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, 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,
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.