Conclusions
-
1.
The cycle for recovery treatment of AL27-1 alloy naturally aged for more than two years is heat at 250°C for 2 min in molten salt or metal.
-
2.
After recovery treatment the alloy has the same tensile properties as after rehardening, the work for failure of a sample with a crack increases by three times, and in a number of cases the time until failure of samples in corrosion cracking tests increases by an order of magnitude in comparison with the original condition.
Similar content being viewed by others
Literature cited
N. N. Belousov and E. N. Mikheeva, Aluminum Alloys, A Handbook. Industrial Wrought, Sintered, and Cast Aluminum Alloys [in Russian], Metallurgiya, Moscow (1972), p. 358.
V. V. Istomin-Kostrovskii et al., "Electron microscopic investigation of the structure of AL27-1 alloy castings," Tsvetn. Met., No. 5, 107 (1975).
M. Bernole, R. Graf, and P. Guyot, Phil. Mag.,28, No. 4, 771 (1973).
P. Brener and W. Roth, J. Inst. Met.,74, 159 (1948).
M. F. Nikitina and G. N. Fadeeva, "Natural aging of aluminum-magnesium alloys," Tekh. Legkikh Splavov, No. 12, 9 (1974).
T. Marinaga, T. Tokanashi, and V. Rojimd, Aluminum,48, No. 8, 539 (1972).
A. Kelly and R. Nicholson, Dispersion Hardening [in Russian], Metallurgiya, Moscow (1966), p. 162.
L. A. Kurtasova and V. M. Polyanskii, "An investigation of the fine structure of AL27-1 alloy in relation to its tendency toward corrosion cracking," Fiz. Khim. Mekh. Mater.,14, No. 5, 35 (1978).
Additional information
Translated from Metallovedenie i Termicheskaya Obrabotka Metallov, No. 3, pp. 62–64, March, 1982.
Rights and permissions
About this article
Cite this article
Polyanskii, V.M., Kovtanyuk, T.D., Karpov, V.N. et al. Recovery treatment of AL27-1 alloy. Met Sci Heat Treat 24, 221–223 (1982). https://doi.org/10.1007/BF01166860
Issue Date:
DOI: https://doi.org/10.1007/BF01166860