An active laminar flow control arrangement may comprise a modular arrangement comprising a plurality of frames and cover panels coupled to an outer skin (312) having a plurality of hat stiffeners (340) and stringers. A first cover panel (324a) may be coupled between a first frame (322a) and a first hat stiffener (340a). A second cover panel (324c) may be coupled between a second frame (322b) and a second hat stiffener (340b). A third cover panel (324b) may be coupled between the first cover panel (324a) and the second cover panel (324c). The cover panels may enclose associated plenums (325) whereby a flow of air is pumped into the arrangement for maintaining a laminar flow across an aerodynamic surface of the outer skin (312).


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    Titel :

    ACTIVE LAMINAR FLOW CONTROL STRUCTURAL PLENUMS FASTENED


    Weitere Titelangaben:

    STRUKTURELLE SAMMELKAMMERSTÜTZE FÜR AKTIVE LAMINARSTRÖMUNGSSTEUERUNG
    PLÉNUMS STRUCTURAUX FIXES DE COMMANDE DE FLUX LAMINAIRE ACTIF


    Beteiligte:

    Erscheinungsdatum :

    28.09.2022


    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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    Active laminar flow control structural plenums fastened

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    Szabo, B. A. / Actis, R. L. / SAE | British Library Conference Proceedings | 1999


    LIGHTWEIGHT COMBINED DUCTWORK/PLENUMS FOR SPACE APPLICATIONS

    CARROLL GALEN DUFF | Europäisches Patentamt | 2016

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