The invention discloses a ducted aircraft and an attitude control method thereof. The ducted aircraft comprises an aircraft body, a ducted fan and a tilting device, and the ducted fan is connected with the aircraft body; the tilting device is rotationally connected to the air outlet side of the ducted fan so that the posture of the machine body can be controlled by rotating the tilting device. The tilting device is arranged on the air outlet side of the ducted fan, air flow sprayed out of the air outlet side of the ducted fan generates lift force and resistance at the tilting device, the lift force and the resistance can be adjusted through rotation of the tilting device, then posture adjustment of the machine body is controlled, and the unmanned aerial vehicle is simple in structure, light in weight and low in cost.
本发明公开一种涵道飞行器及其姿态控制方法。其中,该涵道飞行器包括机体、涵道风扇以及倾转装置,涵道风扇与机体连接;倾转装置转动连接于涵道风扇的出风侧,以通过转动倾转装置控制机体的姿态。本发明通过在涵道风扇的出风侧设置倾转装置,从涵道风扇的出风侧喷出的气流,在倾转装置处产生升力和阻力,可以通过倾转装置的转动来调整升力和阻力,进而控制机体的姿态调整,本发明结构简单、重量轻、成本低。
Ducted aircraft and attitude control method thereof
涵道飞行器及其姿态控制方法
2024-03-01
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Ducted aircraft control structure and control method thereof
Europäisches Patentamt | 2021
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