An air scoop assembly (72) that may be for a nacelle (60) of a turbofan engine (20) includes a surface (84) defining at least in-part a primary flowpath and a hood (74) formed to the surface and projecting into the primary flowpath. The hood includes a distal, leading, edge (82) that is irregular in shape thereby producing air vortices that shed from the leading edge and co-extend in a downstream direction with an airstream in the primary flowpath. The vortices are thereby controlled such that air flow disruption and undesired resonance is minimized or eliminated.


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    Titel :

    NACELLE AIR SCOOP ASSEMBLY


    Weitere Titelangaben:

    GONDELLUFTHAUBENANORDNUNG
    ENSEMBLE DE PRISE D'AIR DE NACELLE


    Beteiligte:

    Erscheinungsdatum :

    23.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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