Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances


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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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