An aircraft cabin partition system may include at least a first partition (112) with a partition cut-out and a first flange (202) with a first flange cut-out. The aircraft cabin partition system may include a first coupling assembly (200) configured to be inserted within the first flange cut-out, configured to be inserted within an opening of a seat rail (106) within a floor of an aircraft cabin, and configured to couple the at least the first partition to the seat rail when engaged. The aircraft cabin partition system may include at least a second partition with a second flange with a second flange cut-out. The aircraft cabin partition system may include a second coupling assembly configured to be inserted within the partition cut-out, configured to be inserted within the second flange cut-out, and configured to couple the at least the second partition to the at least the first partition when engaged.


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    Titel :

    AIRCRAFT CABIN PARTITION SYSTEM


    Weitere Titelangaben:

    TRENNWANDSYSTEM FÜR FLUGZEUGKABINEN
    SYSTÈME DE SÉPARATION DE CABINE D'AÉRONEF


    Beteiligte:
    SKELLY TREVOR (Autor:in) / KRENZ MICHAEL (Autor:in)

    Erscheinungsdatum :

    15.11.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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