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Review | Open Access

Tribological behaviour of C/C–SiC composites—A review

Department of Mechanical Engineering, Indian Institute of Technology (BHU), Varanasi-221005, India
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Abstract

Ceramic matrix composites made of carbon fibres and carbon matrix (C/C) are generally used for aircraft structures and brake discs due to their low density, and good thermal, mechanical, and tribological properties. Silicon carbide (SiC) can be introduced to the matrix to improve the performance of C/C composites, because it increases the hardness and thermal stability, and decreases the chemical reactivity, which leads to the improvement of tribological properties of C/C composites. Thus carbon–carbon silicon carbide (C/C–SiC) composites can be used at high temperature for the application of brake discs, friction clutches, etc. C/C–SiC composites are fabricated by three different methods: (i) chemical vapour infiltration (CVI), (ii) polymer infiltration and pyrolysis (PIP), and (iii) liquid silicon infiltration (LSI), among which LSI method is widely used for the fabrication of C/C–SiC composites due to higher mechanical and thermal properties.

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Journal of Advanced Ceramics
Pages 1-12
Cite this article:
KUMAR P. Tribological behaviour of C/C–SiC composites—A review. Journal of Advanced Ceramics, 2016, 5(1): 1-12. https://doi.org/10.1007/s40145-015-0171-z

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Received: 11 August 2015
Revised: 16 September 2015
Accepted: 24 September 2015
Published: 07 January 2016
© The author(s) 2016

Open Access The articles published in this journal are distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/ by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.

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