Development of High Toughness Sheet and Extruded Products for Airplane Fuselage Structures

  1. Hasso Weiland,
  2. Anthony D. Rollett and
  3. William A. Cassada
  1. P. E. Magnusen1,
  2. D. C. Mooy2,
  3. L. A. Yocum3 and
  4. R. J. Rioja1

Published Online: 4 SEP 2012

DOI: 10.1002/9781118495292.ch78

ICAA13: 13th International Conference on Aluminum Alloys

ICAA13: 13th International Conference on Aluminum Alloys

How to Cite

Magnusen, P. E., Mooy, D. C., Yocum, L. A. and Rioja, R. J. (2012) Development of High Toughness Sheet and Extruded Products for Airplane Fuselage Structures, in ICAA13: 13th International Conference on Aluminum Alloys (eds H. Weiland, A. D. Rollett and W. A. Cassada), John Wiley & Sons, Inc., Hoboken, NJ, USA. doi: 10.1002/9781118495292.ch78

Author Information

  1. 1

    Alcoa Technical Center, 100 Technical Drive, Alcoa Center, PA 15069-0001, USA

  2. 2

    Alcoa Davenport Works, 4879 State Street, Bettendorf, IA 52722, USA

  3. 3

    Alcoa Lafayette Works, 3131 E. Main Street, Lafayette, IN 47905, USA

Publication History

  1. Published Online: 4 SEP 2012
  2. Published Print: 5 JUN 2012

ISBN Information

Print ISBN: 9781118458044

Online ISBN: 9781118495292

SEARCH

Keywords:

  • Al-Li;
  • Al-Cu-Mg-Li;
  • 2199;
  • 2060;
  • Aerospace;
  • Fuselage;
  • Toughness;
  • Fatigue Crack Growth

Summary

This chapter contains sections titled:

  • Introduction

  • Evolution of Aluminum Fuselage Alloys

  • Microstructural considerations

  • Al-Li Fuselage Alloy Development

  • Conclusions