Email this article Increasing the lifetime of gas-turbine engine nozzle blades using a new monocrystalline alloy
- Authors: Semenov S.G.1, Getsov L.B.2, Semenov A.S.1, Petrushin N.V.3, Ospennikova O.G.3, Zhivushkin A.A.4
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Affiliations:
- Peter the Great Polytechnial University
- Polzunov Scientific-Production Association for Research and Design of Power-Generating Equipment
- All-Russia Research Institute of Aviation Materials
- Klimov
- Issue: Vol 45, No 4 (2016)
- Pages: 316-323
- Section: Realibility, Strength, and Wear Resistance of Machines and Structures
- URL: https://journals.rcsi.science/1052-6188/article/view/192874
- DOI: https://doi.org/10.3103/S1052618816040117
- ID: 192874
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Abstract
The article presents the results of experiments to study the creep of an intermetallic monocrystalline alloy used to manufacture nozzle blades. The results serve as a basis for calculating the creep-rupture strength and thermal fatigue of gas-turbine engine blades.
About the authors
S. G. Semenov
Peter the Great Polytechnial University
Author for correspondence.
Email: guetsov@yahoo.com
Russian Federation, St. Petersburg
L. B. Getsov
Polzunov Scientific-Production Association for Research and Design of Power-Generating Equipment
Email: guetsov@yahoo.com
Russian Federation, St. Petersburg
A. S. Semenov
Peter the Great Polytechnial University
Email: guetsov@yahoo.com
Russian Federation, St. Petersburg
N. V. Petrushin
All-Russia Research Institute of Aviation Materials
Email: guetsov@yahoo.com
Russian Federation, Moscow
O. G. Ospennikova
All-Russia Research Institute of Aviation Materials
Email: guetsov@yahoo.com
Russian Federation, Moscow
A. A. Zhivushkin
Klimov
Email: guetsov@yahoo.com
Russian Federation, St. Petersburg
