Development of technologies and equipment for producing blades of the hot path of gas turbine engines from superalloys with directional and single-crystal structure

Bondarenko Yu.A., Echin A.B., Narskiy A.R.
Bondarenko Yu.A., Echin A.B., Narskiy 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 // Proceedings of VIAM. 2023. No. 7. DOI: 10.18577/2307-6046-2023-0-7-3-14. URL: https://test.viam.ru/en/journal/2023/7/1
Keywords
directed crystallization of superalloy, gas turbine engines, plant design, temperature gradient, dendritic structure, liquid metal cooler
Abstract

A description of the development of the technology for obtaining parts of the hot path of gas turbine engines by the method of directed crystallization from superalloys are considered. The analysis of the existing specialized equipment used in Russia, the USA, Germany and other countries to produce blades with a directional and monocrystalline structure is carried out. The prospects of the method of directed crystallization with a liquid-metal cooler in the production of gas turbine engine blades for both modern and promising gas turbine engines are clearly demonstrated.

Reference list
  1. Kablov E.N. Cast blades of gas turbine engines: alloys, technologies, coatings. 2nd ed. Moscow: Nauka, 2006, 632 p.
  2. Kablov E.N. Developments of VIAM for gas turbine engines and installations. Krylya Rodiny, 2010, no. 4, рр. 31–33.
  3. Weingard U. Introduction to the physics of crystallization of metals. Moscow: Mir, 1967, 172 p.
  4. Walston S., Cetel A., MacKay R. et al. Joint development of a fourth generation single crystal superalloys. Superalloys 2004. Minerals, Metals & Materials Society, 2004, рр. 15–24.
  5. Chumakov V.A., Stepanov V.M., Ivanov B.G., Belyaeva I.G., Verin A.S., Sobolev G.I. Casting technology for gas turbine engine blades using the directional crystallization method. Liteynoe proizvodstvo, 1978, no. 1, pp. 23–24.
  6. History of aviation materials science. VIAM – 80 years: years and people. Ed. E.N. Kablov. Moscow: VIAM, 2012, 520 p.
  7. Logunov A.V., Burov M.N., Danilov D.V. Development of power and marine engine building in the world: a review. Part 1. Dvigatel, 2016, no. 1 (103), pp. 10–13.
  8. Giamei A.F., Tschinkel J.G. Liquid Metal Cooling: A New Solidification Technique. Metallurgical Transactions A, 1976, vol. 7A, pp. 1427–1434.
  9. Lohmuller A., Eber W., Grobmann J. et al. Improved Quality and Economics of Investment Castings by Liquid Metal Cooling – the Selection of Cooling Media. Superalloys 2000. The Minerals, Metals & Materials Society, 2000, pp. 181–188.
  10. Hugo F., Betz U., Ren J. et al. Casting of Directionally Solidified and Single Crystal Components Using Liquid Metal Cooling (LMC): Results from Experimental Trials and Computer Simulations. International Symposium on Liquid Metal Processing and Casting. VMD-AVS, 1999, pp. 16–30.
  11. Elliott A.J., Tin S., King W.T. et al. Directional Solidification of Large Superalloy Casting with Radiation and Liquid-Metal Cooling: A Comparative Assessment. Metallurgical and Materials Transactions A, 2004, vol. 35A, no. 3, pp. 3221–3231.
  12. Miller J.D., Pollock T.M. Process Simulation for the Directional Solidification of a Tri-Crystal Ring Segment via the Bridgman and Liquid-Metal-Cooling Processes. Metallurgical and Materials Transactions A, 2012, vol. 43A, pp. 2414–2425.
  13. Pankratov V.A., Kablov E.N. Incubator for turbine blades. Nauka i zhizn, 1991, no. 8, pp. 62–64.
  14. Gerasimov V.V., Visik E.M., Kolyadov E.V. Mastering the technology of directional crystallization of large-sized castings at the UVNK-15 unit. Liteynoe proizvodstvo, 2014, no. 3, pp. 28–31.
  15. Kolyadov EV, Visik EM, Gerasimov VV, Arginbaeva E.G. The influence of directional solidification parameters on the structure and properties of the intermetallic alloys. Trudy VIAM, 2019, no. 3 (75), paper no. 02. Available at: http://www.viam-works.ru (accessed: March 23, 2023). DOI: 10.18577/2307-6046-2019-0-3-14-26.
  16. Bondarenko Yu.A. Trends in the development of high-temperature metal materials and technologies in the production of modern aircraft gas turbine engines. Aviacionnye materialy i tehnologii, 2019, no. 2 (55), pp. 3–11. DOI: 10.18577/2071-9140-2019-0-2-3-11.
  17. Bondarenko Yu.A., Kolodyazhnyj M.Yu., Echin A.B., Narskij A.R. Directional solidification, structure and properties of natural composite based on eutectic Nb–Si at working temperatures up to 1350 °С degrees for the blades of gas turbine engines. Trudy VIAM, 2018, no. 1 (61), paper no. 01. Available at: http://www.viam-works.ru (accessed: March 24, 2023). DOI: 10.18577/2307-6046-2018-0-1-1-1.
  18. Bazyleva O.A., Arginbayeva E.G., Lutskaya S.A., Dmitriev N.S. Foundry intermetallic alloy based on Ni3Al compound for turbine blades gas turbine engines. Aviation materials and technologies, 2022, no. 2 (67), paper no. 01. Available at: http://www.journal.viam.ru (accessed: March 30, 2023). DOI: 10.18577/2713-0193-2022-0-2-5-17.