A window frame assembly for an aircraft, includes a window frame of composite material, adapted for attachment in a window opening of an aircraft, having an outer flange with an exterior surface and an interior surface, a metal erosion shield attached to the exterior surface of the outer flange, and a polymer adapter ring, attached to the interior surface of the outer flange. The window frame has a substantially constant thickness, and the erosion shield has a substantially constant cross-sectional shape. The adapter ring has a sloped engagement surface configured for supporting a window pane assembly.


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    Titel :

    WINDOW FRAME ASSEMBLY FOR AIRCRAFT


    Beteiligte:
    GIDEON DAVID E (Autor:in) / SCHROEDER IAN E (Autor:in) / HALL KRISTIN L (Autor:in) / NG KIN M (Autor:in) / KINNEY MEGAN C (Autor:in) / REYNEKE GREG M (Autor:in) / WILKERSON RANDALL D (Autor:in) / ROSMAN RICHARD R (Autor:in) / BARTEL AARON W (Autor:in)

    Erscheinungsdatum :

    03.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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