An interior component carrier system (10) comprises a first and a second installation rail (12, 14). Each of the first and the second installation rail (12, 14) includes at least one connecting portion (16) being connectable to an associated primary structure component (18) in order to fasten the installation rail (12, 14) to the primary structure component (18), and a carrier portion (20) extending from the connecting portion (16) in a direction along a longitudinal axis (L) of the interior component carrier system (10). The interior component carrier system (10) further comprises a first carrier element (80) having a first end connected to a first carrier rod (82) extending in a direction along the longitudinal axis (L) of the interior component carrier system (10) and a second end which is connectable to a first interior component (94), wherein the first carrier rod (82) is fastened to the carrier portion (20) of the first installation rail (12, 14), and a second carrier element (84) having a first end connected to a second carrier rod (86) extending in a direction along the longitudinal axis (L) of the interior component carrier system (10) and a second end connected to the first carrier element (80), wherein the second carrier rod (86) is fastened to the carrier portion (20) of the second installation rail (12, 14).


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    Title :

    INTERIOR COMPONENT CARRIER SYSTEM AND METHOD FOR MOUNTING AN AIRCRAFT INTERIOR COMPONENT CARRIER SYSTEM


    Additional title:

    INNENRAUMKOMPONENTENTRÄGERSYSTEM UND VERFAHREN ZUR MONTAGE EINES FLUGZEUGINNENRAUMKOMPONENTENTRÄGERSYSTEMS
    SYSTÈME DE SUPPORT DE COMPOSANT INTÉRIEUR ET PROCÉDÉ DE MONTAGE D'UN SYSTÈME DE TEL SUPPORT


    Contributors:

    Publication date :

    2019-06-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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