An aircraft window assembly (10) includes a first panel (12) having a first surface (14) and a second surface (16). In a first state in which there is no pressure difference between the first surface (14) and the second surface (16), the first panel (12) has a cross-sectional shape selected from planar, outwardly convex, or inwardly convex. In a second state in which there is a pressure difference between first surface (14) and the second surface (16), the first panel (12) has an outwardly convex cross-sectional shape. The assembly (10) comprises a wire grid (102) embedded in the first panel (12).


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    Titel :

    DEFORMABLE AIRCRAFT WINDOW


    Weitere Titelangaben:

    VERFORMBARES FLUGZEUGFENSTER
    HUBLOT D'AVION DÉFORMABLE


    Beteiligte:
    MCCARTHY DENNIS P (Autor:in) / BLEVINS CALVIN B (Autor:in) / HARRIS CAROLINE S (Autor:in) / GOODWIN GEORGE B (Autor:in) / GU YABEI (Autor:in)

    Erscheinungsdatum :

    2018-05-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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