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:

    Gegenwärtige Nietverbindungs-Methodologie und Philosophie der künftigen Montageausrüstung


    Contributors:
    Sarh, B. (author) / Janicki, G. (author)


    Publication date :

    1996


    Size :

    17 Seiten, 26 Bilder




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Current Riveting/Fastening Methodology and Future Assembly Equipment Philosophy

    Sarh, B. / Janicki, G. / SAE | British Library Conference Proceedings | 1996


    Current Riveting/Fastening Methodology and Future Assembly Equipment Philosophy

    Sarh, Branko / Janicki, Gerry | SAE Technical Papers | 1996



    Advances in Fastening Rate Improvements for No Wink Automatic Slug Riveting

    Kubanek, K. / Kellner, R. / SAE | British Library Conference Proceedings | 1996


    Advances in Fastening Rate Improvements for No Wink Automatic Slug Riveting

    Kubanek, Kurt / Kellner, Robert | SAE Technical Papers | 1996