Wear and Erosion Resistance of Aircraft Engine Composite Elements in a Gas Abrasive Flow
- Авторы: Zinin A.V.1, Dobrovol’skii S.V.1, Lebedev A.K.1, Krupennikov V.A.2, Shevyakov A.O.1
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Учреждения:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- Выпуск: Том 62, № 4 (2019)
- Страницы: 696-703
- Раздел: Aircraft Production Technology
- URL: https://journals.rcsi.science/1068-7998/article/view/231197
- DOI: https://doi.org/10.3103/S1068799819040226
- ID: 231197
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Аннотация
The results of the experimental study of the structural carbon fiber reinforced plastic (CFRP) erosion resistance applied to gas turbine engine structural elements are presented. A methodology for characterizing the process of gas abrasive wear of thin-walled structures made of polymer composite materials has been developed. The factors are found that determine the level of the abrasive effect of dust and gas mixture formed at the take-off and landing. A criterion for material erosion resistance assessment is presented.
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Об авторах
A. Zinin
Moscow Aviation Institute
Автор, ответственный за переписку.
Email: allzin@yandex.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
S. Dobrovol’skii
Moscow Aviation Institute
Email: allzin@yandex.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Lebedev
Moscow Aviation Institute
Email: allzin@yandex.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
V. Krupennikov
PAO United Engine Corporation Saturn
Email: allzin@yandex.ru
Россия, ul. Lenina 163, Rybinsk, 152903
A. Shevyakov
Moscow Aviation Institute
Email: allzin@yandex.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
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