The present invention relates to a system (10) for an aircraft (100), wherein the system comprises: an electric motor (12) configured for propulsion of the aircraft; at least one 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 by ram air cooling; 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.


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    Title :

    AEROSPACE ELECTRIC PROPULSION THERMAL MANAGEMENT SYSTEM


    Additional title:

    WÄRMEVERWALTUNGSSYSTEM FÜR ELEKTRISCHEN LUFTFAHRTANTRIEB
    SYSTÈME DE GESTION THERMIQUE DE PROPULSION ÉLECTRIQUE AÉROSPATIALE


    Contributors:

    Publication date :

    2025-08-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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