The invention relates to a method for controlling a hybrid helicopter and a hybrid helicopter. The hybrid helicopter has at least one lift rotor (10), at least one advancing propeller (15) and an empennage provided with at least one empennage active surface (26). The method comprises the steps of determining, by means of a main sensor (50), a current value of a rotor parameter that determines a current power consumed by the lift rotor (10), determining, by means of an estimator (76), a current setpoint of the rotor parameter, determining, by means of the estimator (76), the current power consumed by the lift rotor (10) as a function of the current value and the current setpoint. And the position of the tail wing movable surface (26) is adjusted through a steering adjuster (77).

    本发明涉及混合动力直升机的控制方法及混合动力直升机,该混合动力直升机具有至少一个升力旋翼(10)、至少一个前进螺旋桨(15)和设有至少一个尾翼活动面(26)的尾翼。该方法包括以下步骤:通过主传感器(50)确定旋翼参数的当前值,该旋翼参数决定了所述升力旋翼(10)消耗的当前功率,通过估量计(76)确定所述旋翼参数的当前设定点,根据所述当前数值和所述当前设定点,通过转向调节器(77)调节所述尾翼活动面(26)的位置。


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    Titel :

    Hybrid power helicopter control method and hybrid power helicopter


    Weitere Titelangaben:

    混合动力直升机的控制方法及混合动力直升机


    Beteiligte:
    EGLIN PAUL (Autor:in) / HUOT R ¨ (Autor:in) / MI (Autor:in) / EMBACH MARTIN (Autor:in)

    Erscheinungsdatum :

    14.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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