A system (10) for an aircraft (100), including an electric motor (12) configured for propulsion of the aircraft; a motor control unit (14); a first fluid cooling circuit (16) arranged to circulate a first fluid (18a-c) and comprising at least one first cooling channel (20) in the at least one motor control unit; a first heat exchanger (22) connected to the first fluid cooling circuit for providing cooling to the first fluid cooling circuit; a ram air inlet (24) arranged to provide cooling to the first heat exchanger; a second fluid cooling circuit (26) arranged to circulate a second fluid (28a-b) and comprising at least one second cooling channel (30) in the electric motor; and a second heat exchanger (32), wherein the first fluid cooling circuit is arranged to provide cooling or heating to the second fluid cooling circuit via the second heat exchanger.
AEROSPACE ELECTRIC PROPULSION THERMAL MANAGEMENT SYSTEM
31.07.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AEROSPACE ELECTRIC PROPULSION THERMAL MANAGEMENT SYSTEM
Europäisches Patentamt | 2025
|Springer Verlag | 2024
|TIBKAT | 1972
|Fusion-Electric Propulsion for Aerospace Plane Flight
British Library Conference Proceedings | 1993
|