Wear and Erosion Resistance of Aircraft Engine Composite Elements in a Gas Abrasive Flow
- Авторлар: Zinin A.1, Dobrovol’skii S.1, Lebedev A.1, Krupennikov V.2, Shevyakov A.1
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Мекемелер:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- Шығарылым: Том 62, № 4 (2019)
- Беттер: 696-703
- Бөлім: Aircraft Production Technology
- URL: https://journals.rcsi.science/1068-7998/article/view/231197
- DOI: https://doi.org/10.3103/S1068799819040226
- ID: 231197
Дәйексөз келтіру
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.
Негізгі сөздер
Авторлар туралы
A. Zinin
Moscow Aviation Institute
Хат алмасуға жауапты Автор.
Email: allzin@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
S. Dobrovol’skii
Moscow Aviation Institute
Email: allzin@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
A. Lebedev
Moscow Aviation Institute
Email: allzin@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
V. Krupennikov
PAO United Engine Corporation Saturn
Email: allzin@yandex.ru
Ресей, ul. Lenina 163, Rybinsk, 152903
A. Shevyakov
Moscow Aviation Institute
Email: allzin@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993