A structural component, including a composite tapered wing spar including a first fiber layer and a main web, wherein respective longitudinal axes of fibers making up the first layer at least substantially lying on a plane corresponding to the main web of the wing spar are curved over at least most of the respective lengths of the fibers.


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    Title :

    LATERAL PLY LAYUP OF COMPOSITE SPAR


    Contributors:

    Publication date :

    2016-02-11


    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



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