Enviar artigo por via de e-mail Increasing the lifetime of gas-turbine engine nozzle blades using a new monocrystalline alloy
- Autores: 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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Afiliações:
- 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
- Edição: Volume 45, Nº 4 (2016)
- Páginas: 316-323
- Seção: 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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Resumo
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.
Sobre autores
S. Semenov
Peter the Great Polytechnial University
Autor responsável pela correspondência
Email: guetsov@yahoo.com
Rússia, St. Petersburg
L. Getsov
Polzunov Scientific-Production Association for Research and Design of Power-Generating Equipment
Email: guetsov@yahoo.com
Rússia, St. Petersburg
A. Semenov
Peter the Great Polytechnial University
Email: guetsov@yahoo.com
Rússia, St. Petersburg
N. Petrushin
All-Russia Research Institute of Aviation Materials
Email: guetsov@yahoo.com
Rússia, Moscow
O. Ospennikova
All-Russia Research Institute of Aviation Materials
Email: guetsov@yahoo.com
Rússia, Moscow
A. Zhivushkin
Klimov
Email: guetsov@yahoo.com
Rússia, St. Petersburg
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