The invention discloses an unmanned aerial vehicle and a control surface dismounting and mounting structure, and belongs to the field of aircraft structure design, the control surface dismounting and mounting structure is provided with a quick-release pin device, and the quick-release pin device is composed of a plug pin, a spring, a fixing flange, a clamping groove frame, an end rib guide hole and the like, so that quick dismounting and mounting of a control surface can be realized; the control surface dismounting structure is simple in structure and convenient to use, can be quickly dismounted and mounted without tools, is simple in dismounting and mounting processes, is reliable, can be used as a control surface static balance weight due to the additional structure weight, can be used for conveniently and quickly replacing the control surface independently under the condition that the control surface is damaged, and has very high practical application value.

    本发明公开了一种无人机及舵面拆装结构,属于航空飞行器结构设计领域,该舵面拆装结构通过设置快卸销装置,通过插销、弹簧、固定法兰、卡槽框和端肋引导孔等结构构成的快卸销装置,不仅可以实现舵面的快速拆卸和安装,而且在不借助工具的情况下也能实现快速拆装,拆卸和安装过程简单,该舵面拆装结构可靠,附加结构重量可作为舵面静平衡配重使用,该舵面拆装结构解决了在舵面受损的情况下可便捷快速地单独更换舵面,具有很强的实际应用价值。


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    Title :

    Unmanned aerial vehicle and control surface dismounting and mounting structure


    Additional title:

    一种无人机及舵面拆装结构


    Contributors:
    LIU TENGDA (author) / HEI LIJIE (author) / GAO GUAN (author) / WANG YUQING (author) / ZENG PENG (author)

    Publication date :

    2023-05-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U





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