High-temperature composites with a multi-layered structure (review)

Sorokin O.Ju., Kuznetsov B.Yu., Lunegova Yu.V., Erasov V.S.
UDC
66.017
DOI
10.18577/2307-6046-2020-0-45-42-53
Article PDF (Russian) (853.12 KB)
How to cite
Sorokin O.Ju., Kuznetsov B.Yu., Lunegova Yu.V., Erasov V.S. High-temperature composites with a multi-layered structure (review) // Proceedings of VIAM. 2020. No. 4-5. DOI: 10.18577/2307-6046-2020-0-45-42-53. URL: https://test.viam.ru/en/journal/2020/4-5/5
Keywords
ceramic, composite materials, multi-layered structure, toughness, graceful fracture mode, strength, oxidation.
Abstract

Properties, processing techniques and possible applications in «hot sections» of gas turbine engine of different structural high-temperature materials with an operating temperature higher than 1200 °С are highlighted. Composites with a multi-layered structure based on «ceramic/carbon», «ceramic/ceramic», «ceramic/metal» systems have demonstrated to be promising materials. Layer widths with low/high Young modules, their ratio and arrangement have a significant impact on the strength parameters. High-temperature composites with a multi-layered structure can have a «graceful failure» mode and higher toughness as compared to particle reinforced ceramic composites.

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