The invention provides a wing folding structure of a small unmanned aerial vehicle. The wing folding structure of the small unmanned aerial vehicle comprises a main wing, an auxiliary wing and a folding connecting device, wherein the main wing is fixedly connected with an unmanned aerial vehicle body, and the auxiliary wing is connected with the main wing through the folding connecting device. Thefolding connecting device comprises a first connecting piece fixedly connected with one end of the main wing, a second connecting piece fixedly connected with one end of the auxiliary wing, and a plurality of elastic protrusions fixedly connected with the first connecting piece and the second connecting piece respectively. The wing folding structure of a small unmanned aerial vehicle has the beneficial effects that through the arrangement of the main wing and the auxiliary wing, the whole wing of the unmanned aerial vehicle can be formed; through the arrangement of the folding connecting device, the main wing and the auxiliary wing can be fixedly connected together in use, and the main wing and the auxiliary wing can be folded together when not in use.
本发明提供了一种小型无人机的机翼折叠结构,该小型无人机的机翼折叠结构包括:主机翼、副机翼、以及折叠连接装置;所述主机翼与无人机机身固定连接,所述副机翼通过所述折叠连接装置与所述主机翼相连接;所述折叠连接装置包括与所述主机翼的一端固定连接的第一连接片、与所述副机翼的一端固定连接的第二连接片、以及分别与所述第一连接片和所述第二连接片固定连接的多个弹性凸起。本发明的有益效果是:通过设置的主机翼和副机翼,可以组成无人机的整体机翼;通过设置的折叠连接装置,可以在使用时将主机翼和副机翼固定连接在一起,不使用时将主机翼和副机翼折叠在一起。
Wing folding structure of small unmanned aerial vehicle
一种小型无人机的机翼折叠结构
2020-09-01
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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