The invention belongs to the technical field of aircrafts, and particularly relates to a tilting mechanism of an aircraft, the aircraft and a working method thereof, the tilting mechanism comprises an arm, a tilting assembly arranged at the front end of the arm and a power assembly for driving the tilting assembly to tilt around the arm; the tilting assembly comprises a first motor and rotating blades connected to an output shaft of the first motor. A fixed support extending towards the machine arm is convexly arranged on one end face, deviating from the rotating paddle, of the first motor, a rotating space is formed in the position, corresponding to the fixed support, of the machine arm, a rotating shaft is arranged in the rotating space, and a shaft hole corresponding to the rotating shaft is formed in the fixed support; the power assembly is arranged below the fixed support, connected with the first motor and used for pushing the tilting assembly. The problem of motion interference can be solved, it is guaranteed that the vehicle arms have enough strength and are high in reliability, interference external force of air fluid can be effectively resisted, and flight safety is guaranteed from the tilting mechanism.
本发明属于飞行器技术领域,具体为一种飞行器的倾转机构、飞行器及其工作方法,包括机臂、设置在机臂前端的倾转组件以及驱动倾转组件绕机臂进行倾转运动的动力组件;倾转组件包括第一电机和连接在第一电机的输出轴上的旋转桨叶;第一电机背离旋转桨叶的一端面上凸设有向机臂方向延伸的固定支座,机臂上与固定支座对应的位置形成有转动空间,转动空间内布置有转轴,固定支座上设有与转轴对应的轴孔;动力组件设置在固定支座的下方,且与第一电机连接,用于推动倾转组件。本申请不但能够解决运动干涉的问题,保证机臂具有足够的强度,可靠性较高,而且能有效抵抗空气流体的干扰外力,从倾转机构本身保证飞行安全。
Tilting mechanism of aircraft, aircraft and working method of aircraft
一种飞行器的倾转机构、飞行器及其工作方法
08.11.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |