To provide a motor having a structure capable of suppressing vibration of a rotor to which a propeller is detachably mounted.SOLUTION: A motor 10 mounted on an unmanned aerial vehicle includes a rotor 20, having a propeller mounting unit 70 to which a propeller 2 can be detachably mounted, rotatable around a central axis, and a stator 30 facing the rotor in a radial direction through a gap, and an auto balancer 60 capable of automatically correcting the dynamic balance of the rotor.SELECTED DRAWING: Figure 2

    【課題】プロペラが着脱可能に取り付けられたロータの振動を抑制できる構造を有するモータを提供する。【解決手段】無人飛行体に搭載されるモータ10は、プロペラ2が着脱可能に取り付けられるプロペラ取付部70を有し、中心軸を中心として回転可能なロータ20と、ロータと隙間を介して径方向に対向するステータ30と、ロータの動バランスを自動で修正可能なオートバランサ60と、を備える。【選択図】図2


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    Titel :

    MOTOR, ROTOR BLADE DEVICE, AND UNMANNED AERIAL VEHICLE


    Weitere Titelangaben:

    モータ、回転翼装置、および無人飛行体


    Beteiligte:
    TAKEMOTO SHINJI (Autor:in) / MIZUIKE HIROTOMO (Autor:in) / SASAGURI KEISHI (Autor:in)

    Erscheinungsdatum :

    08.10.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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