Some aspects of creation and research of structural casting intermetallide alloys for promising helicopter engines

Bazyleva O.A., Rimsha E.G., Chabina E.B., Raevskih A.N.
Bazyleva O.A., Rimsha E.G., Chabina E.B., Raevskih A.N. Some aspects of creation and research of structural casting intermetallide alloys for promising helicopter engines // Proceedings of VIAM. 2024. No. 3. DOI: 10.18577/2307-6046-2024-0-3-3-17. URL: https://test.viam.ru/en/journal/2024/3/1
Keywords
intermetallide, structure, phase composition, high-temperature treatment, long-term strength, nozzle blades
Abstract

The article presents the calculation of the chemical composition of the intermetallic composition based on the Ni3Al compound using the doping balance formula, while the average electron concentration is the number of valence electrons per unit atomic mass of the composition; studies of structural and phase transformations in an intermetallic alloy based on Ni3Al depending on high-temperature treatment and during long-term tests at temperatures of 1150, 1200 and 1250 °С. The constructability of the structural alloy was experimentally established when testing the casting of blanks of the nozzle blades of the compressor turbine of a promising helicopter engine.

Reference list
  1. Sims Ch., Hagel V. Superalloys II. Heat-resistant materials for aerospace and industrial power plants: in 2 books. Moscow: Metallurgiya, 1995, book 1, 384 p.
  2. Sims Ch., Hagel V. Superalloys II. Heat-resistant materials for aerospace and industrial power plants: in 2 books. Moscow: Metallurgiya, 1995, book 2, pp. 288–298.
  3. Zelenkov Yu.P., Shmotin Yu.N., Chupin P.V. Current state and prospects of supercomputer computing in the design of gas turbine engines. Vestnik Ufimskogo gosudarstvennogo aviatsionnogo universiteta, 2012, vol. 16, no. 3 (48), pp. 91–98.
  4. Shmotin Yu.N., Burov M.N. Increasing reliability and developing the power range of gas turbine units based on the GTD-110M produced by PJSC NPO Saturn. Gazoturbinnyye tekhnologii, 2017, no. 1 (144), pp. 2–4.
  5. Inozemtsev A.A. The PD-14 engine is the future of the Russian aviation industry. Innovatsii, 2019, no. 12 (182), pp. 77–80.
  6. Inozemtsev A.A. The use of promising technologies of aviation gas turbine engines for the creation of high-power power gas turbine units. Elektricheskiye stantsii, 2020, no. 1 (1062), pp. 29–35.
  7. Gladky I.L., Inozemtsev A.A., Morozova M.V. Integration of the PD-14 engine with the MS-21-310 aircraft to ensure the absence of dangerous consequences when the fan blade comes off. Aviation and Cosmonautics: abstracts 21st Int. conf. Moscow: MAI (NIU), 2022, pp. 107–108.
  8. Inozemtsev A.A., Sulimov D.D. Experience and prospects of JSC «UEC-Aviadvigatel» in the creation and operation of aircraft industrial gas turbine plants and power units. Gazoturbinnye tekhnologii, 2022, no. 5 (188), pp. 2–7.
  9. Belikov A.V., Visik E.M., Gerasimov V.V. Modernization of equipment for directional crystallization of monocrystalline castings. Liteynoe proizvodstvo, 2014, no. 4, pp. 34–36.
  10. Visik E.M., Gerasimov V.V., Kolyadov E.V., Kuzmina N.A. Influence of technological casting modes on the structural parameters of single crystals of new heat-resistant alloys. Metallurgiya mashinostroeniya, 2016, no. 5, pp. 27–31.
  11. Visik E.M., Kolyadov E.V., Chabina E.B., Kuzmina N.A. Technological possibilities for controlling the structure of castings made of heat-resistant alloys during directional crystallization. Tekhnologiya metallov, 2022, no. 1, pp. 47–56.
  12. Bondarenko Yu.A., Echin A.B. A look at the history of development and modern research into the process of directed crystallization of cast heat-resistant alloys with a controlled gradient at the growth front. Elektrometallurgiya, 2018, no. 7, pp. 33–40.
  13. 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. 89–98.
  14. Izotov V.A., Grishikhin S.A., Shatulsky A.A. Methodology for calculating the resistance coefficient of a gating system with changing pressure. Liteyshchik Rossii, 2009, no. 3, p. 39.
  15. Grishikhin S.A., Izotov V.A., Shatulsky A.A. Calculation of the flow coefficient of the gating system for various parameters of the metallostatic pressure. Vestnik RGATA im. P.A. Solovyeva, 2009, no. 1 (15), pp. 115–119.
  16. Rassokhina L.I., Parfenovich P.I., Narsky A.R. Problems of creating new generation model compositions based on domestic materials for the manufacture of gas turbine engine blades. Novosti materialovedeniya. Nauka i tekhnika, 2015, no 3 (15), paper no. 07. Available at: http://www.materialsnews.ru (accessed: December 14, 2023).
  17. Yakovlev E.I. Production of castings from heat-resistant nickel alloys with a fine-grained equiaxed structure and reduced porosity. Liteynoe proizvodstvo, 2022, no. 6, pp. 3–6.
