The invention discloses an unmanned aerial vehicle torque arm rotor mechanism which comprises a fixed base, a transmission cavity is formed in the fixed base, a rotor shaft is rotationally connected to the middle of the transmission cavity, a rotor head is connected to the end, extending out of the fixed base, of the rotor shaft, and a driving motor is connected to the left side wall of the inner cavity of the transmission cavity. The power output end of the driving motor is connected with a bevel gear, the outer wall of the rotor shaft is connected with a bevel gear ring, the bevel gear ring is in meshed connection with the bevel gear, the outer wall of the fixed base is connected with a controller, and the controller is provided with a wireless communication module. The mechanism is reasonable in structural design and convenient to operate, reduces the manufacturing cost, can guarantee stable lifting of the unmanned aerial vehicle, and is suitable for popularization and promotion.
本发明公布了一种无人机扭力臂旋翼机构,包括固定座,所述固定座内设有传动腔,所述传动腔的中部转动连接有旋翼轴,所述旋翼轴伸出固定座的一端连接有旋翼头,所述传动腔的内腔左侧壁连接有驱动电机,所述驱动电机的动力输出端连接有锥齿轮,所述旋翼轴的外壁连接有锥齿圈,所述锥齿圈啮合连接锥齿轮,所述固定座的外壁连接有控制器,所述控制器上设有无线通信模块;本发明结构设计合理,操作方便,降低了制作成本,能够保障无人机的稳定升降,适合进行普及推广。
Unmanned aerial vehicle torque arm rotor mechanism
一种无人机扭力臂旋翼机构
2021-09-10
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2024
|European Patent Office | 2023
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