G2000 Nine Axis Flexibility to Fasten 180 Degree Fuselage Assemblies
961873
10/01/1996
- Event
- 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.
- 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.