Riveting Thin A320 Stacks

2014-01-2264

09/16/2014

Event
SAE 2014 Aerospace Manufacturing and Automated Fastening Conference & Exhibition
Authors Abstract
Content
The E7000 riveting machine installs NAS1097KE5-5.5 rivets into A320 Section 18 fuselage side panels. For the thinnest stacks where the panel skin is under 2mm (2024) and the stringer is under 2mm (7075), the normal process of riveting will cause deformation of the panel or dimpling. The authors found a solution to this problem by forming the rivet with the upper pressure foot extended, and it has been tested and approved for production.
Meta TagsDetails
DOI
https://doi.org/10.4271/2014-01-2264
Pages
4
Citation
Zieve, P., Celek, O., and Fenty, J., "Riveting Thin A320 Stacks," SAE Technical Paper 2014-01-2264, 2014, https://doi.org/10.4271/2014-01-2264.
Additional Details
Publisher
Published
Sep 16, 2014
Product Code
2014-01-2264
Content Type
Technical Paper
Language
English