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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    Titel :

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


    Weitere Titelangaben:

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


    Beteiligte:
    EGLIN PAUL (Autor:in) / HUOT RÉMY (Autor:in)

    Erscheinungsdatum :

    12.07.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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    EGLIN PAUL / HUOT REMY | Europäisches Patentamt | 2023

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

    EGLIN PAUL / HUOT RÉMY | Europäisches Patentamt | 2022

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