There is provided an exhaust mixer arrangement for a turbofan engine having a bypass passage for channelling a bypass flow and a core passage for channelling a core flow around a central axis. The exhaust mixer arrangement comprises a mixer body mounted for rotation about the central axis. The mixer body has an annular wall extending around the central axis. The annular wall defines a plurality of circumferentially distributed alternating inner and outer lobes, with each inner lobe protruding into the core passage, and each outer lobe protruding into the annular bypass passage. A driving unit is operatively connected to the mixer body for selectively driving the mixer body in rotation about the central axis. A controller is operatively connected to the driving unit for controlling a rotational speed of the mixer body as a function of a flight operating condition.


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    Titel :

    ROTATABLY DRIVEN EXHAUST MIXER


    Weitere Titelangaben:

    MELANGEUR D~ECHAPPEMENT ENTRAINE EN ROTATION


    Beteiligte:
    LABRECQUE MICHEL (Autor:in) / NGUYEN KEVIN (Autor:in)

    Erscheinungsdatum :

    27.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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