The invention provides an aircraft empennage quick release structure which comprises a first connecting piece and a second connecting piece, the first connecting piece comprises a first bottom plate, a sliding assembly installed on the first bottom plate and a lock hook connected with the sliding assembly, and the sliding assembly can make the lock hook move in the first direction; the second connecting piece comprises a second bottom plate, a pressing assembly installed on the second bottom plate and a lock sleeve connected with the pressing assembly, the lock sleeve is matched with the lock hook, the pressing assembly can make the lock sleeve move in the second direction, and the second direction is perpendicular to the first direction. The invention further provides an unmanned aerial vehicle empennage. The unmanned aerial vehicle empennage comprises an inverted-V-shaped empennage composed of a first empennage and a second empennage and the aircraft empennage quick release structure. A first connecting piece and a second connecting piece in the quick release structure for the empennage of the aircraft are fixedly mounted on a first empennage and a second empennage respectively. The empennage can be rapidly mounted and dismounted without tools, and the use requirement for flexible and rapid dismounting and mounting of a light and small unmanned aerial vehicle in an external field is met.
本发明提供一种飞行器尾翼快拆结构,包括第一连接件和第二连接件,第一连接件包括第一底板、安装在第一底板上的滑移组件以及与滑移组件相连的锁钩,滑移组件能使锁钩沿第一方向移动;第二连接件包括第二底板、安装在第二底板上的按压组件以及与按压组件相连的锁套,锁套与锁钩相匹配,且按压组件能使锁套沿第二方向移动,第二方向与第一方向垂直。还提供一种无人机尾翼,包括由第一尾翼和第二尾翼构成的倒V型尾翼以及上述飞行器尾翼快拆结构;其中飞行器尾翼快拆结构中的第一连接件、第二连接件分别固定安装在第一尾翼、第二尾翼上。本发明可以免工具快速实现尾翼的安装和拆卸工作,满足了轻小型无人机外场灵活快速拆装的使用要求。
Quick release structure for empennage of aircraft and empennage of unmanned aerial vehicle
一种飞行器尾翼快拆结构及无人机尾翼
2022-11-15
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |