Enviar artigo por via de e-mail Calculation of low cycle fatigue life for gas-turbine engine critical parts
- Autores: Pakhomenkov A.V.1, Azimov R.A.1, Bukatyi S.A.2
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Afiliações:
- NPO Saturn
- P. A. Soloviev Rybinsk State Aviation Technical University
- Edição: Volume 60, Nº 3 (2017)
- Páginas: 421-427
- Seção: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230204
- DOI: https://doi.org/10.3103/S106879981703014X
- ID: 230204
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Resumo
The paper presents a technique of calculating the life for gas turbine engine parts in a low cycle area based on the influence coefficients taking into account analytical and operational factors. A statistical method is used to determine the influence coefficients.
Sobre autores
A. Pakhomenkov
NPO Saturn
Email: bukaty_sa@mail.ru
Rússia, ul. Lenina 163, Rybinsk, 152903
R. Azimov
NPO Saturn
Email: bukaty_sa@mail.ru
Rússia, ul. Lenina 163, Rybinsk, 152903
S. Bukatyi
P. A. Soloviev Rybinsk State Aviation Technical University
Autor responsável pela correspondência
Email: bukaty_sa@mail.ru
Rússia, ul. Pushkina 53, Rybinsk, 152934
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