The invention relates to the technical field of unmanned aerial vehicles, and particularly discloses a close-range coupling tandem wing layout unmanned aerial vehicle, which comprises a retainer, front positive lift wings, rear positive lift wings, a flight controller, propellers and an energy management system, the front positive lift force wings are fixedly arranged on the holder; the rear positive lift force wings are fixedly arranged on the holder, the rear positive lift force wings are located below the rear portions of the front positive lift force wings, and the rear positive lift force wings and the front positive lift force wings form a tandem wing layout; the propellers are positioned in front of the front positive lift wings; ailerons and elevators are arranged on the rear positive lift wings, and the ailerons and the elevators are electrically connected with the flight controller; according to the unmanned aerial vehicle with the close-range coupling tandem wing layout, two wings which can provide positive lift force are designed to be connected in series, and the aerodynamic performance of the whole vehicle is improved through the beneficial aerodynamic coupling effect.
本发明涉及无人飞行器技术领域,具体公开一种近距耦合串列翼布局的无人飞行器,包括保持架、前正升力机翼、后正升力机翼、飞行控制器、推进器和能源管理系统;所述前正升力机翼固定地配置在所述保持架上;所述后正升力机翼固定地配置在所述保持架上,所述后正升力机翼位于所述前正升力机翼的后下方,且所述后正升力机翼与所述前正升力机翼形成串列翼布局;所述推进器位于所述前正升力机翼的前方;所述后正升力机翼上设置有副翼和升降舵,所述副翼和升降舵均与所述飞行控制器电性连接;该近距耦合串列翼布局的无人飞行器设计有两个都能提供正升力的机翼串联,利用有利的气动耦合作用改善整机的气动性能。
Unmanned aerial vehicle with close-range coupled tandem wing layout
一种近距耦合串列翼布局的无人飞行器
2024-03-01
Patent
Electronic Resource
Chinese
IPC: | B64U |
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