A method for optimizing the operation of at least one first propeller and of at least one second propeller of a hybrid helicopter. The method comprises the following step during a control phase: deflection, with an autopilot system, of at least one aerodynamic stabilizer member into a setpoint position having, with respect to a reference position, a target deflection angle that is a function of a setpoint deflection angle, the setpoint deflection angle being calculated by the autopilot system in order to compensate for a torque exerted by the lift rotor at zero sideslip.


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    Titel :

    Method for controlling at least one aerodynamic stabilizer member of a hybrid helicopter, and a hybrid helicopter


    Beteiligte:
    EGLIN PAUL (Autor:in) / HUOT REMY (Autor:in) / CONROY ANTOINE (Autor:in)

    Erscheinungsdatum :

    2023-04-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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    EGLIN PAUL / HUOT REMY / CONROY ANTOINE | Europäisches Patentamt | 2021

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    METHOD OF CONTROLLING PROPELLERS OF A HYBRID HELICOPTER, AND A HYBRID HELICOPTER

    EGLIN PAUL / HUOT REMY | Europäisches Patentamt | 2021

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