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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    Title :

    COMPOSITE REINFORCEMENT STRUCTURES AND AIRCRAFT ASSEMBLIES COMPRISING COMPOSITE REINFORCEMENT STRUCTURES


    Contributors:
    AUTRY BRENDEN (author) / WILLIAMS BRYAN (author) / MORI MAURO (author) / CHAPMAN MARK (author)

    Publication date :

    2018-02-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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