An aircraft seat module, which forms an aircraft seat region, includes an aircraft seat that is configured to be mounted in an aircraft cabin at an angle α of 30 degrees to 80 degrees, preferably 45 degrees to 65 degrees, and that comprises at least a base frame and a cinematics unit, with an enclosure unit comprising a first enclosure element, which delimits the aircraft seat region at least partially in the region of the aircraft seat, and a second enclosure element, which delimits the aircraft seat region partially at least in a region in front of the aircraft seat, and includes an ottoman providing a footrest region, and with a console unit that forms at least one stowage and/or depositing region of the aircraft seat region, wherein the aircraft seat is combined in a separately realized 16G module and the second enclosure element, the ottoman and the console unit are combined in a separately realized 9G module, wherein the 16G module and the 9G module are configured to be fastened to a cabin floor separately from each other.


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    Titel :

    AIRCRAFT SEAT MODULE


    Beteiligte:
    UDRISTE DANIEL (Autor:in) / THIELE MAIK (Autor:in) / DRENZECK THOMAS (Autor:in) / HOFFMANN HERMANN (Autor:in)

    Erscheinungsdatum :

    03.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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