G2000 Nine Axis Flexibility to Fasten 180 Degree Fuselage Assemblies

961873

10/01/1996

Event
SAE Aerospace Automated Fastening Conference & Exposition
Authors Abstract
Content
This technical paper will address the advancements made in the area of automatically riveting complex double-contour 180 degree fuselage panels. Detailed is an automatic fastening system that accomplishes the aforementioned task in a single workframe mounted panel/fixture sequence. Through the use of innovative machine motions and enhanced adaptive controls, increased production throughput for difficult to rivet panel assemblies has been realized.
Meta TagsDetails
DOI
https://doi.org/10.4271/961873
Pages
7
Citation
Mangus, W., and McKeown, S., "G2000 Nine Axis Flexibility to Fasten 180 Degree Fuselage Assemblies," SAE Technical Paper 961873, 1996, https://doi.org/10.4271/961873.
Additional Details
Publisher
Published
Oct 1, 1996
Product Code
961873
Content Type
Technical Paper
Language
English