ArticleName |
Controlling the structure formation
of heat-resistant nickel-based alloys, when manufacturing large gas turbine blades |
ArticleAuthorData |
Scientific Production Association Technopark of Aviation Technologies, Ufa, Russia
I. V. Kandarov, Director, Candidate of Technical Sciences, e-mail: tpat@tp-at.ru V. M. Piksaev, Head of the Casting Technology Department, Candidate of Technical Sciences, e-mail: vasiliypiksaev@mail.ru
Kazan (Volga Region) Federal University, Kazan, Russia D. L. Pankratov, Head of the Mechanical Engineering Department, Doctor of Technical Sciences, e-mail: pankratovdl@gmail.com V. G. Shibakov, Mechanical Engineering Department, Doctor of Technical Sciences, e-mail: vladshib50@gmail.com |
Abstract |
Heat-resistant alloys are widely used in hot sections of aviation engines and ground-mounted power gas turbines due to their strength at higher temperatures and high hot corrosion resistance. To increase life of the gas turbine, there are various technological methods; one of them is to influence the structure and properties. The article describes the results of using a combined technological system to achieve a fine-grain structure of large blades (up to 900 mm) from heat-resistant nickel alloy IN792-5А. It has been shown that the best result will be achieved by harmonizing technological effects, entailing a positive synergetic effect. The article presents the results of applying integrated heat treatment, and surface modification. The authors selected process modes to minimize γ'-phase in the body of the cast workpiece. The object under study was the cast workpiece of the operating blade of stage 4. The studies were conducted to develop a technological system for manufacturing large gas turbine blades, potentially ensuring a macro- and microstructure specified by customers and the required operational properties; to study a technological system as an object of control to comply with customers’ requirements; to determine reasonable parameters of processes as part of the technological system under study. To achieve the objectives, the authors solved the following issues: finding the dependence between the effect of casting process parameters and the macrostructure and studying the effect of applying a modifier on the macrostructure. |
References |
1. Kablov E. N. Cast gas turbine engine blades. Moscow : Nauka, 2006. 632 p. 2. Gadalov V. N., Skripkina Yu. V., Gvozdev A. E., Kutepov S. N. et al. Fundamentals of increasing heat resistance of cast nickel-based complex alloys. Izvestiya TulGU. Tekhnicheskie nauki. 2021. No. 5. pp. 583–593. DOI: 10.24412/2071-6168-2021-5-583-593. 3. Kablov E. N., Bratukhin A. G., Shalin R. E. Cast single-crystal turbine blades. Liteynoe proizvodstvo. 1993. No. 6. pp. 3–6. 4. McLean M., Schubert F. Mechanical properties of heat-temperature alloys and directed crystallization eutectic. Moscow : Metallurgiya. 1981. pp. 212–237. 5. Ivanov V. N., Kazennov S. A., Kurchman B. S. et al. Investment casting. Ed. by Shklennik Ya. I., Ozerov V. A. 3rd ed., updated and revised. Moscow : Mashinostroenie, 1984. 408 p. 6. Jonsta Z., Jonsta P., Mazanec K. Microstructural material analysis of superalloy INCONEL 792-5a after high temperature exposition. Communications — Scientific Letters of the University of Zilina. 2009. Vol. 11, No. 1. pp. 34–38. 7. GOST 9391–80. Sintered hardmetals. Methods for determination of porosity and microstructure. Introduced: 01.01.1983. 8. GOST 7512–82. Nondestructive testing. Welded joints. Radiography method. Introduced: 01.01.1984. 9. Flek M. B., Boguslavskiy I. V., Ugnich E. A. Synergistic effects management as the basic driver of enterprise development under current conditions. Advanced Engineering Research (Rostov-on-Don). 2014. Vol. 14, No. 4. pp. 203–209. 10. Shuo Ma, Xiaobin Yang, Liming Fu, Aidang Shan. Achieving high strength-ductility synergy in nickel aluminum bronze alloy via a quenchingaging-tempering heat treatment. Materials Letters. 2023. Vol. 333. 133661. DOI: 10.1016/j.matlet.2022.133661 11. Lysenko N. A., Klochikhin V. V., Temkin D. A. Effect of modifying with titanium carbonitride on the structure and properties of heat-resistant alloy ZhS3DK-VI with a reduced content of carbon. Vestnik dvigatelestroeniya. 2013. No. 1. pp. 109–115. 12. Semenchenko I. V., Mirer Ya. G. Increasing reliability of gas turbine engine blades by technological methods. Moscow : Mashinostroenie, 1977. 160 p. 13. Mengting Zhang, Xinghua Liang, Xiaofeng Zhang, Min Liu et al. Effects of heat treatment on microstructure and properties of inconel 625 alloy blades prepared by selective laser melting. International Journal of Electrochemical Science. 2022. Vol. 17, No. 1. 220112. DOI: 10.20964/2022.01.22 14. Epishin A., Fedelich B., Link T., Feldmann T. et al. Pore annihilation in a single-crystal nickel-base superalloy during hot isostatic pressing: Experiment and modeling. Materials Science and Engineering: A. 2013. Vol. 586. pp. 342–349. 15. Morozova G. I. Phenomenon of γ'-phase in heat-resistant nickel alloys. Doklady Akademii nauk. 1992. Vol. 325, No. 6. 11 p. 16. Novikov I. I. Theory of heat treatment of metals. Moscow : Metallurgiya, 1978. 392 p. 17. Kandarov I. V., Pankratov D. L., Piksaev V. M., Kashapov F. F., Ishmuratov F. A. Obtaining a fine-grained structure of large-sized blades made of heat-resistant nickel alloy IN792. Bulletin of PNRPU. Mechanical Engineering, Materials Science. 2022. No. 3. pp. 64–70. |