Conclusions
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1.
The investigation of the casting properties and manufacture of turbine vanes showed that it is possible to use investment casting for gas turbine vanes of the experimental alloys tested.
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2.
In alloys hardened with aluminum and titanium (alloys 1 and 2) the maximum short-term strength was retained to higher temperatures than for the alloys hardened with aluminum and niobium (alloy 3) or niobium alone (alloy 4).
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3.
All the alloys investigated had stable properties at 700–900°. More notable weakening of the alloys began at 900–950°.
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4.
For long-term operation the heat resistance is highest for alloys with aluminum and titanium as the main hardening elements (alloys 1 and 2), and lower for alloys hardened with aluminum and niobium (alloy 3) as compared with alloys in which the precipitation-hardening element is niobium alone (alloy 4).
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5.
Alloys 1 and 2 can be recommended for manufacturing, guide vanes operating at temperatures up to 950°, and alloys 3 and 4 for temperatures up to 850–900°.
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Literature cited
V. Ya. Bilyk, Casting Properties of Heat-Resisting Alloys, Report No. 224, Leningrad Polytechnical Institute [in Russian] (1963).
Yu. A. Nekhendzi et al., Zavod. Lab. No. 1 (1955).
Yu. A. Nekhendzi et al., Liteinoe Proizvodstvo, No. 7 (1966).
E. E. Levin and E. N. Masaleva, Investigation of Materials for Power Plants, Report No. 69 [in Russian], TsKTI, Leningrad (1966).
E. N. Masaleva et al., Working Capacity of Structural Materials for Power Plants, Report No. 84 [in Russian], TsKTI, Leningrad (1968).
H. Hughes, J. Iron Steel Inst., No. 7 (1967).
Additional information
Leningrad Polytechnical Institute. Translated from Metallovedenie 1 Termicheskaya Obrabotka Metallov, No. 2, pp. 46–50, February, 1971.
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Efimova, M.N., Masaleva, E.N. Cast alloys for gas turbine vanes. Met Sci Heat Treat 13, 132–136 (1971). https://doi.org/10.1007/BF00650930
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DOI: https://doi.org/10.1007/BF00650930