Email this article Calculation of low cycle fatigue life for gas-turbine engine critical parts
- Authors: Pakhomenkov A.V.1, Azimov R.A.1, Bukatyi S.A.2
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Affiliations:
- NPO Saturn
- P. A. Soloviev Rybinsk State Aviation Technical University
- Issue: Vol 60, No 3 (2017)
- Pages: 421-427
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230204
- DOI: https://doi.org/10.3103/S106879981703014X
- ID: 230204
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Abstract
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.
About the authors
A. V. Pakhomenkov
NPO Saturn
Email: bukaty_sa@mail.ru
Russian Federation, ul. Lenina 163, Rybinsk, 152903
R. A. Azimov
NPO Saturn
Email: bukaty_sa@mail.ru
Russian Federation, ul. Lenina 163, Rybinsk, 152903
S. A. Bukatyi
P. A. Soloviev Rybinsk State Aviation Technical University
Author for correspondence.
Email: bukaty_sa@mail.ru
Russian Federation, ul. Pushkina 53, Rybinsk, 152934
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