The invention discloses an empennage folding mechanism of folding-wing unmanned aerial vehicle. The empennage folding mechanism comprises a fixed part, a torsional spring, a fixed part gland and a rotary movable part, the rotary movable part is connected into the fixed part in a sleeved mode, the torsional spring is connected into the rotary movable part in a sleeved mode, one end of the torsionalspring is fixedly connected with the middle of the fixed part, and one end of the rotary movable part is connected with the middle part of the fixed part gland in a penetrating manner. The folding mechanism is simple in structure, convenient to install, small in occupied space, capable of being used when the empennage is rotated and folded along a certain rotating shaft of any plane of the fuselage and wider in application range, in the using process, the empennage can be rapidly unfolded under the torsion effect of the torsion spring, the unfolding efficiency of the empennage is effectivelyimproved, and extra electric losses are avoided.
本发明公开了一种折叠翼无人机的尾翼折叠机构,包括固定件、扭簧、固定件压盖和旋转活动件,所述固定件的内部套设连接有旋转活动件,所述旋转活动件的内部套设连接有扭簧,所述扭簧的一端与固定件的中部固定连接,所述旋转活动件的一端与固定件压盖的中部穿插连接。本发明结构简单、安装方便、占用空间少,可在尾翼沿机身任意平面的某旋转轴旋转折叠时使用,适用范围更大,在使用过程中,尾翼会在扭簧的扭力作用下快速展开,有效的提高尾翼的展开效率,且没有额外电损失。
Empennage folding mechanism of folding-wing unmanned aerial vehicle
一种折叠翼无人机的尾翼折叠机构
2021-02-26
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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