Gas compressor unit of gas turbine inlet based on refrigerant cooling

[0019] The following description is used to disclose the present invention so that those skilled in the art can implement the present invention. The preferred embodiments in the following description are only examples, and those skilled in the art can think of other obvious variations. The basic principles of the present invention defined in the following description can be applied to other embodiments, modifications, improvements, equivalents, and other technical solutions that do not depart from the spirit and scope of the present invention.

[0020] Such as figure 1 , A gas turbine inlet gas compressor unit based on refrigerant cooling, including pre-filter 2, intake valve 3, motor 5, coupling 6, compression chamber 7, gas storage tank 8, coil 9, filter 10 , Gas turbine 12, temperature control valve 13, compressor 14, throttle valve 15, condenser 16, and water tank 17, the outlet of the pre-filter 2 is connected to the compression chamber 7 through the intake valve 3, and the lo