The invention relates to the technical field of unmanned aerial vehicles, and discloses a foldable multi-wing unmanned aerial vehicle system suitable for a polar region environment. The four folding assemblies are arranged on the front side, the rear side, the left side and the right side of the unmanned aerial vehicle body correspondingly; the wing assembly is arranged at the end, away from the unmanned aerial vehicle body, of the folding assembly and used for being matched with the folding assembly to complete folding action; the flight control module is arranged in the unmanned aerial vehicle body and located at the top of the unmanned aerial vehicle body, the flight control module is connected with the folding assembly and the wing assembly, and the flight control module is used for controlling the flight state of the unmanned aerial vehicle; the temperature control module is arranged in the unmanned aerial vehicle body; the number of the landing racks is two, the two landing racks are obliquely arranged at the bottom of the unmanned aerial vehicle body in the vertical direction, and the top ends of the landing racks are connected with the unmanned aerial vehicle body. According to the invention, reliable and efficient flight performance and stable operation in an extreme environment are realized.
本发明涉及无人机技术领域,公开了一种适用于极地环境下可折叠的多机翼无人机系统,该系统包括:无人机机身;折叠组件,具有四组,无人机机身的前侧、后侧、左侧、右侧均设有一组折叠组件;机翼组件,设置在折叠组件远离无人机机身的一端,机翼组件用于与折叠组件配合完成折叠动作;飞行控制模块,设置在无人机机身的内部,且位于无人机机身的顶部,飞行控制模块与折叠组件和机翼组件相连,飞行控制模块用于控制无人机的飞行状态;温度控制模块,设置在无人机机身的内部;降落架,具有两个,两个降落架沿竖直方向倾斜设置在无人机机身的底部,降落架的顶端与无人机机身相连。本发明实现了可靠、高效的飞行性能以及极端环境下的稳定运行。
Foldable multi-wing unmanned aerial vehicle system suitable for polar region environment
一种适用于极地环境下可折叠的多机翼无人机系统
2025-03-25
Patent
Electronic Resource
Chinese
IPC: | B64U |
Downwards foldable-type multi-rotor wing unmanned aerial vehicle
European Patent Office | 2015
|European Patent Office | 2024
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