A window frame assembly (218) for an aircraft (10) includes a window frame (226) of composite material, adapted for attachment in a window opening (236) of an aircraft (10), having an outer flange (230) with an exterior surface (262) and an interior surface (264), a metal erosion shield (252) attached to the exterior surface (262) of the outer flange (230), and a polymer adapter ring (256) attached to the interior surface (264) of the outer flange (230). The window frame (226) has a substantially constant thickness, and the erosion shield (252) has a substantially constant cross-sectional shape. The adapter ring (256) has a sloped engagement surface (250) configured for supporting a window pane assembly (218).


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    Titel :

    WINDOW FRAME ASSEMBLY FOR AIRCRAFT


    Weitere Titelangaben:

    FENSTERRAHMENANORDNUNG FÜR FLUGZEUG
    ENSEMBLE DE DORMANT DE FENETRE POUR AVION


    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 :

    14.08.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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