A panel assembly that includes inside and outside core layers, an armor layer sandwiched between the inside and outside core layers, and an armor member that includes at least an outside portion and a transverse portion. The outside core layer includes a cut out portion defined therein. The armor layer has opposing first and second major surfaces. The outside portion of the armor member is positioned in the cut out portion of the outside core layer and the outer surface of the transverse portion is generally perpendicular to the first and second major surfaces of the armor layer.


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    Titel :

    AIRCRAFT PANEL INCLUDING BALLISTIC STAB-IN ARMOR


    Weitere Titelangaben:

    FLUGZEUGPANEEL MIT BALLISTISCHER STICHFESTER PANZERUNG
    PANNEAU AÉRONAUTIQUE COMPRENANT UN BLINDAGE PARE-BALLES


    Erscheinungsdatum :

    2020-07-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F41H Panzerung , ARMOUR / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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