A method and apparatus are provided. The apparatus comprises a composite stringer having a flange configured to contact a composite skin. The flange comprises a first region comprising tapered plies, a second region comprising tapered plies, and a first end. The first end is configured to extend to an edge of the composite skin.


    Access

    Download


    Export, share and cite



    Title :

    Stringer flange extending to composite skin edge


    Contributors:

    Publication date :

    2018-03-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse



    Skin-stringer design for composite wings

    BALABANOV VLADIMIR / WECKNER OLAF / WU YUAN-JYE et al. | European Patent Office | 2019

    Free access

    SKIN-STRINGER DESIGN FOR COMPOSITE WINGS

    BALABANOV VLADIMIR / WECKNER OLAF / WU YUAN JYE et al. | European Patent Office | 2016

    Free access

    Skin-stringer design for composite wings

    BALABANOV VLADIMIR / WECKNER OLAF / WU YUAN-JYE et al. | European Patent Office | 2019

    Free access

    SKIN/STRINGER DESIGN FOR COMPOSITE WING

    VLADIMIR BALABANOV / OLAF WECKNER / WU YUAN-JYE et al. | European Patent Office | 2016

    Free access

    SKIN-STRINGER DESIGN FOR COMPOSITE WINGS

    BALABANOV VLADIMIR / WECKNER OLAF / WU YUAN-JYE et al. | European Patent Office | 2021

    Free access