An aircraft interior panel for supporting high-weight loads including a core panel sandwiched between structural plies, a panel insert embedded in the panel and passing through and interrupting the core panel, the insert having an elongate stem capped on each end with an enlarged flange, the elongate stem being arranged axially perpendicular to the core panel and the enlarged flanges being arranged parallel to the core panel, and facing sheets bonded outward of the panel insert for concealing the panel insert within the aircraft interior panel.


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    Titel :

    HIGH-STRENGTH AIRCRAFT INTERIOR PANEL WITH EMBEDDED INSERT


    Weitere Titelangaben:

    HOCHFESTE FLUGZEUGINNENRAUMTAFEL MIT EINGEBETTETER EINLAGE
    PANNEAU INTÉRIEUR D'AÉRONEF À HAUTE RÉSISTANCE COMPORTANT UN INSERT INCORPORÉ


    Beteiligte:
    RUONAVAARA KEVIN (Autor:in) / HOHENSEE RYAN (Autor:in) / GRIEVE JAMES C (Autor:in)

    Erscheinungsdatum :

    01.02.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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



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