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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    Title :

    ACTIVE LAMINAR FLOW CONTROL STRUCTURAL PLENUMS FASTENED


    Contributors:

    Publication date :

    2020-04-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Active laminar flow control structural plenums fastened

    SANZ MARTINEZ PABLO T / SCHRELL JOHANN STEVEN / PAOLINI THOMAS | European Patent Office | 2022

    Free access

    ACTIVE LAMINAR FLOW CONTROL STRUCTURAL PLENUMS FASTENED

    SANZ MARTINEZ PABLO T / SCHRELL JOHANN STEVEN / PAOLINI THOMAS | European Patent Office | 2022

    Free access

    Analysis of fastened structural connections

    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


    Mathematical Models of Fastened Structural Connections

    Szabo, Barna A. / Actis, Ricardo L. | SAE Technical Papers | 1999