A static aircraft seat privacy panel (102) may include a body (106). At least a portion of a surface of the body (106) may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge (108) of the body may be configured to couple to a floor via a set of floor-mounted components (300). The set of floor-mounted components (300) may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge (120) of the body may be configured to be offset a selected distance from a surface of one or more overhead structures (116) of the aircraft cabin when the body (106) is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel (102) may be compliant with 9G force requirements for aviation transport.


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    Titel :

    STATIC AIRCRAFT SEAT PRIVACY PANELS


    Weitere Titelangaben:

    STATISCHE SICHTSCHUTZPANEELE FÜR FLUGZEUGSITZE
    PANNEAUX DE CONFIDENTIALITÉ STATIQUES POUR SIÈGE D'AVION


    Beteiligte:
    JOHNSON GLENN A (Autor:in) / DOWTY MARK B (Autor:in) / MCKEE JEFFEREY M (Autor:in) / PENCE TRACY (Autor:in) / PRINCIP MICHAEL M (Autor:in)

    Erscheinungsdatum :

    14.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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