The invention discloses a wing folding mechanism, an unmanned aerial vehicle and a wing folding method of the unmanned aerial vehicle. The wing folding mechanism comprises a fixing part, a folding part, an elastic hinge assembly, a first locking part and a second locking part. One end of the elastic hinge assembly is connected to the end part of the fixed part, and the other end of the elastic hinge assembly is connected to the fixed end of the folding part; the first locking part is mounted on the fixing part, and the second locking part is mounted on the folding part; when the folding part is folded on the fixing part, the second locking part is locked on the first locking part, and the elastic piece on the elastic hinge assembly is in an elastic deformation state. The unmanned aerial vehicle comprises the wing folding mechanism. The fixed part is an inner wing, the folding part is an outer wing, one end of the fixed part away from the elastic hinge assembly is connected with a fuselage, and the folding axis of the outer wing is perpendicular to the extension direction of the leading edge of the wing. The folding structure solves the problems that in the prior art, a folding structure is large in weight and installation space.
本申请公开了一种机翼折叠机构、无人机及其机翼折叠方法,该机构包括固定部、折叠部、弹性铰链组件、第一锁紧部、以及第二锁紧部;弹性铰链组件的一端连接于固定部的端部,弹性铰链组件的另一端连接于折叠部的固定端;第一锁紧部安装于固定部上,第二锁紧部安装于折叠部上;折叠部折叠于固定部上时,第二锁紧部锁紧于第一锁紧部,弹性铰链组件上的弹性件为弹性形变状态。该无人机包括上述的机翼折叠机构;固定部为内机翼,折叠部为外机翼,固定部远离弹性铰链组件的一端用于与机身连接,外机翼的折叠轴线的方向垂直于机翼前缘的延伸方向。本申请解决了现有技术中的折叠结构均存在重量大和安装空间大的问题。
Wing folding mechanism, unmanned aerial vehicle and wing folding method of unmanned aerial vehicle
一种机翼折叠机构、无人机及其机翼折叠方法
2023-08-04
Patent
Electronic Resource
Chinese
IPC: | B64U |
Unmanned aerial vehicle wing folding mechanism and unmanned aerial vehicle
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