The invention relates to a nacelle structure (10) surrounding a blower, including an air inlet sleeve (100) having an inner surface (100A) defining an air supply channel; and at least one ring (22) arranged in said air inlet sleeve and selectively movable between a deployed position in which said ring is radially inwardly moved from the inner surface in order to provide an obstacle to the shock waves from the blower, and a retracted position in which the ring is radially outwardly moved from the deployed position such as to become flush with the inner surface and thus reconstitute the air supply channel.


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    Titel :

    Acoustically optimized air inlet sleeve


    Beteiligte:
    ROMANO PASCAL (Autor:in) / BONNEAU VIRGINIE (Autor:in) / SENSIAU CLAUDE (Autor:in)

    Erscheinungsdatum :

    23.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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