The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with foldable wings, which comprises a fuselage, the wings are mounted at the top of the fuselage, the wings comprise inner wings, the inner wings are fixedly mounted at the top of the fuselage, and outer wings are arranged at the ends of the inner wings. A driving mechanism is arranged between the outer wing and the inner wing, and the driving mechanism is used for driving the outer wing to be folded and overturned. The method has the effect of improving the problem that the occupied space of the unmanned aerial vehicle is too large.

    本申请涉及无人机的技术领域,尤其是涉及一种可折叠机翼的无人机,其包括机身,所述机身的顶部安装有机翼,所述机翼包括内翼,所述内翼固定安装在所述机身的顶部,所述内翼的端部设置有外翼,所述外翼与所述内翼之间设置有驱动机构,所述驱动机构用于驱动所述外翼折叠翻转。本申请具有改善无人机存方占用空间过大的问题的效果。


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    Titel :

    Unmanned aerial vehicle with foldable wings


    Weitere Titelangaben:

    一种可折叠机翼的无人机


    Beteiligte:
    SONG WENHAO (Autor:in) / HAO CHUNYAN (Autor:in) / LIU HUIYING (Autor:in)

    Erscheinungsdatum :

    11.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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