Herein provided are methods and systems for controlling operation a first propeller of an aircraft, the first propeller associated with a first engine, the aircraft further comprising a second propeller associated with a second engine. A first requested engine power for the first engine is obtained. A second requested engine power for the second engine is obtained. The first propeller is synchronized with the second propeller by setting a first propeller command for the first propeller based on the first and second requested engine power, and the first propeller command is sent for the first propeller.


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    Titel :

    SINGLE LEVER CONTROL IN TWIN TURBOPROPELLER AIRCRAFT


    Weitere Titelangaben:

    COMMANDE A LEVIER SIMPLE DESTINEE A UN AERONEF A DOUBLE TURBOPROPULSEUR


    Beteiligte:
    LISIO CARMINE (Autor:in)

    Erscheinungsdatum :

    2018-08-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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