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 :

    PROCÉDÉ DE COMMANDE D'AU MOINS UN ORGANE AÉRODYNAMIQUE DE DÉRIVE D'UN HÉLICOPTÈRE HYBRIDE ET UN HÉLICOPTÈRE HYBRIDE


    Additional title:

    METHOD FOR CONTROLLING AT LEAST ONE AERODYNAMIC RUDDER OF A HYBRID HELICOPTER AND HYBRID HELICOPTER
    VERFAHREN ZUR STEUERUNG MINDESTENS EINES AERODYNAMISCHEN SEITENRUDERS EINES HYBRIDHUBSCHRAUBERS UND ENTSPRECHENDER HYBRIDHUBSCHRAUBER


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

    Publication date :

    2025-05-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge