A sandwich panel for an aircraft includes a lower top layer, an upper top layer and a core layer, wherein the core layer in turn includes pins. The pins extend from a lower top layer in the direction of the upper top layer, and the pins are interconnected by rods. In addition, the rods run inside the core layer, and the pins and rods form a one-piece network.


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    Titel :

    SANDWICH PANEL FOR AN AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    13.10.2016


    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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