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Corrosion-Resistant High-Temperature Alloys for Large Single-Crystal Turbine Blades

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Metal Science and Heat Treatment Aims and scope

Abstract

Corrosion-resistant castable high-temperature alloys with properties close to those of alloys with directed structure used for casting vanes of aircraft gas turbine engines and the process of casting of large single-crystal turbine blades of stationary gas turbine units are described. These alloys and the casting process are used to develop a new generation of gas turbine engines and units.

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REFERENCES

  1. E. N. Kablov and E. R. Golubovskii, High-Temperature Strength of Nickel Alloys [in Russian], Mashinostroenie, Moscow (1998).

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  2. E. N. Kablov, N. G. Orekhov, V. N. Toloraiya, et al., Nickel-Base Refractory Alloys, RF Patent No. 2131944, 10.08.1998 [in Russian].

  3. K. Schneider, “Advanced blading,” in: High Temperature Materials in Thermal Engineering, Part II, Kluwer Academic Publishers (1990), pp. 935–954.

  4. R. E. Shalin, E. N. Kablov, V. N. Toloraiya, and N. G. Orekhov, Device for Fabricating Single-Crystal Castings, RF Patent No. 2080209, 27.05.1997 [in Russian].

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Toloraiya, V.N., Orekhov, N.G. & Lomberg, B.S. Corrosion-Resistant High-Temperature Alloys for Large Single-Crystal Turbine Blades. Metal Science and Heat Treatment 45, 32–34 (2003). https://doi.org/10.1023/A:1023996013031

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  • DOI: https://doi.org/10.1023/A:1023996013031

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