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


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    Titel :

    Active laminar flow control structural plenums fastened


    Beteiligte:

    Erscheinungsdatum :

    26.07.2022


    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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    BORTMAN, JACOB / SZABO, BARNA A. | AIAA | 1992


    Mathematical Models of Fastened Structural Connections

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


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