A method of controlling at least a first pitch of a first propeller and a second pitch of a second propeller of a hybrid helicopter, the hybrid helicopter having a thrust control and a yaw control that are configured to generate orders for modifying respectively a mean pitch component and a differential pitch component of the first pitch and of the second pitch, the hybrid helicopter having a collective pitch control for modifying a collective pitch component of main blades of the lift rotor. The method includes a step of: keeping with the control system the first pitch and the second pitch within a control domain that varies as a function of information relating to the collective pitch component.


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    Title :

    PROCÉDÉ DE COMMANDE D'HÉLICES D'UN HÉLICOPTÈRE HYBRIDE ET HÉLICOPTÈRE HYBRIDE


    Additional title:

    METHOD FOR CONTROLLING THE PROPELLERS OF A HYBRID HELICOPTER AND HYBRID HELICOPTER
    VERFAHREN ZUR STEUERUNG DER PROPELLER EINES HYBRIDHUBSCHRAUBERS UND HYBRIDHUBSCHRAUBER


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

    Publication date :

    2023-07-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    PROCEDE DE COMMANDE D'HELICES D'UN HELICOPTERE HYBRIDE ET UN HELICOPTERE HYBRIDE

    EGLIN PAUL / HUOT REMY | European Patent Office | 2023

    Free access


    procédé de commande d’hélices d’un hélicoptère hybride et un hélicoptère hybride.

    EGLIN PAUL / HUOT RÉMY | European Patent Office | 2022

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