The invention discloses a control surface suspension structure for an unmanned aerial vehicle, a wing and the unmanned aerial vehicle. The control surface suspension structure comprises a connecting rib and a suspension shaft, wherein a mounting groove is formed in the top of the connecting rib; and the suspension shaft comprises a fixing section and a supporting section which are connected with each other, the fixing section is detachably arranged in the mounting groove, and the supporting section extends to the outer side of the connecting rib and is used for mounting the control surface. According to the control surface suspension structure, the assembly complexity can be effectively reduced, the assembly efficiency is improved, and the maintainability of the control surface is improved.

    本发明公开一种用于无人机的舵面悬挂结构、机翼及无人机,包括:连接肋,连接肋的顶部设有安装槽;悬挂轴,悬挂轴包括相互连接的固定段和支撑段,固定段可拆卸的设置于安装槽中,支撑段延伸至连接肋外侧,用于安装舵面。本发明的舵面悬挂结构能够有效的降低装配复杂度,提高装配效率,提高舵面的可维护性。


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    Titel :

    Control surface suspension structure for unmanned aerial vehicle, wing and unmanned aerial vehicle


    Weitere Titelangaben:

    用于无人机的舵面悬挂结构、机翼及无人机


    Beteiligte:
    WANG GUANGBO (Autor:in) / LEI LI (Autor:in) / XU TAO (Autor:in) / YAN DELI (Autor:in)

    Erscheinungsdatum :

    28.01.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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