Method for cooling electronic component in turbojet of aircraft, involves generating electric power from sensors by Seebeck effect, and causing cooling of electronic component by Peltier effect using electric power

摘要

The method involves placing two sensors (107, 108) in two zones (105, 106) of a turbojet (101), where temperature gradient is provided between the two zones. Electric power is generated from the sensors by Seebeck effect. Cooling of an electronic component is caused by Peltier effect using the electric power generated by the Seebeck effect. The electric power is stored into an electric power module (109). A turbine (104) and a compressor (102) are provided in the two zones of the turbojet.