The aircraft seat unit includes a first seat (13), a second seat (14), an intermediate portion (15) disposed between the first seat (13) and the second seat (14), and a front wall (11) adjacent to the intermediate portion (15). An axis line of the first seat (13) and an axis line of the second seat (14) are respectively disposed at angles that are oriented in mutually opposite directions with respect to a traveling direction. The intermediate portion (15) is disposed in a space between the first set and the second seat and is capable of supporting a load of a bassinet (30) placed thereon. The front wall (11) includes engagement holes (11e) that detachably engage with engagement portions (32) of the bassinet (30).


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    Titel :

    AIRCRAFT SEAT UNIT


    Weitere Titelangaben:

    FLUGZEUGSITZEINHEIT
    UNITÉ DE SIÈGE D'AÉRONEF


    Beteiligte:
    KATAKURA SACHIKO (Autor:in) / HAGIWARA HISAYA (Autor:in) / KIMIZUKA KEN (Autor:in) / KIGOSHI REI (Autor:in) / KINOSHITA MICHIO (Autor:in) / MATSUMOTO MANABU (Autor:in) / IGARI AMON (Autor:in) / AKUTSU YUICHI (Autor:in)

    Erscheinungsdatum :

    2023-10-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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