Chapter 47. Fabrication and Mechanical Properties of Reaction Sintered Silicon Carbide Matrix Composite

  1. J. P. Singh
  1. T. Kameda1,
  2. A. Sayano1,
  3. N. Amiji1,
  4. H. Ichikawa2,
  5. H. Hamada3,
  6. A. Fujita3 and
  7. T. Uozumi4

Published Online: 26 MAR 2008

DOI: 10.1002/9780470294437.ch47

Proceedings of the 21st Annual Conference on Composites, Advanced Ceramics, Materials, and Structures: A: Ceramic Engineering and Science Proceedings, Volume 18, Issue 3

Proceedings of the 21st Annual Conference on Composites, Advanced Ceramics, Materials, and Structures: A: Ceramic Engineering and Science Proceedings, Volume 18, Issue 3

How to Cite

Kameda, T., Sayano, A., Amiji, N., Ichikawa, H., Hamada, H., Fujita, A. and Uozumi, T. (1997) Fabrication and Mechanical Properties of Reaction Sintered Silicon Carbide Matrix Composite, in Proceedings of the 21st Annual Conference on Composites, Advanced Ceramics, Materials, and Structures: A: Ceramic Engineering and Science Proceedings, Volume 18, Issue 3 (ed J. P. Singh), John Wiley & Sons, Inc., Hoboken, NJ, USA. doi: 10.1002/9780470294437.ch47

Author Information

  1. 1

    Materials & Devices Development Center, Toshiba Corp., Yokohama 230, Japan

  2. 2

    Research & Development Dept., Nippon Carbon Co., Ltd., Yokohama 221, Japan

  3. 3

    Faculty of Textile Science, Kyoto Institute of Technology, Kyoto 606, Japan

  4. 4

    Braider Section, Murata Machinery, Ltd., Kyoto 612, Japan

Publication History

  1. Published Online: 26 MAR 2008
  2. Published Print: 1 JAN 1997

ISBN Information

Print ISBN: 9780470375495

Online ISBN: 9780470294437

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Keywords:

  • silicon carbide;
  • gas turbine combustor;
  • fiber reinforced ceramic;
  • interfacial layer;
  • porous mold

Summary

Dense silicon carbide (SiC) matrix composite reinforced by Hi-Nicalon braided fabric with boron nitride (BN) interfacial layer was fabricated by slurry impregnation of the fabric and a subsequent reaction sintering process. Some mechanical properties at room temperature and 1300°C were evaluated and discussed. Considering the application as gas turbine combustor parts, braiding technique was also developed and the continuous fiber reinforced ceramic composite (CFCC) combustor part was manufactured as prototype.