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High-Temperature Ceramic Composites (SiC/SiCw)

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The prospects for using ceramic composite materials in place of metallic materials in heat-loaded units in advanced aircraft are examined. The manufacture of silicon carbide based ceramic composite materials, reinforced with filamentary crystals (whiskers), by means of hot-pressing and spark plasma sintering using oxide and nitride sintering additives was investigated. A complex of physical-mechanical and thermal properties of composites was investigated.

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This work was performed as part of the implementation of the complex scientific direction 14.1: structural ceramic composite materials (‘Strategic directions of development of materials and their processing technologies in the period to 2030’) [25].

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Authors and Affiliations

  1. All-Russia Scientific-Research Institute of Aviation Materials (FSUE VIAM), Moscow, Russia

    N. E. Shchegoleva, S. A. Evdokimov, I. V. Osin, A. S. Chainikova & A. A. Shavnev

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  1. N. E. Shchegoleva
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  2. S. A. Evdokimov
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  3. I. V. Osin
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  4. A. S. Chainikova
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  5. A. A. Shavnev
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Correspondence to N. E. Shchegoleva.

Additional information

Translated from Steklo i Keramika, No. 2, pp. 13 – 17, February, 2020.

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Shchegoleva, N.E., Evdokimov, S.A., Osin, I.V. et al. High-Temperature Ceramic Composites (SiC/SiCw). Glass Ceram 77, 47–50 (2020). https://doi.org/10.1007/s10717-020-00235-2

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