Conclusions
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1.
To strengthen compressor disks of alloy VT9 we recommend pneumoshotpeening followed by vibropolishing and microshotpeening, ensuring the formation of the highest compressive stresses at the surface (40–60 kgf/mm2) and extending to a depth exceeding the depth of the damaged layer after turning.
Line broadening amounted to 300±20% and the surface roughness Ra=1.25-0.63.
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2.
The best method of strengthening compressor disks of alloy ÉI698VD is microshotpeening, ensuring formation of compressive stresses with a maximum value of 120 kgf/mm2 at the surface and extending to a depth equal to the depth of the damaged layer after turning.
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Literature cited
I. V. Kudryavtsev, Improving the Strength and Service Life of Machine Parts by Surface Plastic Deformation [in Russian], Conference Materials. TsNIITMASh (1970) p. 262.
A. V. Podzei et al., Technological Residual Stresses [in Russian], Mashinostroenie, Moscow (1973).
I. G. Grinchenko, Strengthening Parts of Heat Resistant and Titanium Alloys [in Russian], Mashinostroenie, Moscow (1971), p. 116.
G. A. Deryagin, "Strengthening the scarf portion of turbine vanes by strain hardening," in: Strengthening Machine Parts by Mechanical Strain Hardening [in Russian], Nauka, Moscow (1965) p. 198.
V. A. Parfenov, Teplotekhnika, No. 5, 78 (1956).
Additional information
Translated from Metallovedenie i Termicheskaya Obrabotka Metallov, No. 4, pp. 13–16, April, 1979.
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Tseitlin, V.I., Poloskin, Y.V., Makarovskii, N.L. et al. Optimal method of surface plastic deformation of compressor disks made of alloys VT9 and ÉI698VD. Met Sci Heat Treat 21, 257–261 (1979). https://doi.org/10.1007/BF00775102
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DOI: https://doi.org/10.1007/BF00775102