The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle attitude adjusting mechanism which comprises a fuselage and four flight assemblies, an arc-shaped through hole is formed in the side of the fuselage, a connecting rod, a mounting plate and a second adjusting assembly are arranged in the fuselage, a supporting frame is hinged to the middle of each flight assembly, and a first adjusting assembly is arranged on each mounting plate. The connecting rod is driven by the first adjusting assembly to slide in the arc-shaped through hole, so that the flight assembly on the connecting rod is obliquely arranged forwards or backwards, the unmanned aerial vehicle moves forwards or backwards, the mounting plate is driven by the second adjusting assembly to move left and right, and the first adjusting assembly is driven by the mounting plate to move. The connecting rod is driven to move through the first adjusting assembly, so that the flight assembly on the connecting rod is arranged in a left-right inclined mode, the unmanned aerial vehicle moves leftwards or rightwards, and the problems that an existing unmanned aerial vehicle attitude adjusting mode is prone to being affected by the wind environment, the attitude of the unmanned aerial vehicle is difficult to adjust, and falling is likely to happen are solved.
本发明涉及无人机技术领域,具体涉及一种无人机姿态调整机构,包括机身和四个飞行组件,机身的旁侧设有弧形通孔,机身的内部设有连接杆,安装板和第二调整组件,飞行组件的中部铰设有支撑架,安装板上设有第一调整组件,通过第一调整组件带动连接杆在弧形通孔中滑动,以使该连接杆上的飞行组件进行向前或向后倾斜设置,从而使无人机进行前进或后退移动,通过第二调整组件带动安装板左右移动,通过安装板带动第一调整组件移动,通过第一调整组件带动连接杆移动,以使连接杆上的飞行组件进行左右倾斜设置,从而使无人机进行向左或向右移动,解决了现有的无人机姿态调整方式,容易受风力环境影响,使无人机的姿态难以调整,易发生坠落的问题。
Unmanned aerial vehicle attitude adjusting mechanism and adjusting method
一种无人机姿态调整机构及调整方法
2023-11-10
Patent
Electronic Resource
Chinese
IPC: | B64U |
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