Wear and Erosion Resistance of Aircraft Engine Composite Elements in a Gas Abrasive Flow
- Autores: Zinin A.1, Dobrovol’skii S.1, Lebedev A.1, Krupennikov V.2, Shevyakov A.1
-
Afiliações:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- Edição: Volume 62, Nº 4 (2019)
- Páginas: 696-703
- Seção: Aircraft Production Technology
- URL: https://journals.rcsi.science/1068-7998/article/view/231197
- DOI: https://doi.org/10.3103/S1068799819040226
- ID: 231197
Citar
Resumo
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.
Palavras-chave
Sobre autores
A. Zinin
Moscow Aviation Institute
Autor responsável pela correspondência
Email: allzin@yandex.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
S. Dobrovol’skii
Moscow Aviation Institute
Email: allzin@yandex.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
A. Lebedev
Moscow Aviation Institute
Email: allzin@yandex.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
V. Krupennikov
PAO United Engine Corporation Saturn
Email: allzin@yandex.ru
Rússia, ul. Lenina 163, Rybinsk, 152903
A. Shevyakov
Moscow Aviation Institute
Email: allzin@yandex.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993