An aircraft evacuation assembly (100) for electricity dispersion may include a composite packboard housing (110) defining a packboard compartment (116), wherein the composite packboard housing (110) is electrically nonconductive, and a girt (7) mounted to the composite packboard housing (110) and disposed in the packboard compartment (116). The evacuation assembly(100) may further include a metal stud (120) extending through the composite packboard housing (110), wherein the metal stud (120) includes a first end portion (124) disposed external to the packboard compartment (116) and a second end portion (122) disposed internal to the packboard compartment (116) in electrical contact with the girt (7). The evacuation assembly may further include a flexible strip (130) attached to an external surface (118), relative to the packboard compartment (116), of the composite packboard housing (110). The flexible strip (130) may be electrically conductive and the flexible strip (130) may extend between and electrically connect the first end portion (124) of the metal stud and an electrical interface (140).


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    Title :

    ELECTRICITY DISPERSION FOR AIRCRAFT EVACUATION ASSEMBLIES


    Additional title:

    ELEKTRIZITÄTSDISPERSION FÜR FLUGZEUGEVAKUIERUNGSANORDNUNGEN
    DISPERSION D'ÉLECTRICITÉ POUR DES ENSEMBLES D'ÉVACUATION D'AÉRONEF


    Contributors:

    Publication date :

    2020-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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