The invention discloses an ultramicro folding fixed-wing unmanned aerial vehicle which comprises a vehicle body. Wings are installed on the vehicle body, connecting shafts are connected into the wingsin a penetrating mode, clamping and locking shafts are installed on the wings, springs are connected to the outer sides of the clamping and locking shafts in a nested mode, and a first tail wing plate is installed at the rear end of the vehicle body. And a fixing rod is mounted on the first tail wing plate. According to the ultramicro folding fixed-wing unmanned aerial vehicle, a control system of the unmanned aerial vehicle is subjected to a chip integrated design, the system stability is greatly improved, meanwhile, the maintenance cost is greatly reduced, and efficiency is improved; compared with a microminiature rotorcraft of the same level, the ultramicro folding fixed-wing unmanned aerial vehicle has more function task choices, and a needed nacelle is mounted according to task requirements; and the ultramicro folding fixed-wing unmanned aerial vehicle is small in size, the wings and an empennage are designed to be a folding structure, and therefore the occupied space for storageis reduced, and the ultramicro folding fixed-wing unmanned aerial vehicle is convenient to store and carry and suitable for individual combat equipment.
本发明公开了一种超微小型折叠固定翼无人机,包括机身,所述机身上安装有机翼,且机翼的内部贯穿连接有连接轴,所述机翼上安装有卡锁轴,且卡锁轴的外侧嵌套连接有弹簧,所述机身的后端安装有第一尾翼板,所述第一尾翼板上安装有固定杆。该超微小型折叠固定翼无人机对无人机的控制系统进行芯片化集成设计,大大增加了系统稳定性,同时极大地降低了维护成本,提高效率;该超微小型折叠固定翼无人机,相比于同级别微小型旋翼机有更多的功能任务选择,根据任务需求,挂载所需吊舱;该超微小型折叠固定翼无人机,体积较小,并且机翼和尾翼部分设计为折叠结构,从而减小收纳的占用空间,便于收纳和携带,适合单兵作战装备。
Ultramicro folding fixed-wing unmanned aerial vehicle
一种超微小型折叠固定翼无人机
2021-03-30
Patent
Elektronische Ressource
Chinesisch
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