Herein provided are methods and systems for producing reverse thrust in a multi-engine propeller aircraft, comprising: obtaining, at a first engine controller of a first engine of the aircraft, a first power request for the first engine for producing reverse thrust; determining, at the first engine controller, a first blade angle for a first propeller coupled to the first engine; obtaining, at the first engine controller and from a second engine controller of a second engine of the aircraft, a second power request for the second engine and a second blade angle for a second propeller coupled to the second engine; and when the second power request is indicative of a request for producing reverse thrust and when the first and second blade angles are beyond a predetermined threshold, commanding, via the first engine controller, the first engine to produce reverse thrust based on the first power request.


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    Titel :

    REVERSE THRUST IN MULTI-ENGINE PROPELLER AIRCRAFT


    Weitere Titelangaben:

    INVERSION DE POUSSEE DANS UN AERONEF A HELICES MULTIMOTEURS


    Beteiligte:
    CHAHAL JASRAJ (Autor:in) / LISIO CARMINE (Autor:in) / MCGRATH DARRAGH (Autor:in) / ZINGARO GIANCARLO (Autor:in)

    Erscheinungsdatum :

    2020-04-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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