The invention discloses a rotor unmanned aerial vehicle with separable and combinable vehicle arms. The unmanned aerial vehicle comprises a first rigid pressing rod, a second rigid pressing rod, a separable and combinable mechanism, a battery, rotor motors, propellers, an electronic speed controller and a flight control system. The first rigid pressing rod and the second rigid pressing rod are arranged side by side and are separably connected together through the separable and combined mechanism; the rotor motors and the batteries are symmetrically mounted on the first rigid pressing rod and the second rigid pressing rod; the rotor motors are electrically connected with the battery through the electronic speed controller and used for driving the propellers to rotate. And the flight control system is in signal connection with the separable and combined mechanism and the electronic speed controller. The unmanned aerial vehicle can be freely separated and combined, can provide high load capacity, and overcomes the defect that an existing unmanned aerial vehicle cannot be freely separated and deformed.
本发明公开了一种机臂可分离合并的旋翼无人机,该无人机包括第一刚性压杆、第二刚性压杆、可分离合并式机构、电池、旋翼电机、螺旋桨、电调以及飞控系统;所述第一刚性压杆与所述第二刚性压杆并排设置,并通过所述可分离合并式机构可分离地连接在一起;在所述第一刚性压杆和所述第二刚性压杆上对称安装有所述旋翼电机和所述电池;所述旋翼电机通过所述电调与所述电池电连接,用于驱动所述螺旋桨旋转;所述飞控系统与所述可分离合并式机构和所述电调信号连接。上述无人机可自由分离合并,并且能够提供较强的负载能力,克服了现有无人机不能自由分离变形的不足。
Rotor wing unmanned aerial vehicle with separable and combinable vehicle arms
一种机臂可分离合并的旋翼无人机
2024-07-09
Patent
Electronic Resource
Chinese
IPC: | B64U |
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