1. 1. Peychev, G.I., Zamkovoy, V.E., Kalashnikov, G.P. et al. (2005) Repair of structural elements worn out in the process of operation of the truss shelves of cast working blades of the turbine made of alloys of the ZS type. Aviats.-Kosmich. Tekhnika i Tekhnologiya, 9(25), 221-223 [in Russian].
2. 2. Yushchenko, K.A., Savchenko, V.S., Yarovitsyn, A.V. et al. (2010) Development of the technology for repair microplasma powder cladding of flange platform faces of aircraft engine high-pressure turbine blades. The Paton Welding J., 8, 21-24.
3. 3. Zhemanyuk, P.D., Petrik, I.A., Chigilejchik, S.L. (2015) Experience of introduction of the technology of reconditioning microplasma powder surfacing at repair of high-pressure turbine blades in batch production. The Paton Welding J., 8, 43-46. DOI: https://doi.org/10.15407/tpwj2015.08.08
4. 4. Yushchenko, K. A., Yarovytsyn, O. V., Khrushchov, G. D. et al. (2022) Research and optimization of refurbishment of HPT blades of the D-18T aircraft gas turbine engine by microplasma powder welding. Kosmichna Nauka i Tekhnologiya, 3(28), 3-16. DOI: https://doi.org/10.15407/knit2022.03.01-01 [in Ukrainian].
5. 5. Zhemanyuk, P., Klochyhyn, V., Lysenko, N., Naumyk, V. (2015) Structure and properties of cast aircraft engines blades (HA26-VI alloy) from heatproof nickeliferrous alloy after hot isostatic pressing. Vestnik Dvigatelestroeniya, 1, 139-146 [in Russian].