Conclusions
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1.
In alloying of 0.11–0.17% C steel used for the production of turbogenerator rotors with nickel up to 4.5–4.7% in comparison with type 25KhN3MFA steels used at present for this purpose a fine grain and a uniform bainitic structure are obtained in a broad range of cooling rates from the austenitizing temperature and also a high guaranteed level of mechanical properties of σ0.2 ≧ 600 N/mm2, σt ≧ 800 N/mm2, δ ≧ 18%, ψ ≧ 50%, a0.25≧100 J/cm2, and T50=−60°C.
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2.
The steel with 0.11–0.17% C and 4.2–4.6% Ni (heat 1) has a higher fatigue limit for unnotched specimens (350–380 N/mm2) in comparison with steel I of type 25KhN3MFA (300–320 N/mm2).
Surface plastic deformation of specimens with a groove leads to an increase in the fatigue limit from 360 to 410 N/mm2, which makes it possible to recommend this method for the purpose of an additional increase in the fatigue resistance of turbogenerator rotors.
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3.
Combined alloying with niobium and cobalt of steel with a reduced carbon content and an increased nickel content (heat 3) causes an increase in the fatigue limit of unnotched specimens from 350 to 360 N/mm2 and of specimens with a stress raiser from 200 to 220 N/mm2.
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4.
The use in melting of the steels of pure primary charge materials makes it possible to obtain the very highest fatigue limit on unnotched specimens (σ−1 = 400 N/mm2) and specimens with a groove (σ=1r = 250 N/mm2).
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Central Scientific-Research Institute for Machine Building Technology Scientific and Production Union. Translated from Metallovedenie i Termicheskaya Obrabotka Metallov, No. 9, pp. 15–19, September, 1986.
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Naumchenkov, N.E., Filimonova, O.V. & Borisov, I.A. Influence of alloying, stress concentration, and surface hardening on the fatigue resistance of rotor steel. Met Sci Heat Treat 28, 637–642 (1986). https://doi.org/10.1007/BF00742741
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DOI: https://doi.org/10.1007/BF00742741