A method comprises embedding tear straps in a metal aircraft structure having a fully formed contour and thickness. The tear straps include strips of fibers that are substantially stronger and stiffer than the metal aircraft structure. The fibers are embedded beneath at least one surface of the metal aircraft structure via ultrasonic consolidation.


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    Titel :

    Embedded tear straps in metal structures


    Beteiligte:
    NORDMAN PAUL S (Autor:in)

    Erscheinungsdatum :

    2018-08-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B23K Löten , SOLDERING OR UNSOLDERING



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