The invention discloses a folding four-rotor unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The quad-rotor unmanned aerial vehicle comprises a vehicle shell, an upper center plate and a lower center plate are arranged in the vehicle shell from top to bottom, a plurality of vehicle arm seats are arranged between the upper center plate and the lower center plate at intervals, a folding part is arranged on one side of each vehicle arm seat, one end of each folding part is hinged to the corresponding vehicle arm seat, and the other end of each folding part is hinged to the corresponding vehicle arm seat. The other end of the folding piece is provided with a machine arm, the other end of the machine arm is provided with a motor, the output end of the motor is provided with a wing, the wing is arranged at the output end of the motor in a foldable mode, and a pod is arranged below the machine shell. The folding type four-rotor unmanned aerial vehicle can solve the problem that an existing folding type four-rotor unmanned aerial vehicle is large in size after being folded.
本发明公开了一种折叠式四旋翼无人机,属于无人机技术领域。所述四旋翼无人机包括机壳,所述机壳内部由上而下设置有上中心板和下中心板,所述上中心板与所述下中心板之间间隔设置有多个机臂座,每个所述机臂座的一侧设置有折叠件,所述折叠件的一端与对应的所述机臂座相铰接,所述折叠件的另一端设置有机臂,所述机臂的另一端设置有电机,所述电机的输出端设置有机翼,所述机翼可折叠地设置于所述电机的输出端,所述机壳的下方设置有吊舱。本发明能够解决现有的折叠式四旋翼无人机折叠后体积较大的问题。
Folding four-rotor unmanned aerial vehicle
折叠式四旋翼无人机
2023-06-13
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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