Abstract
The influence of thermal barrier coatings based on nickel aluminides on the long-term strength and creep characteristics of nickel superalloys is considered. The increase in the fatigue life of coated alloy specimens at high temperatures under high-temperature oxidation conditions is shown to be primarily due to the protection of the surface layer of the metal from chemical destruction during gas corrosion. The decrease in the fatigue life of the uncoated specimens is due to the oxidation of the alloy elements, which becomes more intense with the test time. The complex coatings Ni–Cr–Al–Y, Cr–Al–Ti–Hf, and Ni–Al–Hf–Y under study are found to exert a positive effect on the creep characteristics of high-temperature alloys ZhS6U, VZhL12U, ZhS16, and ZhS30M.
Similar content being viewed by others
REFERENCES
A. V. Logunov, Nickel Superalloys for Gas Turbine Blades and Disks (Izd. Dom Gazoturbinnye Tekhnologii, Rybinsk, 2017).
E. N. Kablov, Cast Gas Turbine Engine Blades: Alloys, Technologies, and Coatings (Nauka, Moscow, 2006).
V. V. Sidorov, D. N. Petrov, O. M. Kosenkov, “Development of technological parameters for processing the substandard wastes of a VZhM-4VI nickel superalloy to reduce the carbon content in them,” Elektrometallurgiya, No. 12, 28–36 (2019).
N. V. Abraimov and V. A. Geikin, Temperature-Resistant Coatings and Welding in Gas Turbine Engines (Nauka Tekhnol., Moscow, 2018).
N. V. Abraimov and A. Yu. Zolotareva, “Influence of high-temperature coatings on the reliability characteristics of GTE blade elements,” Elektrometallurgiya, No. 6, 24–32 (2019).
S. A. Budinovskii, P. V. Matveev, A. A. Smirnov, and D. A. Chubarov, “Investigation of heat-protective coatings for turbine blades made of nickel superalloys with an external magnetron ceramic layer,” Elektrometallurgiya, No. 1, 3–10 (2019).
S. A. Budinovskii, S. A. Muboyadzhyan, A. M. Gayamov, and P. V. Matveev, “Development of ion-plasma heat-resistant metal layers of heat-protective coatings for cooled turbine blades,” Metalloved. Term. Obrab. Met., No. 11, 16–21 (2013).
I. L. Svetlov, N. V. Petrushin, E. R. Golubovskii, K. K. Khvatskii, D. V. Shchegolev, and E. S. Elyutin, “Mechanical properties of single crystals of a nickel superalloy containing rhenium and ruthenium,” Deform. Razrushenie Mater., No. 11, 26–35 (2008).
M. A. Shtremel’, Fracture. Book 2. Fracture of Structures: Monograph (Izd. Dom MISiS, 2015).
V. V. Ovchinnikov, Yu. V. Petrov, and N. V. Abraimov, “Influence of operational factors on the fatigue life characteristics of aircraft,” Elektrometallurgiya, No. 11, 22–35 (2018).
V. P. Alekhin, Physics of Strength and Plasticity of Surface Layers in Materials (Nauka, Moscow, 1983).
I. S. Tsvilyuk and D. S. Avramenko, “Parametric methods of description and extrapolation of the long-term strength characteristics of refractory materials,” Probl. Prochnosti, No. 12, 59–63 (1985).
Author information
Authors and Affiliations
Corresponding author
Additional information
Translated by K. Shakhlevich
Rights and permissions
About this article
Cite this article
Abraimov, N.V., Orekhova, V.V. Effect of Thermal Barrier Coatings on the High-Temperature Strength of Nickel Alloys. Russ. Metall. 2021, 735–745 (2021). https://doi.org/10.1134/S0036029521060021
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S0036029521060021