Отправить статью по E-mail Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
- Авторы: Arkhipov A.1, Volgina M.2, Matushkin A.1, Ravikovich Y.1, Kholobtsev D.1
-
Учреждения:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- Выпуск: Том 62, № 3 (2019)
- Страницы: 455-462
- Раздел: 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
Цитировать
Открытый доступ
Доступ предоставлен
Только для подписчиков
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.
Об авторах
A. Arkhipov
Moscow Aviation Institute
Автор, ответственный за переписку.
Email: arkhipov.48@list.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
M. Volgina
PAO United Engine Corporation Saturn
Email: arkhipov.48@list.ru
Россия, ul. Lenina 163, Rybinsk, 152903
A. Matushkin
Moscow Aviation Institute
Email: arkhipov.48@list.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
Yu. Ravikovich
Moscow Aviation Institute
Email: arkhipov.48@list.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
D. Kholobtsev
Moscow Aviation Institute
Email: arkhipov.48@list.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
