The invention belongs to the technical field of unmanned aerial vehicles, and discloses a redundant limiting low-torsion full-freedom-degree unmanned aerial vehicle. The unmanned aerial vehicle comprises a lifting assembly used for providing spiral lifting force, a main machine plate used as structural support and an annular concave part located on the main machine plate, provided with four concave parts and used for containing the lifting assembly. A concentric first annular ring is pivoted in each annular concave part, concentric second annular rings are pivoted in the first annular rings, the first annular rings and the second annular rings are coaxially arranged to form a coaxial nested structure, and the lift assembly is assembled in the second annular rings; and gyroscope distribution structure. The redundant limiting low-torsion full-freedom-degree unmanned aerial vehicle is simple in mechanism, the structure is novel, and outstanding innovativeness is achieved.
本发明公开了一种冗余限位低扭全自由度无人机,属于无人机技术领域,包括作为用于提供螺旋升力的升力组件,包括作为结构支撑的主机机板,位于主机机板上具有四个凹陷的且作为容纳升力组件的环形凹陷部;位于每个环形凹陷部内枢接有同心的第一环形圈,位于第一环形圈内枢接有同心的第二环形圈,第一环形圈与第二环形圈同轴心设置形成同轴嵌套结构,所述的升力组件就配装在第二环形圈内;实现了陀螺仪分布结构。机构简洁,结构新颖,具备突出的创新性。
Redundant limiting low-torsion full-freedom-degree unmanned aerial vehicle
一种冗余限位低扭全自由度无人机
2020-04-14
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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