Patent ID: 11867120
Assignee: YANTAI JEREH PETROLEUM EQUIPMENT & TECHNOLOGIES CO., LTD.
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  E | IPC E  F

Claim 13:
14. The turbine engine air-inlet cooling system according to claim 1, further comprising:
a liquefied natural gas gasification device, configured to gasify liquefied natural gas;
a gasification pipeline, connected to the liquefied natural gas gasification device; and
a cooling liquid transmission pipeline, connected to the gasification pipeline,
wherein;
the liquefied natural gas is gasified to cool a working liquid in the cooling liquid transmission pipeline;
the air-inlet cooling device comprises a air-liquid heat exchange device; and
the air-liquid heat exchange device comprises an air-inlet end, a air-outlet end and a liquid-inlet end, the air-inlet end of the air-liquid heat exchange device being connected to the cooling liquid transmission pipeline and serving as the air-input end of the air-inlet cooling device, the working air being input into the air-liquid heat exchange device through the air-inlet end of the air-liquid heat exchange device and the working liquid being input into the air-liquid heat exchange device through the liquid-inlet end of the air-liquid heat exchange device conducting heat exchange in the air-liquid heat exchange device, and the air-outlet end of the air-liquid heat exchange device serving as the air-output end of the air-inlet cooling device to be connected to the air-inlet end of the turbine engine.