首页> 外国专利> Helicopter with coaxial, contrarotating main rotors has at least three control drives at distance from main rotor axle; each control drive has rotor and drive device

Helicopter with coaxial, contrarotating main rotors has at least three control drives at distance from main rotor axle; each control drive has rotor and drive device

机译:具有同轴,反向旋转主旋翼的直升机在距主旋翼轴一定距离处至少具有三个控制驱动器;每个控制驱动器都有转子和驱动装置

摘要

The helicopter (1) has at least two main rotors (2,3) mounted coaxially with respect to each other on a main rotor axle and at least one drive device (4,5) that drives the main rotors to rotate in contrarotation. It also has at least three control drives (7,10,11) that are provided at a distance from the main rotor axle (15). Each control drive has a rotor and a drive device. An independent claim is also included for a method of controlling helicopters.
机译:直升机(1)具有相对于彼此同轴安装在主旋翼轴上的至少两个主旋翼(2,3)和驱动该主旋翼反向旋转的至少一个驱动装置(4,5)。它还具有至少三个控制驱动器(7、10、11),它们与主转子轴(15)相距一定距离。每个控制驱动器都有一个转子和一个驱动装置。还包括关于直升机控制方法的独立权利要求。

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