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Condensation and condensation-diffusion coatings for turbine blades made of high-temperature alloys with a directed crystal structure

  • Heat-Resistant Alloys
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Metal Science and Heat Treatment Aims and scope

Abstract

Results of an investigation of condensation (condensed) and condensation-diffusion coatings for protecting working turbine blades made of high-temperature nickel alloys from high-temperature gas corrosion are presented. The coatings were deposited on specimens of a high-temperature model nickel alloy by the ion-plasma method.

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References

  1. P. G. Kolomytsev,Gas Corrosion and Strength of Nickel Alloys [in Russian], Metallurgiya, Moscow (1984).

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  2. B. E. Paton, G. B. Stroganov, S. T. Kishkin, et al.,High-Temperature Strength of Nickel Alloys and Their Protection from Oxidation (in Russian], Naukova Dumka, Kiev (1987).

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  3. S. A. Muboyadzhyan, E. N. Kablov, and S. A. Budinovskii, “Vacuum-plasma technology for producing protective coatings from complexly alloyed alloys,”Metalloved. Term. Obr. Metallov, No. 2, 15 – 18 (1995).

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Authors and Affiliations

  1. All-Russia Institute of Aircraft Materials, Moscow, Russia

    S. A. Muboyadzhyani & S. A. Budinovskii

Authors
  1. S. A. Muboyadzhyani
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  2. S. A. Budinovskii
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Translated from Metallovedenie i Tetmicheskaya Obrabotka Metallov, No. 4, pp. 15 – 18, April, 1996.

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Muboyadzhyani, S.A., Budinovskii, S.A. Condensation and condensation-diffusion coatings for turbine blades made of high-temperature alloys with a directed crystal structure. Met Sci Heat Treat 38, 159–162 (1996). https://doi.org/10.1007/BF01401512

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  • DOI: https://doi.org/10.1007/BF01401512

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