A Y-shaped stringer (100) made of composite material for a panel (1010) of an aircraft, the Y-shaped stringer (100) comprising a stringer web (110) having a cross-section in a I-shape, first and second flanges (130a, 130b) configured to be connectable to the composite panel of the aircraft, an open triangular shape structure (120) comprising first and second lower vertices (120a, 120b) respectively joined to the first and second flanges (130a, 130b) and an upper vertex (120c) connected to a first end of the stringer web (110), wherein the open triangular shape structure (120) and the stringer web (110) form a cross-section in a Y-shape.


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    Titel :

    Y-SHAPED STRINGERS MADE OF COMPOSITE MATERIAL


    Weitere Titelangaben:

    Y-FÖRMIGE STRINGER AUS VERBUNDWERKSTOFF
    LISSES EN Y EN MATÉRIAU COMPOSITE



    Erscheinungsdatum :

    14.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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