A divider device for an aircraft cabin is disclosed comprising a plurality of elongate bar elements (1, 1', 1"), wherein each bar element (1, 1', 1") is planar and flexible so that it may assume a linear state in which it extends rectilinearly along a longitudinal axis parallel to a plane (7), wherein each bar element (1, 1', 1") has a first stable state in which it is curved, so that it deforms into its first stable state when being bent out of the linear state towards the stable state to a predetermined extent, wherein the bar elements (1, 1', 1") are arranged side-by-side and adjacent bar elements (1, 1', 1") are pivotably interconnected with each other, so that when the bar elements (1, 1', 1") are in the linear state, their longitudinal axes extend in parallel, and wherein each pair of first and second adjacent bar elements (1', 1") are designed such that when the first and the second bar elements (1', 1") are in the linear state and extend in a common plane (7), in the first stable state of the first bar element (1') one end (9') thereof is positioned on a first side of the plane (7) whereas in the first stable state of the second bar element (1") its end (9") corresponding to the end (9') of the first bar element (1') is located on a second side of the plane (7) opposite the first side.


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    Titel :

    Foldable divider device for an aircraft cabin


    Weitere Titelangaben:

    Faltbare Trennvorrichtung für eine Flugzeugkabine
    Dispositif diviseur pliant destiné à une cabine d'aéronef


    Beteiligte:
    MAYER TOBIAS (Autor:in)

    Erscheinungsdatum :

    2020-10-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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