Patent ID: 11912427
Assignee: HAMILTON SUNDSTRAND CORPORATION
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC B  F  Y | IPC B  F

Claim 9:
10. A method of managing heat of an electronic device on an aircraft engine comprising:
pumping a coolant through a passage of a body coupled to a generator power electronics module, housed in a belly fairing of the aircraft;
transferring heat from the electronic device to the coolant within the passage of the body;
pumping the coolant through an out-cooling line;
cooling the coolant within the cooling line;
pumping the coolant to a generator, housed within an engine nacelle of the aircraft;
transferring heat from the generator to the coolant;
transferring heat from the coolant to a first fluid within a heat exchanger; and
pumping the coolant through a return-cooling line.