A nacelle is provided for an aircraft propulsion system. The nacelle may include an outer barrel and an active laminar flow control system. The active laminar flow control system may include a plurality of suction sources and a plurality of arrays of perforations in the outer barrel. The active laminar flow control system may be configured with a plurality of zones. Each of the zones may include a respective one of the suction sources which is fluidly coupled with a respective one of the arrays of perforations in the outer barrel.


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    Titel :

    MULTI-ZONE ACTIVE LAMINAR FLOW CONTROL SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM


    Beteiligte:
    BROWN KEITH T (Autor:in) / BYRNE STUART J (Autor:in) / KESTLER STEVEN M (Autor:in)

    Erscheinungsdatum :

    2016-12-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    MULTI-ZONE ACTIVE LAMINAR FLOW CONTROL SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM

    BROWN KEITH T / BYRNE STUART J / KESTLER STEVEN M | Europäisches Patentamt | 2019

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    Multi-zone active laminar flow control system for an aircraft propulsion system

    BROWN KEITH T / BYRNE STUART J / KESTLER STEVEN M | Europäisches Patentamt | 2018

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    Propulsion systems for laminar flow aircraft

    Connors, J.W. / Pfenninger, W. / Smith, C.B. | Engineering Index Backfile | 1961