The invention discloses a vertical take-off and landing fixed-wing unmanned aerial vehicle which comprises a vehicle body and two vehicle arms, wherein the two vehicle arms are connected to the two sides of the vehicle body respectively, and the two vehicle arms and the vehicle body are integrally formed. According to the vertical take-off and landing fixed-wing unmanned aerial vehicle, the two vehicle arms and the vehicle body are integrated, the vehicle body is fused with the vehicle arms, and the mounting structures of the vehicle arms are reduced, so that the overall weight of the verticaltake-off and landing fixed-wing unmanned aerial vehicle is reduced, and the purpose of improving flight endurance is achieved. Meanwhile, the overall rigidity and strength of the vehicle bodyand thevehicle arms are enhanced, and the safety and stability of the vertical take-off and landing fixed-wing unmanned aerial vehicle are greatly improved.
本发明公开了一种垂直起降固定翼无人机,其包括机身和两个机臂,两个所述机臂分别连接于所述机身的两侧,且两个所述机臂与所述机身之间一体成型。本发明的垂直起降固定翼无人机,通过将两个机臂与机身一体化,利用机身融合机臂,减少机臂的安装结构,从而减轻垂直起降固定翼无人机的整体重量,达到提升飞行航时目的。同时,增强机身与机臂的整体刚度强度,大大提高了垂直起降固定翼无人机的安全稳定性。
Vertical take-off and landing fixed-wing unmanned aerial vehicle
垂直起降固定翼无人机
2020-10-30
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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