Отправить статью по E-mail Increasing the lifetime of gas-turbine engine nozzle blades using a new monocrystalline alloy
- Авторы: Semenov S.1, Getsov L.2, Semenov A.1, Petrushin N.3, Ospennikova O.3, Zhivushkin A.4
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Учреждения:
- 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
- Выпуск: Том 45, № 4 (2016)
- Страницы: 316-323
- Раздел: 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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Аннотация
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.
Об авторах
S. Semenov
Peter the Great Polytechnial University
Автор, ответственный за переписку.
Email: guetsov@yahoo.com
Россия, St. Petersburg
L. Getsov
Polzunov Scientific-Production Association for Research and Design of Power-Generating Equipment
Email: guetsov@yahoo.com
Россия, St. Petersburg
A. Semenov
Peter the Great Polytechnial University
Email: guetsov@yahoo.com
Россия, St. Petersburg
N. Petrushin
All-Russia Research Institute of Aviation Materials
Email: guetsov@yahoo.com
Россия, Moscow
O. Ospennikova
All-Russia Research Institute of Aviation Materials
Email: guetsov@yahoo.com
Россия, Moscow
A. Zhivushkin
Klimov
Email: guetsov@yahoo.com
Россия, St. Petersburg
