The invention belongs to the technical field of flight equipment, and discloses a wing body overturning structure which comprises a first wing and a second wing. The second wing is provided with at least two power assemblies, the second wing is provided with a joint between the two farthest power assemblies, and the joint is rotationally connected with one end of the first wing through a rotating assembly. The requirements of vertical take-off and landing and efficient cruising of the flight equipment can be met, and the reliability of the turnover mechanism to the overall structure of the flight equipment is effectively improved. Based on the wing body turnover mechanism, the invention further discloses a wing, and based on the wing, the invention further discloses an unmanned aerial vehicle.

    本发明属于飞行设备技术领域,公开了一种翼身翻转结构,包括第一机翼和第二机翼;所述第二机翼设有至少两个动力组件,所述第二机翼于相隔最远的两个动力组件之间具有连接处,该连接处通过转动组件与第一机翼的一端转动连接。本发明能够实现飞行设备垂直起降与高效巡航的要求,并有效提高翻转机构对飞行设备整体结构的可靠性。基于上述翼身翻转机构,本发明还公开了一种机翼,基于该机翼,本发明还公开了一种无人机。


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    Titel :

    Wing body overturning structure, wing and unmanned aerial vehicle


    Weitere Titelangaben:

    一种翼身翻转结构、机翼、无人机


    Beteiligte:
    HE BIN (Autor:in) / HENG LEE KWANG (Autor:in) / DU YAHUI (Autor:in)

    Erscheinungsdatum :

    29.07.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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