A nacelle is provided for an aircraft propulsion system. This nacelle includes an outer barrel and an active laminar flow control system. The active laminar flow control system includes an array of perforations in the outer barrel, a suction source and a drain mechanism. The suction source is fluidly coupled with the array of perforations. The drain mechanism is fluidly coupled with and between the array of perforations and the suction source.


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    Titel :

    ACTIVE LAMINAR FLOW CONTROL SYSTEM WITH DRAINAGE


    Beteiligte:
    PUJAR VIJAY V (Autor:in) / BROWN KEITH T (Autor:in)

    Erscheinungsdatum :

    23.03.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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