the water outlet of the first chilled water circulating pump 10, the water inlet of the first chilled water circulating pump 10 is connected to the chilled water outlet of the main refrigerator 11, and the first surface heat exchanger 9 ...

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Abstract

The invention relates to a combined type energy-saving gas turbine inlet air cooling system which comprises an air compressor, a combustion chamber and a gas turbine, wherein the air compressor is connected with an air outlet pipeline of a cooler, the air inlet of the cooler is connected with an air filter, a demister is arranged in the cooler, a first surface heat exchanger is arranged in the air cooler, the water inlet of the first surface heat exchanger is connected with the water outlet of a first chilled water circulating pump, the water inlet of the first chilled water circulating pump is connected with the chilled water outlet of a main refrigerator, the water outlet of the first surface heat exchanger is connected with the chilled water inlet of the main refrigerator, the water outlet of the cooler is connected with a water inlet of a condensed water tank, condensed water returns to the cooler via a high pressure pipe, an atomizing nozzle is arranged on the high pressure pipe stretching into the cooler, and the high pressure pipe outside the cooler is provided with a condensed water pump and a condensed water filtering device. According to the invention, indirect heat exchange cooling and direct evaporative cooling are adopted by the combination, so that the energy consumption is reduced, the installing capacity of the main refrigerator is reduced, and the system is suitable for use in areas with high temperature and high humidity.

Description

Technical field [0001] The invention relates to a gas turbine inlet air cooling device, in particular to a combination that uses spray direct evaporative cooling and indirect heat exchange cooling, and recovers the condensed water from the indirect heat exchange cooling process and uses it as a cold source for spray direct evaporative cooling A type energy-saving gas turbine intake air cooling system, in particular, relates to a system for cooling the gas turbine intake air used in gas-steam combined cycle power generation. Background technique [0002] In the gas-steam combined cycle power generation system, the main structure of a gas turbine (hereinafter referred to as "gas turbine") includes a compressor, a combustion chamber, and a gas turbine. The compressor compresses the air sucked in, and the compressed air enters the combustion chamber and is injected The fuel mixes and burns into high-temperature gas, which then flows into the gas turbine to expand and do work, pushing...

Claims

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Application Information

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IPC IPC(8): F02C7/141
Inventor 陈若莱夏国华
Owner 无锡金龙石化冶金设备制造有限公司
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