Wear and Erosion Resistance of Aircraft Engine Composite Elements in a Gas Abrasive Flow
- 作者: Zinin A.1, Dobrovol’skii S.1, Lebedev A.1, Krupennikov V.2, Shevyakov A.1
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隶属关系:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- 期: 卷 62, 编号 4 (2019)
- 页面: 696-703
- 栏目: Aircraft Production Technology
- URL: https://journals.rcsi.science/1068-7998/article/view/231197
- DOI: https://doi.org/10.3103/S1068799819040226
- ID: 231197
如何引用文章
详细
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.
作者简介
A. Zinin
Moscow Aviation Institute
编辑信件的主要联系方式.
Email: allzin@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
S. Dobrovol’skii
Moscow Aviation Institute
Email: allzin@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
A. Lebedev
Moscow Aviation Institute
Email: allzin@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
V. Krupennikov
PAO United Engine Corporation Saturn
Email: allzin@yandex.ru
俄罗斯联邦, ul. Lenina 163, Rybinsk, 152903
A. Shevyakov
Moscow Aviation Institute
Email: allzin@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993