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.


    Access

    Download


    Export, share and cite



    Title :

    SANDWICH PANEL FOR AN AIRCRAFT


    Contributors:

    Publication date :

    2016-10-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Aircraft interior sandwich panel development

    Anderson, R. A. / Johnson, G. A. | NTRS | 1977


    Aircraft sandwich panel, associated propulsion unit and aircraft and method of manufacture

    BROCHARD WOLFGANG / BLANKE JU RG | European Patent Office | 2023

    Free access

    METHOD FOR MANUFACTURING SANDWICH PANEL AND SANDWICH PANEL

    UESAKA MASAO | European Patent Office | 2022

    Free access

    SANDWICH PANEL

    UESAKA MASAO | European Patent Office | 2022

    Free access

    SANDWICH PANEL AND METHOD FOR MANUFACTURING SANDWICH PANEL

    SUEOKA MASAAKI | European Patent Office | 2015

    Free access