AeroMat Home      Exposition      To Register      ASM Homepage
Back to "Session 2: Durability and Damage Tolerant Aluminum Alloys" Search
  Back to "Light Alloy Technology" Search  Back to Main Search

Tuesday, June 8, 2004 - 1:30 PM
LAT2.1

Development of Advanced High Damage Tolerance Sheet Alloys for Application in Large Aircraft Structures

B. C. Meyer, J. Schumacher, Airbus Germany, Bremen, Germany; G. Tempus, Airbus, Bremen, Germany; J. Newman, Alcoa Technical Center, Alcoa Center, PA; H. Ribes, Alcan Aerospace Transportation and Industry, Issoire Cedex, France; A. Heinz, CORUS Aluminum Rolled Products GmbH, Koblenz, Germany

The introduction of new FAA (Federal Aviation Administration) regulations for the design and manufacture of civil aircrafts has increased drastically the importance of the so called “damage tolerance properties” of aluminum alloys. This has led to the development of high damage tolerance variants of the well know AA2024. First generations of those new alloys are flying today in B777 and Airbus A340-500/600 aircrafts.

However, this development of damage tolerance properties is certainly not at the end so that current aluminum manufacturers are, in close cooperation with Airbus, developing even better alloys with especially tailored material properties. Those new alloys may combine damage tolerance with increased strength, improved manufacturability or corrosion resistance. A summary of the current developments, with a concentration on sheet alloys for fuselage applications, is given in the presentation.