The invention discloses a folding type unmanned aerial vehicle wing assembly which comprises a main wing, an auxiliary wing and a folding assembly, the folding assembly at least comprises a driving part and a limiting part, the limiting part is arranged on the auxiliary wing and movably arranged on the driving part in a limited mode, and the driving part is used for driving the auxiliary wing to be folded. The occupied space during storage and transportation is reduced, and storage and carrying are facilitated.

    本发明公开了一种折叠式无人机机翼总成,包括主机翼、副机翼和折叠组件,所述折叠组件至少包括驱动件和限位件,所述限位件设置于副机翼,所述限位件可被限位的活动设置于驱动件上,所述驱动件用于驱动副机翼折叠,降低在储存运输时的占用空间,利于收纳和携带。


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    Titel :

    Folding type unmanned aerial vehicle wing assembly


    Weitere Titelangaben:

    折叠式无人机机翼总成


    Beteiligte:
    YU YANG (Autor:in) / XU SHULIN (Autor:in) / MAO YUEPENG (Autor:in) / YU TAO (Autor:in)

    Erscheinungsdatum :

    2021-09-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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