The invention is directed to an installation system (1) for installing at least one auxiliary device (2a-f) overhead and/or at a sidewall area in a fuselage (3) of an aircraft (4). The installation system includes at least one in principle two-dimensional carrier (5a, 5b, 5c, 5a′, 5b′, 5c′) with fastening points (6) and at least one tie rod (7) interconnected to a fastening point (6) and suited to be mechanically interconnected to a predefined fastening point (8) of the fuselage (3). The at least one auxiliary device (2) is attached to the carrier (5).


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    Titel :

    INSTALLATION SYSTEM FOR AN AIRCRAFT


    Beteiligte:
    WHITE ADAM (Autor:in) / NICOLAS LIONEL (Autor:in) / NINI LOIC (Autor:in)

    Erscheinungsdatum :

    16.08.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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