Disclosed is an unmanned aerial vehicle thrust device. According to one embodiment of the present invention, the unmanned aerial vehicle thrust device includes: an independent multiphase motor generating thrust of an unmanned aerial vehicle; and a driving unit receiving the thrust from the independent multiphase motor and driving the unmanned aerial vehicle, wherein the independent multiphase motor includes: a housing which becomes a body; a shaft transmitting power to the driving unit; a fixing pin coupling the shaft to the housing; a coil generating a magnetic field when an electric current flows; and a connector formed in a pin type and supplied with electricity.

    무인항공기 추력 장치가 개시된다. 본 발명의 일실시예에 따른 무인항공기 추력 장치는 무인항공기의 추력을 발생시키는 독립다상모터 및 상기 독립다상모터로부터 추력을 인가 받아 상기 무인항공기를 구동하는 구동부를 포함할 수 있으며, 상기 독립다상모터는 몸체가 되는 하우징, 동력을 상기 구동부에 전달하는 샤프트, 상기 하우징과 샤프트를 결합하는 고정핀, 전류가 흐르는 경우, 자기장을 발생하는 코일 및 핀 타입으로 구성되어 전기를 공급받는 커넥터를 포함할 수 있다.


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    Titel :

    UNMANNED AERIAL VEHICLE THRUST DEVICE


    Weitere Titelangaben:

    무인항공기 추력 장치


    Beteiligte:
    SONG HONG TAE (Autor:in) / KANG SEONG SIG (Autor:in) / OH JOO HYEONG (Autor:in) / KANG BYUNG JOO (Autor:in)

    Erscheinungsdatum :

    2019-09-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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