Study of the feasibility of using intermetallic alloy VKNA-1V mono instead of alloy VKNA-1VR for the manufacture of nozzle blades of a high-pressure turbine of a promising gas turbine engine

Rimsha E.G., Bazyleva O.A., Lutskaya S.A., Artemenko J.V.
Rimsha E.G., Bazyleva O.A., Lutskaya S.A., Artemenko J.V. Study of the feasibility of using intermetallic alloy VKNA-1V mono instead of alloy VKNA-1VR for the manufacture of nozzle blades of a high-pressure turbine of a promising gas turbine engine // Proceedings of VIAM. 2026. No. 5. DOI: 10.18577/2307-6046-2026-0-5-13-24. URL: https://test.viam.ru/en/journal/2026/5/2
Keywords
intermetallic, compound Ni3Al, balance of alloying, composition of the alloy, phase, polycrystalline structure, monocrystalline structure, mechanical properties, long-term strength
Abstract

The article presents comparative studies of the structure, phase composition, mechanical properties and long-term strength of casting structural alloys based on the Ni3Al compound VKHA-1VR with a polycrystalline structure and VKHA-1V Mono in two crystallographic orientations [111] and [001]. It is shown that the intermetallic alloys calculated taking into account the balance of alloying have passed technological testing with a positive result in the manufacture of castings of nozzle blades of a high-pressure turbine. VKNA-1VR alloy nozzle blades were also used on a promising gas turbine engine with positive results.

