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).


    Access

    Download


    Export, share and cite



    Title :

    ACTIVE LAMINAR FLOW CONTROL STRUCTURAL PLENUMS FASTENED


    Additional title:

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


    Contributors:

    Publication date :

    2022-09-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    ACTIVE LAMINAR FLOW CONTROL STRUCTURAL PLENUMS FASTENED

    SANZ MARTINEZ PABLO T / SCHRELL JOHANN STEVEN / PAOLINI THOMAS | European Patent Office | 2020

    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


    Fastened Joint Design

    Waters.W.A. | Automotive engineering | 1978


    LIGHTWEIGHT COMBINED DUCTWORK/PLENUMS FOR SPACE APPLICATIONS

    CARROLL GALEN DUFF | European Patent Office | 2016

    Free access