Boguslaev VA, Muravchenko FM, Zhemanyuk PD, Kolesnikov VI, Yatsenko VK, Orlov MR, et al. Technological Support of Operational Characteristics of Gas Turbine Engine Parts. Part 1. Compressor and Fan Blades. Zaporozhye: Motor Sich; 2003. (In Russian)
Zheng J, Li Z, Chen X. Worn area modeling for automating the repair of turbine blades. The International Journal of Advanced Manufacturing Technology. 2006; (29): 1062–1067. https://doi.org/10.1007/s00170-003-1990-6.
Petrik IA, Perimilovskiy IA. Further development of the technology for strengthening the shroud shelves of turbine blades made of heat-resistant alloys. Technological Systems [Tekhnologicheskie sistemy]. 2001; (3): 90–92. (In Russian)
Kermanpur A, Amin SH, Ziaei-Rad S, Nourbakhshnia N. Failure characterisation of Ti6Al4V gas turbine compressor blades. WIT Trans. Eng. Sci. 2007; 57: 383–392.
Kermanpur A, Amin SH, Ziaei-Rad S, Nourbakhshnia N, Mosaddeghfar M. Failure analysis of Ti6Al4V gas turbine compressor blades. Eng. Failure Anal. 2008; 15(8): 1052–1064. https://doi.org/10.1016/j.engfailanal.2007.11.018.
Rottwinkel B, Nölke C, Kaierle S, Wesling V. Laser cladding for crack repair of CMSX-4 single-crystalline turbine parts. Lasers in Manufacturing and Materials Processing. 2017; 4: 13–23. https://doi.org/10.1007/s40516-016-0033-8.
Farafonov DP, Degovets ML, Rogalev AM. Research of experimental compositions of wear-resistant alloys on the basis of cobalt for repair and hardening of working blades of high-pressure turbines by method of laser welding. Proceedings of VIAM [Trudy VIAM]. 2017; 56(8): article ID 5. https://doi.org/10.18577/2307‑6046‑2017‑0‑8‑5‑5. (In Russian)
Company “Auremo”. Alloy ЧС-70. Available from: https://auremo.biz/materials/splav-chs70.html [Accessed: 2 November 2024]. (In Russian)
European Metallurgical Company. Homepage. Available from: https://emk24.ru/ [Accessed: 2 November 2024]. (In Russian)