The invention relates to a flight attitude adjusting device and an unmanned aerial vehicle, the flight attitude adjusting device comprises a first servo motor, an output shaft of the first servo motor is fixedly connected with a mounting seat, the mounting seat is rotatably connected with two first rotating shafts, the two first rotating shafts transversely extend, and one end of each first rotating shaft penetrates through the side wall of the mounting seat; the ends, away from the mounting base, of the two first rotating shafts are fixedly connected with propeller blades, angle adjusting assemblies are mounted between the two propeller blades and the mounting base correspondingly, and the two angle adjusting assemblies are used for adjusting the inclination angles between the two propeller blades and the horizontal plane correspondingly. The invention aims at providing the flight attitude adjusting device and the unmanned aerial vehicle to solve the problems that in the prior art, the attitude control of the unmanned aerial vehicle is realized by further adjusting the rotating speed of propeller blades by adjusting the rotating speed of a motor, the adjustable range is relatively small and the unmanned aerial vehicle is easy to collide with obstacles in a complex and changeable environment.
本发明涉及一种飞行姿态调节装置及无人机,包括第一伺服电机,所述第一伺服电机的输出轴上固定连接有安装座,所述安装座上转动连接有两根第一转轴,两根所述第一转轴横向延伸且一端贯穿安装座的侧壁,两根所述第一转轴远离安装座的一端固定连接有螺旋桨叶片,两个所述螺旋桨叶片与安装座之间均安装有角度调节组件,两个所述角度调节组件分别用于调节两个所述螺旋桨叶片与水平面之间的倾斜角度。目的在于提供一种飞行姿态调节装置及无人机,以解决现有技术中通过调整电机转速进一步调节螺旋桨叶片转速实现无人机姿态控制,在面对复杂多变的环境时,可调节的范围较小,容易撞击障碍物的问题。
Flight attitude adjusting device and unmanned aerial vehicle
飞行姿态调节装置及无人机
2025-02-14
Patent
Electronic Resource
Chinese
IPC: | B64U |
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