The invention relates to the technical field of unmanned aerial vehicles, in particular to a shell of an unmanned aerial vehicle and the unmanned aerial vehicle, the shell of the unmanned aerial vehicle comprises a shell body and a top cover, the top cover has an open state and a closed state relative to the shell body, and the top cover is switched from the closed state to the open state under the impact of a parachute opening process of a parachute module; in the open state, the top cover acts relative to the shell body so as to form an opening in the shell body, the opening is used for allowing a parachute of the parachute module to penetrate through the inner side of the shell body so as to be opened on the outer side of the shell body, and in the closed state, the top cover covers the opening. Through the design of the shell, the parachute module can be installed in the unmanned aerial vehicle shell, the integrity and the appearance effect of the unmanned aerial vehicle and the parachute module are improved, and the situation that the parachute module falls off from the unmanned aerial vehicle is also avoided.
本公开涉及无人机技术领域,尤其涉及一种无人机的壳体及无人机,无人机的壳体包括壳主体以及顶盖,其中,顶盖具有相对于壳主体的开启状态和封闭状态,顶盖在降落伞模组的开伞过程的冲击下自封闭状态切换至开启状态;在开启状态,顶盖相对于壳主体动作以在壳主体上形成开口,开口用于供降落伞模组的降落伞自壳主体的内侧穿过以在壳主体的外侧开启,在封闭状态,顶盖覆盖开口。本公开通过对壳体的设计能够使得降落伞模组安装在无人机壳体的内部,提高了无人机与降落伞模组的一体性以及外观效果,也避免了降落伞模组从无人机上脱落的情况发生。
Shell of unmanned aerial vehicle and unmanned aerial vehicle
无人机的壳体及无人机
03.01.2025
Patent
Elektronische Ressource
Chinesisch
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