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.
G2000 Nine Axis Flexibility to Fasten 180 Degree Fuselage Assemblies
Sae Technical Papers
SAE Aerospace Automated Fastening Conference & Exposition ; 1996
1996-10-01
Conference paper
English
G2000 Nine Axis Flexibility to Fasten 180 Degree Fuselage Assemblies
British Library Conference Proceedings | 1996
|FUSELAGE BARREL ASSEMBLIES AND METHODS OF ASSEMBLING FUSELAGE BARREL ASSEMBLIES
European Patent Office | 2024
|FUSELAGE BARREL ASSEMBLIES AND METHODS OF ASSEMBLING FUSELAGE BARREL ASSEMBLIES
European Patent Office | 2022
|FUSELAGE BARREL ASSEMBLIES AND METHODS OF ASSEMBLING FUSELAGE BARREL ASSEMBLIES
European Patent Office | 2022
|Fuselage barrel assemblies and methods of assembling fuselage barrel assemblies
European Patent Office | 2024
|