The present invention relates to a floor arrangement in an aircraft. In order to provide an improved cabin floor construction, a floor arrangement (10) for a cabin of an aircraft (11) is provided. The arrangement comprises two floor support part-structures (12a, 12b), each having a plurality of vertical support members (14), at least one longitudinal beam member (16), a plurality of cantilevering members (18) and at least one seat rail (20). The at least one longitudinal beam member extends in a first direction (D1). The at least one first seat rail extends in the first direction and is carried by the at least one first longitudinal beam member. The cantilevering members cantilever in a second direction (D2) transverse to the first direction. The vertical support members extend in a third direction (D3) transverse to the first and the second direction. The two floor support part-structures are each configured to be arranged along opposing side portions within a fuselage structure (28) of the aircraft. The vertical support members are configured to transfer load from the cantilevering members and the at least one first longitudinal beam member to the fuselage structure of the aircraft. The plurality of cantilevering members and the at least one first longitudinal beam member are configured to carry a cabin floor (30) that is configured to provide a load transfer in a plane direction of the floor and to contribute to a stiffening of the fuselage structure.


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    Titel :

    FLOOR ARRANGEMENT IN AN AIRCRAFT


    Weitere Titelangaben:

    BODENANORDNUNG IN EINEM FLUGZEUG
    AGENCEMENT DE PLANCHER DANS UN AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    03.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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