The invention discloses a coaxial propeller-reversing unmanned aerial vehicle structure for launch lift-off and flying in a projectile form. The coaxial propeller-reversing unmanned aerial vehicle structure comprises a rack, a base, a driving assembly, a steering mechanism, a pop-up mechanism, a rotor wing and a balance rod. The base is located at the bottom, fixedly connected with the elastic shell and used for fixing the electronic device. The pop-up mechanism is connected with the base, the pop-up mechanism is connected with the pop-up part, and the pop-up mechanism acts to drive the pop-up part to move; the popping part comprises a rack, a driving assembly and a steering mechanism; the rack is used for bearing the driving assembly and the steering mechanism; the driving assembly is used for providing power to enable the upper and lower layers of rotors to rotate to provide lift force; and the steering mechanism is used for adjusting the blade pitch. The coaxial propeller-reversing unmanned aerial vehicle structure provided by the invention can be compressed into an elastic structure to be launched and launched and unfolded at a target position, so that the risks of being detected, intercepted and hit are reduced.
本发明公开了一种面向发射升空并以射弹形式飞行的共轴反桨无人机结构,包括机架、基座、驱动组件、转向机构、弹出机构、包括旋翼和平衡杆;基座位于底部与弹型壳体固定连接且用于固定固定电子器件;弹出机构与基座连接,弹出机构连接可弹出部分,弹出机构动作,带动可弹出部分运动;可弹出部分包括机架,驱动组件和转向机构;机架用于承载驱动组件和转向机构;驱动组件用于提供动力,使上下两层旋翼旋转提供升力;转向机构用于调节桨叶桨距。本发明提供的一种共轴反桨无人机结构,可以压缩为一个弹型结构用于发射升空并在目标位置展开,降低了被探测、拦截和打击的风险。
Launching-oriented coaxial propeller-reversing unmanned aerial vehicle structure
一种面向发射的共轴反桨无人机结构
2023-12-26
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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