The invention pertains to the field of aviation, in particular, to a structure for fastening components of interior equipment in the passenger compartment of an airplane. The fastening structure contains fastening means produced on the fuselage; suspension elements (2) immovably connected to said fastening means, and at least one system support (1) running in the longitudinal direction of the fuselage, connected to the suspension elements (2). The suspension elements (2) include at least one first suspension element (9) and at least one second suspension element (10, 11), wherein each of the first suspension elements is rigidly connected to the system support, and each of the second suspension elements forms with the system support a sliding connection, so that the system support is able to slide relative to these second suspension elements along the longitudinal axis of the airplane fuselage. The sliding capability of the system support relative to the second suspension elements substantially reduces the load on the bulkhead in the longitudinal direction. 12 dependent claims, 13 illustrations.


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    Titel :

    STRUCTURE FOR FASTENING EQUIPMENT IN AIRCRAFT


    Weitere Titelangaben:

    STRUKTUR ZUR BEFESTIGUNG VON VORRICHTUNGEN IN FLUGZEUG
    STRUCTURE POUR FIXATION D'INSTALLATIONS DANS AERONEF


    Beteiligte:
    MAMUSHKIN DMITRIY (Autor:in) / BESPALOV IVAN (Autor:in)

    Erscheinungsdatum :

    07.12.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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