The invention relates to a control device for an engine, comprising means (150) for calculating a blade pitch angle setpoint (160) of at least one propeller of the engine, the calculating means (150) using a propeller performance model, taking into account at least one flight speed (115) in order to adapt a blade pitch angle setpoint by taking into account a shaft horsepower setpoint.


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    Titel :

    Control device for an engine


    Beteiligte:

    Erscheinungsdatum :

    2015-09-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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