Abstract
This paper describes the major changes at Airbus aircraft from the A300 aircraft developed in the early 1970s up to the A380-800, which will be certified and delivered in early 2006. The examples presented deal with new metallic materials and structural developments for the fuselage and other main components of the aircraft. Current advances in technologies, processes, and procedures have resulted in evolutionary improvements in metallic structural optimization, which will be summarized. Furthermore, special attention will be given to advanced manufacturing methods and processes introduced to former and current Airbus aircraft programs. A brief description of future technologies allows for the assessment of additional opportunities.
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