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
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[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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