The invention relates to the technical field of aircraft folding rudders, and discloses an aircraft control surface folding mechanism and an aircraft, the aircraft control surface folding mechanism comprises a base, a control surface and a self-locking assembly, the base is rotatably connected to the base in the length direction of the control surface and has a folding position and an unfolding position relative to the base, and a mounting cylinder is arranged on the side, close to the base, of the control surface; a spiral groove is formed in the mounting cylinder; the self-locking assembly comprises a lock seat, a lock rod and a pin, the lock seat is arranged on the base, a guide hole is formed in the lock seat, the lock rod is contained in the mounting cylinder and tends to be away from the lock seat, one end of the lock rod is slidably arranged in the guide hole in a sleeved mode, and the pin is connected to the other end of the lock rod and penetrates through the spiral groove. The aircraft comprises an aircraft body and the aircraft control surface folding mechanism, the practicability and flexibility are good, and the flight stability is high.

    本发明涉及飞行器折叠舵技术领域,公开一种飞行器舵面折叠机构及飞行器,飞行器舵面折叠机构包括底座、舵面和自锁组件,底座绕舵面的长度方向转动连接于底座并相对底座具有折叠位和展开位,舵面靠近底座的一侧设置有安装筒,安装筒上开设有螺旋槽;自锁组件包括锁座、锁杆和销钉,锁座设置在底座上,锁座上开设有导向孔,锁杆容纳在安装筒内并具有远离锁座的趋势,锁杆的一端滑动套设在导向孔中,销钉连接于锁杆的另一端,并穿过螺旋槽。飞行器包括机身和飞行器舵面折叠机构,实用性和灵活性较佳,飞行稳定性较高。


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    Title :

    Aircraft control surface folding mechanism and aircraft


    Additional title:

    一种飞行器舵面折叠机构及飞行器


    Contributors:
    DU SHUANG (author) / MA HUAIBO (author) / XUE SHIMING (author) / DUAN XIANGJIE (author) / WANG LI (author) / ZHANG HUI (author) / HUANG YIMING (author) / HUANG WEI (author)

    Publication date :

    2024-01-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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