Essential technological premises for the introduction of composite materials into the fuselage structure of future commercial aircraft were prepared. Selected critical as well as production-development components were manufactured, tested and evaluated. Tests were developed and prepared in order to continue post crash fire research. The possibilities to improve materials and processes were analyzed. The structural efficiency of the selected critical components was proved. The development risks are therefore sufficiently minimized.
Development and Testing of Critical Components for Technological Preparation of an Airbus CFRP (Carbon Fiber Reinforced Plastics) Fuselage, Phase 2. Final Report, May 1, 1986-June 30, 1987
1987
75 pages
Report
Keine Angabe
Englisch
New production techniques for CFRP components in Airbus production
Tema Archiv | 1987
|AIRBUS A340 Final Assembly by S.O.J.A.: Semi-Automatic Orbital Fuselage Join Up Robot
SAE Technical Papers | 2002
|AIRBUS A340 Final Assembly by S.O.J.A.: Semi-Automatic Orbital Fuselage Join Up Robot
British Library Conference Proceedings | 2002
|