Apparatus and methods provide for utilizing continuous curved composite stringers to control the loads and corresponding moments within curved regions of an aircraft or other vehicle without delamination or other interlamina failures. According to embodiments described herein, any number of tapered height curved composite stringers may be coupled to continuous skin components to create a curved continuous panel. The tapered height curved composite stringers may have webs that taper to a reduced height within curved regions and corresponding base flanges that widen during web tapering. Reinforcement fittings may be coupled to the base flanges in the curved regions for further strengthening and to provide for the attachment of supplemental panels to the stringers.


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    Titel :

    TAPERED HEIGHT CURVED COMPOSITE STRINGERS AND CORRESPONDING PANELS


    Weitere Titelangaben:

    FASERVERBUNDPANEL AUFWEISEND VERJÜNGTE UND GEBOGENE STRINGERS
    PANEL AVEC LISSES EFFILÉS ET COURBES


    Beteiligte:
    KWON HYUKBONG (Autor:in) / NELSON PAUL E (Autor:in) / WELTE BEN CHRISTOPHER (Autor:in) / LEE KARL B (Autor:in)

    Erscheinungsdatum :

    2017-10-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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