The invention provides a combined unmanned aerial vehicle wing body connecting structure and a combined unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles, the connecting structure comprises a wing body connecting piece, the bottom end of the wing body connecting piece is used for being rotationally connected to a fuselage of the unmanned aerial vehicle, and the top end of the wing body connecting piece is used for being connected with a wing of the unmanned aerial vehicle; the at least four wing lugs are used for being connected to a wing and are located on the peripheral side of the wing body connecting piece; the at least four fuselage lugs are used for being connected to the fuselage and located on the peripheral side of the wing body connecting piece, the wings can rotate relative to the fuselage, and when the wings are in an unfolded state, the at least four wing lugs and the at least four fuselage lugs can be attached to each other; the wing lugs and the fuselage lugs which are attached to each other are detachably connected. The unmanned aerial vehicle can be rapidly unfolded, and meanwhile load transmission between the wings and the fuselage can be achieved.
本发明提供一种组合式无人机翼身连接结构及组合式无人机,涉及无人机技术领域,该连接结构包括:翼身连接件,翼身连接件的底端用于转动连接在无人机的机身上,翼身连接件的顶端用于与无人机的机翼连接;至少四个机翼耳片,至少四个机翼耳片用于连接在机翼上,并位于翼身连接件的周侧;至少四个机身耳片,至少四个机身耳片用于连接在机身上,并位于翼身连接件的周侧,机翼能够相对于机身旋转,机翼处于展开状态时,至少四个机翼耳片分别与至少四个机身耳片能够相互贴靠在一起,相互贴靠的机翼耳片和机身耳片可拆卸连接。可以实现无人机快速展开,同时,也能够实现机翼与机身之间载荷的传递。
Combined unmanned aerial vehicle wing body connecting structure and combined unmanned aerial vehicle
一种组合式无人机翼身连接结构及组合式无人机
2024-03-26
Patent
Electronic Resource
Chinese
IPC: | B64U |
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