The invention provides a wingtip connection unmanned aerial vehicle air docking mechanism based on an electric push rod, and the mechanism comprises a left docking mechanism which is provided with a docking groove and a locking assembly, and the locking assembly is arranged at the end part of the docking groove; the right butt-joint mechanism is provided with a right driving assembly and a butt-joint cone, the right driving assembly can drive the butt-joint cone to stretch out or retract, and in the stretching-out state, the butt-joint cone is arranged in the butt-joint groove and abuts against the locking assembly; and in the retraction state, the butt joint cone is completely arranged in the right butt joint mechanism. According to the invention, a mode that a plurality of fixed-wing unmanned aerial vehicles are relatively static and wing tip rib parts are in local motion butt joint is adopted, so that simultaneous butt joint of the plurality of fixed-wing unmanned aerial vehicles can be realized; according to the scheme, a butt joint/separation mechanism does not need to provide lateral force to realize mutual approaching of the unmanned aerial vehicles, so that the structural strength and the manufacturing process of the mechanism can be reduced to a certain extent.
本发明提供一种基于电推杆的翼尖连接无人机空中对接机构,包括:左对接机构,设置有对接槽和锁止组件,锁止组件设置在对接槽的端部;右对接机构,设置有右驱动组件和对接锥,右驱动组件能够驱动对接锥伸出或者缩回,且在伸出状态下,对接锥置于对接槽中并与锁止组件抵接;在缩回状态时,对接锥完全置于右对接机构内。本发明采用了多架固定翼无人机相对静止,机翼翼尖端肋部分局部运动对接的方式,可以实现多架固定翼无人机的同时对接;并且该方案由于不需要对接/分离机构提供侧向力实现无人机之间的互相靠近,因此可以在一定程度上降低该机构的结构强度及制造工艺。
Wingtip connection unmanned aerial vehicle air docking mechanism based on electric push rod and unmanned aerial vehicle
基于电推杆的翼尖连接无人机空中对接机构及无人机
2025-02-07
Patent
Electronic Resource
Chinese
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