An electric motor includes a stator having a first side and a second side, a first housing coupled to the first side of the stator, and a second housing coupled to the second side of the stator. A shaft of the electric motor has a first end and a second end. The shaft is rotatably supported by a first bearing and a second bearing. A propeller of the electric motor couples to the first end of the shaft. An inverter includes an inverter housing directly coupled to the first housing.


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    Title :

    AIRCRAFT ELECTRIC MOTOR WITH COOLING SYSTEM


    Contributors:

    Publication date :

    2025-04-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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