The invention discloses a reconfigurable combined unmanned aerial vehicle, which particularly relates to the technical field of aerodynamic design of aircrafts. A reconfigurable combined unmanned aerial vehicle comprises nine unmanned aerial vehicle single bodies, the nine unmanned aerial vehicle single bodies are arranged in two rows, the number of the unmanned aerial vehicle single bodies located in the front row is four, and the number of the unmanned aerial vehicle single bodies located in the rear row is five. The unmanned aerial vehicle single bodies located in the front row are connected to the heads of the unmanned aerial vehicle single bodies located in the rear row through winglets. According to the technical scheme, the problem that the small unmanned aerial vehicle is short in voyage endurance is solved, and the aerodynamic performance of the small unmanned aerial vehicle can be improved.
本发明专利公开了一种可重构的组合式无人飞行器,具体涉及飞行器气动设计的技术领域。一种可重构的组合式无人飞行器,包括九架无人机单体,九架所述无人机单体分两排设置,位于前排的所述无人机单体数量为四架,位于后排的所述无人机单体数量为五架,位于前排的所述无人机单体通过翼梢小翼连接在位于后排的无人机单体的头部。采用本发明技术方案解决了小型无人机航程航时短的问题,可用于增加小型无人机的气动性能。
Reconfigurable combined unmanned aerial vehicle
一种可重构的组合式无人飞行器
2021-10-22
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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