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Single-rotor helicopter having a compound anti-torque system, and a method of countering the torque induced by said single rotor

机译:具有复合反扭矩系统的单旋翼直升机,以及一种抵消由所述单旋翼引起的扭矩的方法

摘要

A helicopter comprising: a single main rotor for forwards motion and for support; and an anti-torque system comprising: an auxiliary, anti- torque rotor rotated from the engine means of said main rotor and exerting controllable anti-torque lateral thrust; and at least one steering airfoil that is controllable in steering and that generates anti- torque transverse lift. According to the invention, the helicopter includes automatic swivel control means for automatically controlling the swivel angle of said steering airfoil as a function of the collective pitch angle of said main rotor and of the forward speed of said helicopter.
机译:一种直升机,包括:单个主旋翼,用于向前运动和支撑;一种抗扭矩系统,包括:辅助抗扭矩转子,从所述主转子的发动机装置旋转并施加可控的抗扭矩横向推力;至少一个转向方向盘可控,并且产生反扭矩横向升力。根据本发明,直升机包括自动旋转控制装置,该自动旋转控制装置根据所述主旋翼的总俯仰角和所述直升机的前进速度来自动地控制所述转向翼型的旋转角。

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