Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
- 作者: Arkhipov A.N.1, Volgina M.V.2, Matushkin A.A.1, Ravikovich Y.A.1, Kholobtsev D.P.1
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隶属关系:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- 期: 卷 62, 编号 3 (2019)
- 页面: 455-462
- 栏目: 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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详细
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.
作者简介
A. Arkhipov
Moscow Aviation Institute
编辑信件的主要联系方式.
Email: arkhipov.48@list.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
M. Volgina
PAO United Engine Corporation Saturn
Email: arkhipov.48@list.ru
俄罗斯联邦, ul. Lenina 163, Rybinsk, 152903
A. Matushkin
Moscow Aviation Institute
Email: arkhipov.48@list.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
Yu. Ravikovich
Moscow Aviation Institute
Email: arkhipov.48@list.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
D. Kholobtsev
Moscow Aviation Institute
Email: arkhipov.48@list.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
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