The invention discloses a light hanging device, an aircraft and a hanging method. The light hanging device comprises a self-locking mechanism. The self-locking mechanism comprises a shell, and a hook is arranged in the shell; the hook is rotationally connected to the shell close to the middle position, the bottom end is close to the bottom of the shell, the top end is close to the top of the shell, the bottom end of the hook makes contact with the bottom of the shell, and the top end of the hook is rotationally connected with the front end of a self-locking rod; the rear end of the self-locking rod is located on the side facing the bottom end of the hook, the rear end of the self-locking rod is hinged to the front end of a rocker, and the rear end of the rocker is rotationally connected to the shell. A limiting boss, a self-locking boss and a locking boss are arranged in the shell, the limiting boss is located above the rear end of the rocker, the locking boss is located at the front end of the self-locking rod, the self-locking boss is arranged between the rear end of the rocker and the locking boss, the position of the self-locking boss is lower than the connecting line of the locking boss and the rear end of the rocker, and the end, facing the self-locking boss, of the locking boss is obliquely arranged upwards. The device has the characteristics of simple structure, small size, light weight and high reliability.
本发明公开了一种轻型吊挂装置、飞行器及吊挂方法,包括自锁机构;自锁机构包括壳体,壳体内部设置有挂钩;挂钩靠近中间位置转动连接在壳体上,底端靠近壳体底部,顶端靠近壳体顶部,挂钩底端与壳体底部接触,挂钩顶端转动连接有自锁杆前端;自锁杆后端位于朝向挂钩底端一侧,自锁杆后端铰接有摇杆前端,摇杆后端转动连接在壳体上;壳体内设置有限位凸台、自锁凸台和锁闭凸台,限位凸台位于摇杆后端上方,锁闭凸台位于自锁杆前端,摇杆后端和锁闭凸台之间设置有自锁凸台,自锁凸台位置低于锁闭凸台和摇杆后端的连线,锁闭凸台朝向自锁凸台一端向上倾斜设置。具有结构简单、体积小、重量轻、可靠性高的特点。
Light hanging device, aircraft and hanging method
一种轻型吊挂装置、飞行器及吊挂方法
2024-05-10
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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