An airfoil includes at least one precured composite spar (66, 68) having a web (82, 88) and at least one flange (84, 86, 90, 92) integrated with an end of the web (82, 88). A precured composite skin (74, 76) is attached to the spar (66, 68) by adhesive bonding the skin to the flange (84, 86, 90, 92). 7209158v1:PRW 672a FIG. 3 4 56 147 7490 '1 78 66 -' 72 84 82 92 78 > 70a '1-86 78 66 146 7 147 7 go68 70 104 84 7 106 82-- /88 70a 86 8 16 76 4 47 92 8


    Access

    Download


    Export, share and cite



    Title :

    Bonded composite airfoil and fabrication method


    Contributors:

    Publication date :

    2017-04-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Bonded composite airfoil and fabrication method

    NORDMAN PAUL STANLEY | European Patent Office | 2019

    Free access

    BONDED COMPOSITE AIRFOIL AND FABRICATION METHOD

    NORDMAN PAUL STANLEY | European Patent Office | 2017

    Free access

    BONDED COMPOSITE AIRFOIL AND FABRICATION METHOD

    European Patent Office | 2020

    Free access

    Bonded composite airfoil

    NORDMAN PAUL STANLEY | European Patent Office | 2016

    Free access

    Bonded-Plate Airfoil Construction

    Lawing, Pierce L. | NTRS | 1987