The invention provides a hovercar double-rotor system and a control method thereof, and relates to the technical field of hovercar rotors, the hovercar double-rotor system comprises a main rotor system and a standby rotor system, the standby rotor system comprises a plurality of blades, a propeller hub and an independent motor, the propeller hub is provided with a clamping groove, and the clamping groove is connected with the main rotor system. The plurality of paddles are vertically arranged with the propeller hub in an equidistant dispersion manner through the clamping grooves; the independent motor is arranged below the propeller hub, is electrically connected with the propeller hub and drives the propeller hub to drive the blades to rotate; the standby rotor wings are arranged at the four corners of a hovercar body, keep a silent state and do not participate in flight power output when the main rotor wing system works normally, and when the main rotor wing system breaks down or even fails, the hovercar main controller receives a failure signal and starts the standby rotor wing system, the standby rotor wing system drives the independent motor, and the standby rotor wing system drives the independent motor. And the propeller hub is driven to drive the blades to rotate.
本公开提供了一种飞行汽车双旋翼系统及其控制方法,涉及飞行汽车旋翼技术领域,包括主旋翼系统以及备用旋翼系统,所述备用旋翼系统包括多个桨叶、桨毂以及独立电机,桨毂上设置卡槽,多个桨叶通过卡槽与所述桨毂等距离分散垂直设置;所述独立电机设置在桨毂下方,并与所述桨毂电连接,驱动桨毂带动桨叶转动;所述备用旋翼设置飞行汽车车身四个角上,在主旋翼系统正常工作时保持静默状态,不参与飞行动力输出,当主旋翼系统发生故障乃至失效时,飞行汽车主控制器接收失效信号,启动备用旋翼系统,备用旋翼系统驱动独立电机,驱动桨毂带动桨叶转动。
Aerocar double-rotor system and control method thereof
一种飞行汽车双旋翼系统及其控制方法
2025-04-25
Patent
Electronic Resource
Chinese