Chapter 86. Mechanical Properties of Si-Zr-C-O/SiC Composite Material for Advanced Heat Resistance Combustor Liner

  1. Waltraud M. Kriven and
  2. Hua-Tay Lin
  1. Kenichiroh Igashira1,
  2. Yoshihiro Matsuda2 and
  3. Go Matsubara3

Published Online: 26 MAR 2008

DOI: 10.1002/9780470294826.ch86

27th Annual Cocoa Beach Conference on Advanced Ceramics and Composites: B: Ceramic Engineering and Science Proceedings, Volume 24, Issue 4

27th Annual Cocoa Beach Conference on Advanced Ceramics and Composites: B: Ceramic Engineering and Science Proceedings, Volume 24, Issue 4

How to Cite

Igashira, K., Matsuda, Y. and Matsubara, G. (2003) Mechanical Properties of Si-Zr-C-O/SiC Composite Material for Advanced Heat Resistance Combustor Liner, in 27th Annual Cocoa Beach Conference on Advanced Ceramics and Composites: B: Ceramic Engineering and Science Proceedings, Volume 24, Issue 4 (eds W. M. Kriven and H.-T. Lin), John Wiley & Sons, Inc., Hoboken, NJ, USA. doi: 10.1002/9780470294826.ch86

Author Information

  1. 1

    Kawasaki Heavy Industries, Ltd 1-1 Kawasaki-cho Akashi, 673-8666 Japan

  2. 2

    Kawasaki Heavy Industries, Ltd. 1-1 Kawasaki-cho Akashi, 673-8666 Japan

  3. 3

    Kawasaki Heavy Industries, Ltd 1-1 Kawasaki-cho Akashi, 673-8666 Japan

Publication History

  1. Published Online: 26 MAR 2008
  2. Published Print: 1 JAN 2003

ISBN Information

Print ISBN: 9780470375846

Online ISBN: 9780470294826

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Keywords:

  • generation supersonic transport;
  • combustor liner;
  • fuel-air mixture;
  • mounting system;
  • cobalt-based superalloys

Summary

In the “Research and Development of Environmentally Compatible Propulsion System for Next-Generation Supersonic Transport (ESPR)” project, R&D of the Ceramic Matrix Composite (CMC) is a key item for NOx reduction.

In this R&D, actual CMC combustor liners with the maximum diameter of 870 mm are being fabricated for combustion tests. The Si-Zr-C-O/SiC test sample, which imitated the structure of the actual CMC combustor liner was fabricated by the applicable manufacture technique for the large parts, and was evaluated its applicability for the combustor liner.