The present invention provides an electric aircraft motor having a cooling structure, which minimizes rotational resistance of a rotating cylinder and improves the performance of introducing outside air into the motor by applying an engraved outside air inflow structure to an outer surface of the rotating cylinder of an outer rotor type. The electric aircraft motor having a cooling structure comprises: a fixed shaft; a rotating cylinder rotatably coupled to the fixed shaft; a stator provided on the fixed shaft; and a rotor provided on the rotating cylinder.

    본 발명은 전기로부터 회전력을 얻어 추력을 발생시키는 전기 비행기용 모터에 관한 것으로, 더욱 상세하게는 모터의 회전 저항을 최소화하면서도 모터의 냉각 성능을 향상시키는 냉각 구조를 갖는 전기 비행기 용 모터에 관한 것이다.


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    Titel :

    Electric Aircraft Motor having Cooling Device


    Weitere Titelangaben:

    냉각 구조를 갖는 전기 비행기 용 모터


    Beteiligte:
    CHANG JAE WON (Autor:in) / KIM MYUNG JAE (Autor:in)

    Erscheinungsdatum :

    28.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64U / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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