A structural element, in particular for an aircraft, such as an airplane, contains a laminate having a plurality of layers made of a fiber composite plastics material with carbon fibers, a lightning protection layer and optionally an electrically insulating dielectric protection layer. The laminate contains at least one hybrid layer, which comprises a carbon fiber-absorption fiber composite, the elongation at break of the absorption fiber being greater than the elongation at break of the carbon fibers.


    Access

    Download


    Export, share and cite



    Title :

    Structural element


    Contributors:

    Publication date :

    2020-09-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse



    STRUCTURAL ELEMENT

    GAFNI IZHAR | European Patent Office | 2020

    Free access

    Structural element

    MELLAND TRISTAN | European Patent Office | 2019

    Free access

    Structural element

    ECKERT MARC OLIVER / RIEGER ROGER PAUL / SPOHDE ULRICH | European Patent Office | 2019

    Free access

    STRUCTURAL ELEMENT

    DITTRICH KAY / KARCH CHRISTIAN | European Patent Office | 2016

    Free access

    Structural element

    MELLAND TRISTAN | European Patent Office | 2022

    Free access