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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    Titel :

    AIRCRAFT ELECTRIC MOTOR WITH COOLING SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    10.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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