The invention discloses a wing damping device and a fixed-wing unmanned aerial vehicle, and belongs to the field of unmanned aerial vehicles. The wing damping device comprises a fitting plate, a connecting plate and a roller, the surface of the fitting plate is detachably and fixedly connected to the section of the wing, the connecting plate is detachably and fixedly connected to the fitting plate, the roller is installed on the connecting plate, and the circumferential side wall of the rolling wheel protrudes out of the lower end of the connecting plate. The fixed-wing unmanned aerial vehicle comprises a fuselage and wings mounted on the fuselage, wing tips of the wings are provided with wing-shaped sections, and the wing damping devices are mounted on the wing-shaped sections. The device is simple in structure and reasonable in design, and can effectively reduce and even avoid loss caused by too large up-down vibration amplitude of the wings in the take-off and landing process.

    本发明公开了一种机翼减震装置及固定翼无人机,属于无人机领域。其中,机翼减震装置包括贴合板、连接板和滚轮;贴合板的表面可拆卸固定连接在机翼的剖面上,连接板可拆卸固定连接在贴合板上,滚轮安装在连接板上且滚轮的圆周侧壁凸出于连接板的下端。固定翼无人机则包括机身以及安装在机身上的机翼,机翼的翼梢设置有翼形剖面,翼形剖面上安装有上述的机翼减震装置。本发明结构简单且设计合理,能够有效的降低乃至避免机翼在起降过程中因上下振动幅度过大导致的损失。


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    Titel :

    Wing damping device and fixed-wing unmanned aerial vehicle


    Weitere Titelangaben:

    一种机翼减震装置及固定翼无人机


    Beteiligte:
    GONG BANGMIN (Autor:in) / AI JIANLIANG (Autor:in)

    Erscheinungsdatum :

    2021-07-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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