This paper is focusing on considerations pertaining to riveting/fastening systems and assembly methodology currently in use for large aircraft fuselage structures. Discussion of process principles on which current systems are based is addressing distribution of rivets along the aircraft structure, riveting/fastening systems and equipment flexibility.An attempt was made to predict the most probable future equipment development trends based on the need for more efficiency in all aircraft structural assembly and in high level and final assembly areas.


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    Title :

    Current Riveting/Fastening Methodology and Future Assembly Equipment Philosophy


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE Aerospace Automated Fastening Conference & Exposition ; 1996



    Publication date :

    1996-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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