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 comprises 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).

    L'invention concerne un système d'installation (1) pour installer au moins un dispositif auxiliaire (2a-f) au plafond et/ou sur une zone de paroi latérale dans le fuselage (3) d'un avion (4). Le système d'installation comprend au moins un support en principe bidimensionnel (5a, 5b, 5c, 5a', 5b', 5c') ayant des points de fixation (6), et au moins un tirant (7) relié à un point de fixation (6) et approprié pour être relié mécaniquement à un point de fixation prédéfini (8) du fuselage (3). Le ou les dispositifs auxiliaires (2) sont fixés sur le support (5).


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    Title :

    INSTALLATION SYSTEM FOR AN AIRCRAFT


    Additional title:

    SYSTÈME D'INSTALLATION POUR AVION


    Contributors:
    WHITE ADAM (author) / NICOLAS LIONEL (author) / NINI LOIC (author)

    Publication date :

    2017-02-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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