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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    Title :

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


    Contributors:
    EGLIN PAUL (author) / HUOT REMY (author) / CONROY ANTOINE (author)

    Publication date :

    2023-04-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    METHOD FOR CONTROLLING AT LEAST ONE AERODYNAMIC STABILIZER MEMBER OF A HYBRID HELICOPTER, AND A HYBRID HELICOPTER

    EGLIN PAUL / HUOT REMY / CONROY ANTOINE | European Patent Office | 2021

    Free access



    HELICOPTER STABILIZER

    KOZULIN ANTON SERGEEVICH / VOROBEV GRIGORIJ OLEGOVICH | European Patent Office | 2020

    Free access

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

    EGLIN PAUL / HUOT REMY | European Patent Office | 2021

    Free access