Researh of Influence of Technological Factors of Formation of Plasma Coatings on their Thermal Technical Properties

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The article considers issues related to the choice of abrasive material and technology of its use for the formation of necessary roughness on the base material and necessary heat resistance of the heat-protective coating during plasma spraying. The influence of the shape and size of the abrasive on final roughness of the treated surface was studied at various angles of contact between the sprayed abrasive and the surface (angle of attack). From the condition of maximum heat resistance, the composition of the heat-resistant composite coating of the spinel type was determined, which consists of 3 layers: the 1st layer (sublayer) material is a chromium-aluminum composite and the 2nd layer of a transitional spinel-based aluminum and chromium oxide + chromium-aluminum composite and the 3rd a layer of spinel based on aluminum and chromium oxides.

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188-193

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May 2020

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© 2020 Trans Tech Publications Ltd. All Rights Reserved

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[1] Lyalyakin, V.P., Litovchenko., N.N., Sablukov, A.S., Denisov, V.I., & Sokovtseva, V.N. (2006). The physical nature and conditions of adhesion of particles of a metal powder to a substrate during thermal spraying. Technology of metals, (5), 36-44.

Google Scholar

[2] Bolshakov, V.I. et al. (2011). Ceramic composite materials for work at high temperatures. Scientific works Construction, materials science, mechanical engineering, (58), 351-352.

Google Scholar

[3] Lakiza, S. M., Tyschenko, J. S., & Lopato, L. M. (2011). Phase diagram of the Al2O3–HfO2–Y2O3 system. Journal of the European Ceramic Society, 31(7), 1285-1291. https://doi.org/10.1016/j.jeurceramsoc.2010.04.041.

DOI: 10.1016/j.jeurceramsoc.2010.04.041

Google Scholar

[4] Friedman, A.Kh., & Mikus, E.B. (2001). Coatings for refractory alloys for short-term service at high temperatures. FriedmanProtective coatings on metals, Kyiv.

Google Scholar

[5] Stubican, V.S., & Hellman, J.R. (1981). Phase Equilibria in some Zirconia System. Science and Technology of Zirconia, (3), 25.

Google Scholar

[6] Vashkevich, F.F., Spilnik, A.Ya., & Esipova, E.S. (2010). Thermal technical properties of protective coatings obtained by thermal spraying. Construction, materials science, engineering. Sat. scientific labor, (55), 54-58.

Google Scholar

[7] Loshchinin, Yu.V., Razmakhov, M.G., Pakhomkin, S.I., & Lutsenko, A N. (2019). The influence of the composition and technology of applying multilayer heat-protective coatings made by gas spraying on thermal conductivity. Proceedings of VIAM, 6(78), 96-103.

Google Scholar

[8] Chubarov, D.A., & Budinovsky, S.A. (2015). The choice of ceramic material for heat-protective coatings of aircraft turbine blades for operating temperatures up to 1400ºС. Transactions of VIAM, electron. scientific - tech. Journal, (4).

Google Scholar

[9] Loshchinin, Y. V., Budinovsky, S. A., & Razmakhov, M. G. (2018). heat conductivity of heat-protective coatings ZRO2–Y2O3 alloyed by rem oxides obtained by magnetronny application. Aviation Materials and Technologies», (3), 42-49. https://doi.org/10.18577/2071-9140-2018-0-3-42-49.

DOI: 10.18577/2071-9140-2018-0-3-42-49

Google Scholar

[10] Matveev, P.V., &Budinovsky, S.A. (2014). The study of the properties of protective heat-resistant coatings for intermetallic nickel alloys type VKNA for operating temperatures up to 1300ºС. Aviation materials and technologies, 3(52). 22-26.

DOI: 10.18577/2071-9140-2014-0-3-22-26

Google Scholar

[11] Matveev, P.V., Budinovsky, S.A., & Chubarov. D.A. (2014). The technology for producing ion-plasma heat-resistant sublayers with a high aluminum content for promising TZP. Aviation materials and technologies, (5), 56-60.

Google Scholar