A composite reinforcement structure including a first skin having a first end and a second end and a second skin having a first end and a second end. The first end of the first skin and the first end of the second skin are coupled. A corrugated spar is disposed between the first skin and the second skin and is bonded to the first skin and the second skin.


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    Titel :

    COMPOSITE REINFORCEMENT STRUCTURES AND AIRCRAFT ASSEMBLIES COMPRISING COMPOSITE REINFORCEMENT STRUCTURES


    Beteiligte:
    AUTRY BRENDEN (Autor:in) / WILLIAMS BRYAN (Autor:in) / MORI MAURO (Autor:in) / CHAPMAN MARK (Autor:in)

    Erscheinungsdatum :

    2018-02-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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