An electromagnetic energy protection system for an aircraft component, the system including a plurality of conductive sheets (208A, 208B, 208C, 208D, 208E) ohmically connected by conductive interconnects (210A, 210B). The conductive interconnects are metal formed by a metal deposition process. The metal deposition process can include a plasma deposition process. The conductive interconnects prevent the formation of surface deformities such as bumps that may be caused when connecting, either physically or electrically, adjacent conductive sheets.


    Access

    Download


    Export, share and cite



    Title :

    Electromagnetic energy surface protection


    Additional title:

    Elektromagnetischer Energieoberflächenschutz
    Protection de surface d'énergie électromagnétique


    Contributors:

    Publication date :

    2018-12-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    ELECTROMAGNETIC ENERGY SURFACE PROTECTION

    ROBERT MARSHALL BURGESS / JOSEPH A MARSHALL | European Patent Office | 2015

    Free access

    Electromagnetic energy surface protection

    BURGESS ROBERT MARSHALL / MARSHALL JOSEPH A | European Patent Office | 2017

    Free access

    ELECTROMAGNETIC ENERGY SURFACE PROTECTION

    BURGESS ROBERT MARSHALL / MARSHALL DZHOZEF A | European Patent Office | 2018

    Free access

    Electromagnetic energy surface protection

    BURGESS ROBERT MARSHALL / MARSHALL JOSEPH A | European Patent Office | 2017

    Free access

    Automobile electromagnetic energy absorption and protection device group

    JIANG SHIWEI | European Patent Office | 2020

    Free access