The invention relates to the technical field of unmanned aerial vehicles, and particularly discloses an unmanned aerial vehicle empennage. An unmanned aerial vehicle empennage comprises a left vertical tail assembly, a right vertical tail assembly and a horizontal tail assembly. The horizontal tail assembly comprises a horizontal wing, two front inserting pieces and two rear inserting pieces. The horizontal wing is provided with two side flat plates, a front inserting piece is fixed to the front portion of each side flat plate, and a rear inserting piece is fixed to the rear portion of each side flat plate. When the shifting plate is rotated, the protruding rod and the spring bolt can be driven to move along the limiting groove, so that the spring bolt leaves the front clamping groove, under the state that the rear inserting piece on each side is inserted into the bottom of the rear clamping groove, the horizontal wing is rotated, the front inserting piece on each side can be inserted into the bottom of the front clamping groove in a matched mode, and after the shifting plate is released, the spring bolt is inserted into the front clamping groove again to lock the front inserting piece in a matched mode. And meanwhile, the side flat plate on each side is attached to the outer plane, so that the two sides of the horizontal tail assembly are fixed to the two vertical tail assemblies. According to the unmanned aerial vehicle empennage of the structure, all the components are convenient to disassemble and assemble, the disassembly and assembly time is short, and the higher assembly time limit requirement is met.
本申请涉及无人机技术领域,具体公开一种无人机尾翼。一种无人机尾翼,包括左右两个垂尾组件和水平尾组件。水平尾组件包括水平翼、两个前插装件和两个后插装件。水平翼具有两个侧平板,每个侧平板的前部固定一个前插装件,每个侧平板的后部固定一个后插装件。转动拨板,能带动凸杆连同锁舌沿限位槽移动,使得锁舌离开前卡槽,在每一侧的后插装件插入后卡槽底部的状态下,转动水平翼,每一侧的前插装件能适配的插入前卡槽的底部,在放开拨板后,锁舌重新插入前卡槽而适配的封锁前插装件,同时每一侧的侧平板均贴合外平面,使得水平尾组件的两侧固定于两个垂尾组件。该结构的无人机尾翼,各部件拆装方便,拆装时间短,适应较高的组装时限性要求。
Unmanned aerial vehicle empennage
一种无人机尾翼
2024-12-06
Patent
Electronic Resource
Chinese
IPC: | B64U |