An aircraft system (36) includes a housing (80) having an outer surface (83) and an inner surface (85) defining a cavity (87). A motor (89) is arranged in the cavity. The motor includes a heat producing component (93) mounted to the inner surface. A first cooling system (102) is configured to direct a first heat exchange fluid in a first thermal exchange relationship with the heat producing component and a second cooling system (104) is configured to direct a second heat exchange fluid in a second thermal exchange relationship with the heat producing component. The second heat exchange fluid is distinct from the first heat exchange fluid and the second thermal exchange relationship is distinct from the first thermal exchange relationship.


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    Title :

    CABIN AIR COOLING SYSTEM


    Additional title:

    KABINENLUFTKÜHLSYSTEM
    SYSTÈME DE REFROIDISSEMENT D'AIR DE CABINE


    Contributors:

    Publication date :

    2023-10-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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