  18. Li P., Li S.S., Han Y.F. Influence of solution heat treatment on microstructure and stress rupture properties of NI3Al base single crystal superalloy IC6SX. Intermetallics, 2011, vol. 19, is. 2, pp. 182–186.
  19. He X., Zhang J., Peng Y. et al. Microstructure evolution of primary γʹ phase in NI3Al-base superalloy. Acta metallurgica sinica, 2020, vol. 33, pp. 1709–1726.
  20. Liwu J., Xuezheng D., Meiling W. Effect of stress on creep behavior of single crystal alloy IC6SX at 980еC. International Journal of Photoenergy, 2020, vol. 3, pp. 1–5.
  21. Liwu J., Meiling W., Yafang H., Yanna C. Creep behavior and dislocation mechanism of NI3Al base single crystal alloy IC6SX at 760еC. Progress in Natural Science, 2021, vol. 9, p. 239.
  22. An alloy based on the Ni3Al intermetallic compound and a product made from it: pat. 2588949 Rus. Federation; appl. 01.04.15; publ. 10.07.16.
  23. Kablov E.N., Sidorov V.V., Kablov D.E., Min P.G., Rigin V.E. Resource-saving technologies for smelting promising cast and wrought super-heat-resistant alloys, taking into account the processing of all types of waste. Elektrometallurgiya, 2016, no. 9, pp. 30–41.
  24. Buntushkin V.P., Kablov E.N., Bazyleva O.A., Morozova G.I. Basic principles of alloying the Ni3Al intermetallic compound when creating high-temperature alloys. Materialovedenie, 1998, no. 7, pp. 13–15.
  25. Morozova G.I. Compensation for the imbalance of alloying of heat-resistant nickel alloys. Metallovedenie i termicheskaya obrabotka metallov, 2012, no. 12, pp. 52–58.
  26. Visik E.M., Gerasimov V.V., Kolyadov E.V., Filonova E.V. Features of the single-crystal structure of turbine blades made of carbon-free and carbon-containing heat-resistant nickel alloys. Zavodskaya laboratoriya. Diagnostika materialov, 2018, vol. 84, no. 6, pp. 38–43.
  27. Visik E.M., Koljadov E.V., Kuzmina N.A. Influence of directional crystallization parameters on the structure of the intermetallic nickel alloy VIN4M-VI when casting single-crystal blanks of nozzle blades. Trudy VIAM, 2023, no. 9 (127), paper no. 01. Available at: http://www.viam-works.ru (accessed: November 20, 2023). DOI: 10.18577/2307-6046-2023-0-9-3-15.
  28. Toloraya V.N., Ostroukhova G.A. Preparation of single-crystal [001] seeds from alloys of the Ni–W system by directional crystallization. Voprosy materialovedeniya, 2021, no. 2 (106), pp. 55–65.
  29. Kuzmina N.A., Pyankova L.A. Control of crystallographic orientation of monocrystalline nickel castings heat-resistant alloys by x-ray diffractometry. Trudy VIAM, 2019, no. 12 (84), paper no. 02. Available at: http://www.viam-works.ru (accessed: November 24, 2023). DOI: 10.18577/2307-6046-2019-0-12-11-19.
  30. Bazyleva O.A., Arginbaeva E.G., Shestakov A.V., Fesenko T.V. Structure and properties of an intermetallic alloy based on nickel aluminide microalloyed with rare earth metals. Voprosy materialovedeniya, 2018, no. 1 (93), pp. 35–49.
  31. Bazyleva O.A., Karashaev M.M., Shestakov A.V., Arginbaeva E.G. Effect of annealing temperature on the homogeneity of intermetallic alloy based on Ni3Al compound. Trudy VIAM, 2020, no. 8 (90), paper no. 01. Available at: http://www.viam-works.ru (accessed: November 24, 2023). DOI: 10.18577/2307-6046-2020-0-8-3-10.
  32. Bazyleva O.A., Arginbaeva E.G., Chabina E.B., Raevskikh A.N. Study of structural-phase transformations in a cast structural alloy based on the Ni3Al intermetallic compound after high-temperature holding and during the process of operating the alloy as a nozzle blade. Voprosy materialovedeniya, 2023, vol. 114, no. 2, pp. 60–70.
  33. Artemenko N.I. Features of the surface condition of gas-thermal coatings obtained by atmospheric plasma spraying. Elektrometallurgiya, 2020, no. 2, pp. 25–31.
  34. Artemenko N.I., Barinov D.Ya., Akopyan A.G. Study of the thermophysical properties of the ceramic material ZrO2–7%Y2O3, obtained by various methods, used for applying a heat-protective coating. Elektrometallurgiya, 2022, no. 5, pp. 24–29.
  35. Artemenko N.I., Tatarnikov S.V., Doronin O.N. Investigation of the influence of the parameters of applying the ceramic layer of the ZrO2–7%Y2O3 heat-shielding coating by plasma spraying on the productivity of the technological process. Trudy VIAM, 2023, no. 4 (122), paper no. 07. Available at: http://www.viam-works.ru (accessed: November 24, 2023). DOI: 10.18577/2307-6046-2023-0-4-69-80.
  36. Chabina E.B., Alekseev A.A., Filonova E.V., Lukinа E.A. The use of methods of analytical microscopy and x-ray diffraction analysis for the study of the structural phase state materials. Trudy VIAM, 2013, no. 5, paper no. 06. Available at: http://www.viam-works.ru (accessed: November 27, 2023).
  37. Kablov E.N. Innovative developments of FSUE «VIAM» SSC of RF on realization of «Strategic directions of the development of materials and technologies of their processing for the period until 2030». Aviacionnye materialy i tehnologii, 2015, no. 1 (34), pp. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-3.