Conclusions
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1.
Fatigue tests of alloys KhN77TYuR and EI929 showed that the effectiveness of surface hardening by plastic deformation decreases with increasing testing temperatures, and at 900° the fatigue limit is the same in both cases.
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2.
The decreasing hardening effect at high temperatures results from relaxation of the favorable compressive stresses and changes in the surface layer.
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Literature cited
Yu. V. Poloskin and V. V. Davydova, "The surface layer of hardened machine parts of heat resistant alloys," Metal. i Term. Obrabotka Metal., No. 2, 56–58 (1971).
M. S. Rakhmarova, and Ya. G. Mirer, Effect of Technological Factors on the Reliability of Gas Turbine Blades [in Russian], Mashinostroenie, Moscow (1966).
G. V. Makhanek, S. N. Petrova, and V. D. Sadovskii, in: Properties and Applications of Heat Resistant Alloys [in Russian], Nauka, Moscow (1966).
S. Z. Bokshtein, T. I. Gudkova, and S. T. Kishkin, in: Diffusion Processes, Structure, and Properties of Metals [in Russian], Mashinostroenie, Moscow (1964).
Additional information
Translated from Metallovedenie i Termicheskaya Obrabotka Metallov, No. 5, pp. 56–59, May, 1973.
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Poloskin, Y.V., Makarovskii, N.L. Effect of temperature on the effectiveness of hardening of heat resistant alloys. Met Sci Heat Treat 15, 418–420 (1973). https://doi.org/10.1007/BF01166660
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DOI: https://doi.org/10.1007/BF01166660