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Development of technology extension resource ХН65ВМТЮ alloy turbine blades
- Authors: Berdnik O.B.1, Tsareva I.N.1, Razov E.N.1
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Affiliations:
- Nizhny Novgorod branch Institutions of the Russian Academy of Sciences Institute of engineering them named A.А. Blagonravov SPC «Tribonika»
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 240-247
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6818
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-240-247
- ID: 6818
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Abstract
The goal was to examine postèkspluatacion of material working blades of gas turbine engines have a long lifespan and determining their maintainability. Looking for studies of chemical composition, microstructure, phase, physical and mechanical properties of heat-resistant nickel alloy. Have been developed for high-temperature heat treatment alloy modes (ЭИI893) to save the product.
About the authors
O. B. Berdnik
Nizhny Novgorod branch Institutions of the Russian Academy of Sciences Institute of engineering them named A.А. Blagonravov SPC «Tribonika»
Author for correspondence.
Email: tribonikanpc@mail.ru
Candidate of technical Sciences
senior researcher
I. N. Tsareva
Nizhny Novgorod branch Institutions of the Russian Academy of Sciences Institute of engineering them named A.А. Blagonravov SPC «Tribonika»
Email: tribonikanpc@mail.ru
Candidate of Phisic and Mathematik Sciences
senior researcher
E. N. Razov
Nizhny Novgorod branch Institutions of the Russian Academy of Sciences Institute of engineering them named A.А. Blagonravov SPC «Tribonika»
Email: tribonikanpc@mail.ru
researcher
Russian FederationReferences
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