The unmanned aerial vehicle comprises a shell, a rotor wing, an undercarriage and a first driving assembly, the rotor wing is arranged on the shell in a foldable mode, the undercarriage is arranged at the bottom of the shell in a foldable mode, and the first driving assembly is in driving fit with the rotor wing and the undercarriage. According to the unmanned aerial vehicle, the foldable rotor wings and the landing gear are arranged on the shell, so that the rotor wings and the landing gear can be stored in the shell when not used, the shell can protect the rotor wings and the landing gear, the size of the unmanned aerial vehicle can be reduced, the first driving assembly drives the rotor wings and the landing gear to be unfolded and folded, and the unmanned aerial vehicle is more convenient to use. And the space utilization rate of the vehicle can be improved.
本发明公开了一种无人机、无人机总成和车辆,无人机包括:壳体、旋翼、起落架和第一驱动组件,旋翼可折叠地设置于所述壳体上,起落架可折叠地设置于所述壳体的底部,第一驱动组件分别与旋翼和起落架驱动配合。通过在壳体上设置可折叠地旋翼和起落架,这样设置可以使旋翼和起落架在不使用时收纳在壳体中,从而可以使壳体对旋翼和起落架进行保护,还可以减小无人机的体积,而且第一驱动组件驱动旋翼和起落架进行展开和收缩,进而可以提升车辆的空间利用率。
Unmanned aerial vehicle, unmanned aerial vehicle assembly and vehicle
无人机、无人机总成和车辆
2024-08-13
Patent
Electronic Resource
Chinese
IPC: | B64U |
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