Reference list
  1. Portnoy K.I., Buntushkin V.P., Bogdanov V.I. et al. Influence of Alloying on the Thermodynamic Stability of Phases in the Ni–Al System. Doklady Akademii nauk SSSR, 1980, vol. 252, no. 1, рр. 209–214.
  2. Kishkin S.T., Portnoy K.I., Buntushkin V.P. et al. Theoretical Research of High-Temperature Nickel and Intermetallic Materials. Aviation Materials. Moscow: ONTI VIAM, 1982, рр. 27–34.
  3. Grinberg B.A., Ivanov M.A. Ni3Al and TiAl intermetallides: microstructure, deformation behavior. Ekaterinburg: Publ. House of Institute of Metal Physics UB of RAS, 2002, 359 p.
  4. Povarova K.B., Drozdov A.A., Buntushkin V.P. Special-Light High-Temperature Nanostructured Ni3Al-Based Alloys for Aviation Engine and Power Engineering. Voprosy materialovedeniya, 2008, no. 2 (54), рp. 85–93.
  5. Wahl J.B., Harris K. New Single crystal superalloys, CMSX-7 and CMSX-8. Superalloys 2012. Cham: Springer Nature, 2012, pp. 179–188.
  6. Petrushin N.V., Epishin A.I., Svetlov I.L., Nolze G., Elutin E.S., Solovyov A.E. Influence of sign /ʹ-misfite on the structure and long-term strength of single crystals of nickel heat-resistant alloys. Materialovedenie, 2022, no. 2, pp. 21–31.
  7. Chabina E.B., Petrushin N.V., Filonova E.V., Yelutin E.S., Raevsky A.N. Evolution of the structure and phase composition of the material of working blades made of ZhS32 alloy as a result of operational factors. New materials and technologies for processing raw materials – the basis of innovative development of Russia: Materials of the III Int. Sc. and Tech. Conf. Moscow, 2022, pp. 85–97.
  8. Bityutskaya O.N., Petrushin N.V., Rassokhina L.I., Avdeev V.V. Casting of turbine blades from a new generation of heat-resistant nickel alloy VZhL21 with a polycrystalline structure. Klimov readings-2024: Promising directions for the development of aircraft engine building: coll. of articles of a sc. and tech. conf. St. Petersburg, 2024, pp. 373–381.
  9. Kablov E.N., Lomberg B.S., Buntushkin V.P. Intermetallic alloy Ni3AI a promising material for turbine blades. Metallovedenie i termicheskaya obrabotka metallov, 2002, no. 7, pp. 15–20.
  10. Povarova K.B. Physical and Chemical Principles of Creating Thermally Stable Alloys Based on Transition Metals. Materialovedenie, 2007, no. 12, pp. 20–27.
  11. Buntushkin V.P., Bazyleva O.A., Burkina V.I. High-temperature heat-resistant alloys based on intermetallic Ni3Al for parts of the hot path of the gas turbine engine. Avaitsionnaya promyshlennost, 2007, no. 2, pp. 41–43.
  12. Kablov E.N., Buntushkin V.P., Bazyleva O.A. Structural heat-resistant materials based on the Ni3Al compound for hot-path parts of gas-turbine engines. Tekhnologiya legkih splavov, 2007, no. 2, pp. 75–80.
  13. Wufeng D., Tietao Zh., Heli L. et al. Effects of hafnium and yttirium on the oxidation resistence of Ni3Al/ CrMoB alloy. Rare Metal Materials and Engineering, 2008, no. 37, р. 1549.
  14. Stepanova N.N., Rinkievich A.B., Mitrokhin Yu.S. Physical Properties of Ni3Al Alloyed with a Third Element: Experiment and Modeling. Ekaterinburg: Publ. House of Institute of Metal Physics UB of RAS, 2010, 175 р.
  15. Jozwik P., Polkowski W., Bojar Z. Applications of Ni3Al Based Intermetallic Alloys–Current Stage and Potential Perceptivities. Materials, 2015, no. 8, pp. 2537–2568.
  16. Bazyleva O.A., Ospennikova O.G., Arginbaeva E.G., Letnikova E.Yu., Shestakov A.V. Development trends of nickel-based intermetallic alloys. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 104–115. DOI: 10.18577/2071-9140-2017-0-S-104-115.
  17. Bazyleva O.A., Arginbaeva E.G., Echin A.B., Shestakov A.V. Influence mickoalloying with rare earch metals and production technology of structural intermetallidу alloy based on nickel aluminide on alloy properties. Inorganic Materials: Applied Research, 2017, vol. 8, no. 1, pp. 14–20.
  18. Drozdov A.A., Povarova K.B., Bazyleva O.A. et al. Intermetallic alloys based on ʹ Ni3Al. Part I. Peculiarities of structure, formation (ʹ+) of structures and alloying. Perspektivnye materialy, 2023, no. 9, pp. 5–25.
  19. Structure and Properties of Intermetallic Materials with Nanophase Hardening. Eds. E.N. Kablov, Yu.R. Kolobov. Moscow: MISIS Publ. House, 2008, 327 p.
  20. Sidorov V.V., Rigin V.E., Goryunov A.V., Kablov D.E. High-Efficiency technologies and modern equipment for the production of foundry blanks from heat-resistant alloys. Metallurg, 2012, no. 5, pp. 26–30.
  21. Sidorov V.V., Kablov E.N., Rigin V.E. Metallurgy of foundry heat-resistant alloys: technologies and equipment. Ed. E.N. Kablov. Moscow: VIAM, 2016, pp. 280–285.
  22. Bondarenko Yu.A., Echin A.B., Surova V.A., Narsky A.R. On the Directed Crystallization of Heat-Resistant Alloys Using a Cooler. Liteynoe proizvodstvo, 2011, no. 5, pp. 36–39.
  23. Visik E.M., Rassokhina L.I., Echin A.B., Gamazina M.V. On Some Aspects of Improving the Quality of Cast Turbine Blades of Gas-Turbine Engines Made of Heat-Resistant Nickel Alloys. Voprosy materialovedeniya, 2021, no. 4 (108), pp. 82–98.
  24. Kuzmina N.A., Lifshitz V.A., Potrakhov E.N., Potrakhov N.N. Specificity of application of x-ray methods of «swing» and Laue in determining the quality of the structure of castings of nickel heat-resistant alloys. Trudy VIAM, 2021, no. 8 (102), pp. 75–83. Available at: http://www.viam-works.ru (accessed: November 10, 2025). DOI: 10.18577/2307-6046-2021-0-8-75-83.
  25. Yakovlev E.I. Production of castings from heat-resistant nickel alloys with fine-grained equiaxial structure and reduced porosity. Liteynoe proizvodstvo, 2022, no. 6, pp. 3–6.
  26. Narsky A.R., Deynega G.I., Kuzmina I.G. Obtaining a fine-grained structure of castings from nickel superalloys using a cobalt aluminate modifier. Aviation materials and technologies, 2023, no. 3 (72), pp. 3–14. Available at: http://www.journal.viam.ru (accessed: November 10, 2025). DOI: 10.18577/2713-0193-2023-0-3-3-14.
  27. Bondarenko Yu.A., Echin A.B., Surova V.A., Narsky A.R. Development of technologies and equipment for producing blades of the hot path of gas turbine engines from superalloys with directional and single-crystal structure. Trudy VIAM, 2023, no. 7 (125), pp. 3–14. Available at: http://www.viam-works.ru (accessed: November 10, 2025). DOI: 10.18577/2307-6046-2023-0-7-3-14.
  28. Kolyadov E.V., Visik E.M., Gerasimov V.V., Bityutskaya O.N. Features of the morphology of the structure of nickel superalloy depending on the values of the axial and radial temperature gradients at the crystallization front. Aviation materials and technologies, 2024, no. 2 (75), pp. 15–24. Available at: http://www.journal.viam.ru (accessed: November 10, 2025). DOI: 10.18577/2713-0193-2024-0-2-15-24.
  29. Min P.G., Vadeev V.E., Min M.G. Development and implementation in production of the new single-crystal high-temperature nickel alloy for casting of gas turbine blades for the prospective engine PD-8. Aviation materials and technologies, 2025, no. 1 (78), pp. 3–17. Available at: http://www.journal.viam.ru (accessed: November 10, 2025). DOI: 10.18577/2713-0193-2025-0-1-3-17.
  30. Morozova G.I. The Role of Electronic and Dimensional Factors in the Self-Organization of the '-Phase and Its Stability. Doklady Akademii nauk SSSR, 1986, vol. 288, no. 6, рp. 1415–1418.
  31. Morozova G.I. Compensation of Alloying Imbalance in Heat-Resistant Nickel Alloys. Metallovedenie i termicheskaya obrabotka metallov, 2012, no. 12, pp. 52–58.
  32. Alekseev A.V., Yakimovich P.V. Application of the glow discharge high resolution mass spectrometry method in analysis of nickel alloys. Trudy VIAM, 2020, no. 8 (90), pp. 101–108. Available at: http://www.viam-works.ru (accessed: November 10, 2025). DOI: 10.18577/2307-6046-2020-0-8-101-108.
  33. Sidorov V.V., Kablov D.E., Chabina E.B. et al. Influence of Impurities and Microalloying on the Structure and Performance Properties of Single Crystals of High-Temperature Nickel Alloys. Ed. E.N. Kablov. Moscow: VIAM, 2020, pp. 98–105.
  34. Khodinev I.A., Monin S.A., Gorbovets M.A. Research of the Characteristics of Low-Cycle Fatigue of the Heat-Resistant Nickel Alloy VKNA-1VR. Physical and Mechanical Tests, Strength, and Reliability of Structural and Functional Materials: Materials of the XIV All-Rus. Conf. on Testing and Research of Material Properties «TestMat». Moscow, 2022, рр. 41–64.