The present invention discloses a motor, a gimbal including the motor and an aircraft including the gimbal. The motor includes a base, a rotation shaft, a stator assembly, a first bearing, a stator bearing and a rotor assembly that is used for driving an external member to rotate. The rotation shaft has a first end portion, a second end portion and a middle portion connecting the first end portion to the second end portion. The base is connected to the first end portion by using the first bearing. The rotor assembly is connected to the middle portion. The stator bearing, the rotor assembly and the first bearing are sequentially arranged along an axial direction of the rotation shaft. The stator assembly is connected to the rotation shaft by using the stator bearing. The present invention can reduce a torque force that is generated by a rotation shaft and that is transmitted to an external member, thereby improving movement stability of the external member, and additionally reduce a time loss of movement on the rotation shaft, thereby increasing a speed at which the external member responds to motor movement.


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    Titel :

    MOTOR, PAN-TILT, AND AIRCRAFT


    Weitere Titelangaben:

    MOTOR, SCHWENK-NEIGUNG UND FLUGZEUG
    MOTEUR, PANORAMIQUE HORIZONTAL-VERTICAL ET AÉRONEF


    Beteiligte:
    ZHANG ZHENGLI (Autor:in) / CHEN FAZHAN (Autor:in)

    Erscheinungsdatum :

    04.09.2024


    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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