The Paton Welding Journal, 2011, #9, 22-26 pages
OPTIMIZATION OF CONDITIONS OF REDUCTION HEAT TREATMENT OF BLADES OF ALLOY KhN65VMTYu AFTER LONG-TERM SERVICE
Yu.P. TARASENKO, O.B. BERDNIK and I.N. TSARYOVA
A.A. Blagonravov Institute of Engineering Science, RAS, Novgorod, Russian Federation
Abstract
Condition of the material of gas turbine engine blades after long-term service was studied and their repairability was determined. Parameters were developed for high-temperature heat treatment of alloy KhN65VMTYu (EI893) to extend the service life of product.
Keywords: blades, reduction heat treatment, microstructure, physical-mechanical properties, extension of service life
Received: ??.??.??
Published: 28.09.11
References
1. Getsov, L.B. (2010) Materials and strength of gas turbine parts. Book 1. Rybinsk: Gazoturb. Tekhnologii.
2. Rybnikov, A.I., Getsov, L.B. (1995) Heat treatment of coated blades. Metallovedenie i Termich. Obrab. Metallov, 9, 21-25.
3. Filatov, M.A., Sudakov, V.S. (1995) Effect of heat treatment on structure and properties of heat-resistant nickel alloys. Ibid., 6, 12-15.
Suggested Citation
Yu.P. TARASENKO, O.B. BERDNIK and I.N. TSARYOVA (2011) OPTIMIZATION OF CONDITIONS OF REDUCTION HEAT TREATMENT OF BLADES OF ALLOY KhN65VMTYu AFTER LONG-TERM SERVICE.
The Paton Welding J., 09, 22-26.