The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle wing and fuselage connecting structure and method. The unmanned aerial vehicle wing and fuselage connecting structure comprises a fuselage and wings, first mounting parts are arranged on the two sides of the fuselage, second mounting parts are arranged at the connecting ends of the wings, lock catch mechanisms are formed between the first mounting parts and the second mounting parts, and a guide reinforcing pipe sleeve is arranged on the periphery of the first mounting parts of the fuselage. The connection operation of the wings and the fuselage of the unmanned aerial vehicle is simple, the first mounting parts are additionally arranged on the fuselage, the second mounting parts are additionally arranged on the wings, and the lock catch mechanisms are formed between the first mounting parts and the second mounting parts, so that quick locking can be performed, quick assembly connection can be realized by matching with the limiting of the guide reinforcing pipe sleeve, and the realization of intelligent automatic modular assembly is facilitated; and when the wings are damaged due to accidental falling, the wings can be quickly replaced without overall replacement, so that the use cost is relatively low.
本发明属于无人机技术领域,具体涉及一种无人机机翼与机身连接结构及方法,包括机身和机翼,所述机身的两侧设有第一安装部,所述机翼的连接端设有第二安装部,所述第一安装部和第二安装部之间形成有锁扣机构,所述机身位于第一安装部的外围设有导向加强管套。本发明无人机机翼与机身连接操作简单,通过在机身增设第一安装部,在机翼增设第二安装部,并使得第一安装部和第二安装部之间形成锁扣机构,可进行快速锁合,再配合导向加强管套的限位即可实现快速装配连接,利于智能自动模块化装配的实现;当机翼因意外跌落出现损坏后,能够快速对其进行更换,无需整体更换,使用成本较低。
Unmanned aerial vehicle wing and fuselage connecting structure
一种无人机机翼与机身连接结构及方法
2022-01-28
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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