Hostname: page-component-cd9895bd7-jn8rn Total loading time: 0 Render date: 2024-12-25T06:56:00.670Z Has data issue: false hasContentIssue false
  • English
  • Français

The application of improved aluminium alloys and steels in aircraft structures

Published online by Cambridge University Press:  04 July 2016

C. J. Peel  and
D. S. McDarmaid
C. J. Peel
Affiliation:
Materials Department, Royal Aircraft Establishment, Farnborough
D. S. McDarmaid
Affiliation:
Materials Department, Royal Aircraft Establishment, Farnborough
Get access Rights & Permissions [Opens in a new window]

Extract

This paper deals, in the main, with aluminium alloys and steels that are currently available on a commercial basis or are likely to become available in the near future. It highlights the more significant improvements made during the past two decades.

Aircraft structures have been built predominantly of aluminium alloys since the Second World War and, although certain improvements have been made over this period, the alloy systems used have changed little essentially because the alloys available have been limited by the solid solubilities of the selected solute elements at safe solution temperatures. The slow but certain development of novel production routes including fibre and whisker reinforcement of metals, powder production and rapid solidification techniques will circumvent this limitation by the turn of the century.

Type
Developments in structures and manufacturing techniques
Information
The Aeronautical Journal , Volume 85 , Issue 847 , September 1981 , pp. 320 - 326
Copyright
Copyright © Royal Aeronautical Society 1981 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Swihart, J. M. 12th 1CAS Congress, Munich, October 1980.Google Scholar
2. Hyatt, M. V. Aluminium alloys in the Aircraft Industries, Turin Symposium, October 1976.Google Scholar
3. Kaufman, J. G. and Holt, M. Alcoa Technical Paper 18,1965.Google Scholar
4. Bucci, R. J. Alcoa Report No. 57-77-24, September 1978.Google Scholar
5. Peel, C. J. and Forsyth, P. J. Metal Science Jnl, 7, pl21,1973.Google Scholar
6. Thompson, D. S. Metallurgical Transactions (A), 6, April 1975.Google Scholar
7. Rosenfield, A. R. et al. AFML TR-74-129, Part 1, December 1974.Google Scholar
8. Baker, C. and Martin, D. C. Aluminium alloys in the Aircraft Industries, Turin Symposium, October 1976.Google Scholar
9. Reynolds, M. A., Fitzsimmons, P. E. and Harris, J. G. ibid.Google Scholar
10. Poole, P. Greenfield, D. and Percy, S. RAE Technical Report 80116, September 1980.Google Scholar
11. Sanders, T. H., and Balmuth, E. S. Metal Progress, March 1978.Google Scholar
12. Cebulak, W. S., Johnson, E. W. and Markus, H. Metals Engineering Quarterly, November 1976.Google Scholar
13. Wanhill, R. J. Fatigue of Engineering Materials and Structures, 2, p319,1979.Google Scholar
14. Little, C. D. and Machmeier, P. M. AFML-TR-76-148, September 1975.Google Scholar
15. McDarmaid, D. S. British Corrosion Journal, 15,4,1980.Google Scholar
16. Townsend, D. P. and Zaretsky, E.V. ASME Publication Paper No 80-C2/DET-58.Google Scholar