Herein provided are methods and systems for controlling operation of a first propeller (120) of an aircraft, the first propeller (120) associated with a first engine (110), the aircraft further comprising a second propeller (170) associated with a second engine (160). A first requested engine power for the first engine (110) is obtained. A second requested engine power for the second engine (160) is obtained. The first propeller (120) is synchronized with the second propeller (170) by setting a first propeller command for the first propeller (120) based on the first and second requested engine power, and the first propeller command is sent for the first propeller (120).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SINGLE LEVER CONTROL IN TWIN TURBOPROPELLER AIRCRAFT


    Weitere Titelangaben:

    EINHEBELSTEUERUNG IN FLUGZEUG MIT ZWEI TURBOPROPELLERN
    COMMANDE À LEVIER UNIQUE DANS UN AÉRONEF À DOUBLE TURBOPROPULSEUR


    Beteiligte:
    LISIO CARMINE (Autor:in)

    Erscheinungsdatum :

    29.08.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    SINGLE LEVER CONTROL IN TWIN TURBOPROPELLER AIRCRAFT

    LISIO CARMINE | Europäisches Patentamt | 2018

    Freier Zugriff

    SINGLE LEVER CONTROL IN TWIN TURBOPROPELLER AIRCRAFT

    LISIO CARMINE | Europäisches Patentamt | 2018

    Freier Zugriff

    Single lever control in twin turbopropeller aircraft

    LISIO CARMINE | Europäisches Patentamt | 2018

    Freier Zugriff

    SINGLE LEVER POWERPLANT CONTROL ON TWIN TURBOPROPELLER AIRCRAFT

    LISIO CARMINE | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRCRAFT TURBOPROPELLER

    VLASTUIN JONATHAN | Europäisches Patentamt | 2016

    Freier Zugriff