Email this article Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
- Authors: Arkhipov A.N.1, Volgina M.V.2, Matushkin A.A.1, Ravikovich Y.A.1, Kholobtsev D.P.1
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Affiliations:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- Issue: Vol 62, No 3 (2019)
- Pages: 455-462
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/231056
- DOI: https://doi.org/10.3103/S1068799819030139
- ID: 231056
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Abstract
The results of the probabilistic assessment of life for the low-pressure compressor rotor of the gas turbine engine for a regional aircraft are presented taking into account production tolerances. The calculation algorithm, preparation of the probabilistic model parameters, and the experimental program of automated probabilistic analysis are described, the example of the life calculation results is given.
About the authors
A. N. Arkhipov
Moscow Aviation Institute
Author for correspondence.
Email: arkhipov.48@list.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
M. V. Volgina
PAO United Engine Corporation Saturn
Email: arkhipov.48@list.ru
Russian Federation, ul. Lenina 163, Rybinsk, 152903
A. A. Matushkin
Moscow Aviation Institute
Email: arkhipov.48@list.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
Yu. A. Ravikovich
Moscow Aviation Institute
Email: arkhipov.48@list.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
D. P. Kholobtsev
Moscow Aviation Institute
Email: arkhipov.48@list.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
