A blade stringer for a composite panel having an inside surface includes a proximal section, comprising a web attached to and extending approximately perpendicularly from the inside surface of the panel, and a free distal end. The web has a thickness and a height, and includes a plurality of continuous composite plies. The free distal end has a plurality of local plies interleaved and co-cured with the continuous plies, the distal end defining a bulb having a thickness that is greater than the web thickness and less than about a third of the web height.


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    Titel :

    LAMINATED I-BLADE STRINGER


    Beteiligte:
    TIEN ALLAN (Autor:in) / REUSCH DAVID C (Autor:in) / HART MARCUS C (Autor:in) / SOUKSAMRANE SAMSON (Autor:in)

    Erscheinungsdatum :

    2015-08-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS



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