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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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