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.
Current riveting/fastening methodology and future assembly equipment philosophy
Gegenwärtige Nietverbindungs-Methodologie und Philosophie der künftigen Montageausrüstung
1996
17 Seiten, 26 Bilder
Conference paper
English
Current Riveting/Fastening Methodology and Future Assembly Equipment Philosophy
British Library Conference Proceedings | 1996
|Current Riveting/Fastening Methodology and Future Assembly Equipment Philosophy
SAE Technical Papers | 1996
|Advances in Fastening Rate Improvements for No Wink Automatic Slug Riveting
British Library Conference Proceedings | 1996
|European Patent Office | 2015
|Advances in Fastening Rate Improvements for No Wink Automatic Slug Riveting
SAE Technical Papers | 1996
|