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The Atmospheric Stress-Corrosion Resistance of some Forged High Strength Aluminium Alloys and an Assessment of the Effects of a Step-Quench into Molten Salt

Published online by Cambridge University Press:  07 June 2016

W. M. Doyle
Affiliation:
High Duty Alloys Limited
R. G. Jones
Affiliation:
High Duty Alloys Limited
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Extract

Since the introduction of aluminium-zinc-magnesium-copper alloys, investigations into the behaviour of these high strength materials, over a wide range of composition, have indicated the significance of corrosion as a factor affecting the cracking of these alloys after prolonged stressing at loads below the ultimate tensile strength of the material.

Most of the previous work designed to assess the stress-corrosion resistance of aluminium-zinc-magnesium-copper alloys (D.T.D. 683A*) was carried out on sheet and plate material and the present investigation is concerned with the examination of these materials in the form of large hand-forged slabs, tested in the short transverse direction.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society. 1959

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References

1. Rosenhain, W., Archbutt, S. L. and Hanson, D. Eleventh Report to the Alloys Research Committee: On Some Alloys of Aluminium (Light Alloys). Institution of Mechanical Engineers, 1921.CrossRefGoogle Scholar
2. Sander, W. and Meissner, K. L. The Influence of the Compound MgZn2 on the Workability of Aluminium Alloys. (In German). Zeitschrift für unorganische Chemie, Vol. 154, p. 144, 1926 Google Scholar
3. Bradbury, T. F. A New Aluminium Alloy. BP.476, 930.Google Scholar
4. Bradbury, T. F. and Warrington, H. G. Improvements Relating to Extruded Aluminium Base Alloys. BP.601, 813.Google Scholar
5. Dix, E. H. Aluminium-Zinc-Magnesium Alloys: Their Development and Commercial Production. Transactions of the American Society for Metals, Vol. 42, p. 1057, 1950.Google Scholar
6. Chadwick, R., Muir, N. B. and Grainger, H. B. Stress-Corrosion of Wrought Ternary and Complex Alloys of the Aluminium-Zinc-Magnesium System. Journal of the Institute of Metals, Vol. 85, p. 161, 1957.Google Scholar
7. Perryman, E. C. W. and Blade, J. C. Relationship Between the Ageing and Stress-Corrosion Properties of Aluminium-Zinc Alloys. Journal of the Institute of Metals, Vol. 77, p. 263, 1950.Google Scholar
8. Perryman, E. C. W. Intercrystalline Cracking of Aluminium-Zinc Alloys. (In French). Comptes Rend., Vol. 235, p. 884, 1952.Google Scholar
9. Hardy, H. K. Modern Descriptive Theories of Precipitation Processes. Journal of the Institute of Metals, Vol. 75, p. 707, 1949.Google Scholar
10.British Intelligence Objectives Sub-Committee. High Strength Aluminium-Zinc- Magnesium Alloy Development in Germany. B.I.O.S. Final Report No. 1770, Item No. 21.Google Scholar
11. Meikle, G. and Lewis, D. The Atmospheric Stress-Corrosion of Aluminium-Zinc-Magnesium Type Alloys. R.A.E. Report No. Met. 88, October 1955.Google Scholar
12. Fink, W. L. and Willey, L. A. Quenching of 75S Aluminium Alloy. Metals Technology, Vol. 14, No. 5, Technical Publication No. 2225, 1947.Google Scholar
13. Wilson, C. Quenching Conditions. Aircraft Production, Vol. 17, p. 72, 1955.Google Scholar
14. Edmunds, W. T. and Lloyd, R. C. The Production of Light-Alloy Drop-Forgings, Their Heat Treatment, Inspection and Testing. Institute of Metals Monograph and Report Series No. 17: 1955–59.Google Scholar
15.High Duty Alloys Limited. Hiduminium Technical Data, 1958.Google Scholar