A table (30) for an aircraft includes a table surface (56) deployable between a retracted position and a deployed position, an arm (50) having a first end and a second end, the arm (50) supporting the table (66) surface at the first end, a support connected to the arm (50) at the second end, the support connecting the arm to a structure interior to the aircraft, a sensor (136) within the aircraft to detect if a seat adjacent to the table surface is occupied, and a mechanism (120) for retracting the table surface to the retracted position if the sensor (136) detects at least one of that the seat is not occupied and that the aircraft flight mode meets predetermined criteria.


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    Titel :

    Exit row table for an aircraft


    Beteiligte:
    GAGNON PIERRE (Autor:in) / ROY JORDAN (Autor:in) / DEKA TOM (Autor:in) / MAGEAU CHRISTIAN (Autor:in) / MONARDO MICHELE (Autor:in) / HUBER STEFAN (Autor:in) / HASELBERGER CHRISTOPH (Autor:in)

    Erscheinungsdatum :

    2018-10-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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