The invention discloses a vertical lifting fixed-wing unmanned aerial vehicle. Comprising a body; the wings are connected to the two sides of the fuselage; the lifting systems are arranged on the wings on the two sides of the fuselage, and the lifting systems can generate thrust in the vertical direction; the propelling systems are arranged on the wings on the two sides of the fuselage, and the propelling systems can change the thrust directions of the propelling systems, so that the propelling systems have a first state when providing lifting force in the vertical direction and a second state when providing thrust in the horizontal direction; wherein the vertical lifting fixed-wing unmanned aerial vehicle has a lifting state when the propelling system is in the first state and a cruising state when the propelling system is in the second state, and when the vertical lifting fixed-wing unmanned aerial vehicle is in the lifting state, at least one of the propelling system and the lifting system provides lifting force in the vertical direction. The vertical lifting fixed-wing unmanned aerial vehicle has high safety performance, and safe landing of the unmanned aerial vehicle can be ensured when part of power fails.
本发明公开了一种垂直升降固定翼无人机。包括:机身;机翼,机身的两侧均连接有机翼;升降系统,机身两侧的机翼上均设有升降系统,且升降系统能够产生竖直方向上的推力;推进系统,机身两侧的机翼上均设有推进系统,推进系统能够改变其推力方向,以使推进系统具有提供竖直方向上的升力时的第一状态和提供水平方向上的推力时的第二状态;其中,垂直升降固定翼无人机具有推进系统处于第一状态时的升降状态和推进系统处于第二状态时的巡航状态,并且垂直升降固定翼无人机处于升降状态时,推进系统和升降系统其中至少一个提供竖直方向上的升力。本发明的垂直升降固定翼无人机具有较高的安全性能,在部分动力失效时能够确保无人机安全降落。
Vertical lifting fixed-wing unmanned aerial vehicle
垂直升降固定翼无人机
2023-09-05
Patent
Electronic Resource
Chinese
IPC: | B64U |
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