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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    Title :

    Y-SHAPED STRINGERS MADE OF COMPOSITE MATERIAL


    Additional title:

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



    Publication date :

    2025-05-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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