Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
- Авторлар: Arkhipov A.N.1, Volgina M.V.2, Matushkin A.A.1, Ravikovich Y.A.1, Kholobtsev D.P.1
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Мекемелер:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- Шығарылым: Том 62, № 3 (2019)
- Беттер: 455-462
- Бөлім: 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
Дәйексөз келтіру
Аннотация
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.
Авторлар туралы
A. Arkhipov
Moscow Aviation Institute
Хат алмасуға жауапты Автор.
Email: arkhipov.48@list.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
M. Volgina
PAO United Engine Corporation Saturn
Email: arkhipov.48@list.ru
Ресей, ul. Lenina 163, Rybinsk, 152903
A. Matushkin
Moscow Aviation Institute
Email: arkhipov.48@list.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
Yu. Ravikovich
Moscow Aviation Institute
Email: arkhipov.48@list.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
D. Kholobtsev
Moscow Aviation Institute
Email: arkhipov.48@list.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
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