The invention relates to a multi-rotor aircraft equipped with continuously variable transmissions. The multi-rotor aircraft comprises a flight power source, at least three rotors and at least two continuously variable transmissions. According to the invention, the connection mode of the rotors, the continuously variable transmissions and the flight power source is specifically set, so that the control requirement on the flight power source of the multi-rotor aircraft is reduced, and the overall control tends to be simple; the specific arrangement mode of the continuously variable transmissionsis limited, and particularly, the structural characteristics of a continuously variable transmission chain and a speed regulation cam are specifically set, so that the continuously variable transmissions are more suitable for being assembled on the multi-rotor aircraft, and the performance and controllability of the multi-rotor aircraft are integrally improved.
本发明涉及一种装备无级变速器的多旋翼飞行器,包括飞行动力源、至少三个旋翼以及至少两个无级变速器。通过对旋翼与无级变速器以及飞行动力源的连接方式进行具体设置,使得该多旋翼飞行器降低了对飞行动力源的控制要求,并且可使整体的控制趋于简单;通过对无级变速器的具体设置方式进行限定,尤其是对无级变速链和调速凸轮的结构特征进行具体设置,使得该无级变速器更加适应装备于多旋翼飞行器,从而整体提升多旋翼飞行器的性能和可操控性。
A multi-rotor aircraft equipped with continuously variable transmissions
一种装备无级变速器的多旋翼飞行器
2021-01-08
Patent
Electronic Resource
Chinese
Continuously- variable transmissions.
Automotive engineering | 1975
Lubrication of continuously variable transmissions
Automotive engineering | 1998
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