Chapter 30. Effects of Mullite/ Ysz Coatings on the Performance of Sic/ Sic Composite Combustion Liners

  1. Todd Jessen,
  2. Ersan Ustundag
  1. L. C. Russell1,
  2. J. Sankar1,
  3. R. A. Miller2,
  4. D. Zhu2,
  5. A. Calomino2

Published Online: 28 MAR 2008

DOI: 10.1002/9780470294635.ch30

24th Annual Conference on Composites, Advanced Ceramics, Materials, and Structures: B: Ceramic Engineering and Science Proceedings, Volume 21, Issue 4

24th Annual Conference on Composites, Advanced Ceramics, Materials, and Structures: B: Ceramic Engineering and Science Proceedings, Volume 21, Issue 4

How to Cite

Russell, L. C., Sankar, J., Miller, R. A., Zhu, D. and Calomino, A. (2008) Effects of Mullite/ Ysz Coatings on the Performance of Sic/ Sic Composite Combustion Liners, in 24th Annual Conference on Composites, Advanced Ceramics, Materials, and Structures: B: Ceramic Engineering and Science Proceedings, Volume 21, Issue 4 (eds T. Jessen and E. Ustundag), John Wiley & Sons, Inc., Hoboken, NJ, USA. doi: 10.1002/9780470294635.ch30

Author Information

  1. 1

    NSF- Center for Advanced Materials & Smart Structures North Carolina A&T State University Greensboro. NC 27411

  2. 2

    NASA Glenn Research Center Cleveland, OH 44135

Publication History

  1. Published Online: 28 MAR 2008
  2. Published Print: 1 JAN 2000

ISBN Information

Print ISBN: 9780470375693

Online ISBN: 9780470294635

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Keywords:

  • thermal barrier;
  • hygrothermal soaking;
  • coating system;
  • coefficient of thermal expansion (CTE);
  • ceramic composites

Summary

Silicon carbide/ Silicon carbide (SiC/ SiC) woven composites were covered with plasma- sprayed mullite/ ZrO2- 8 wt % Y2O3 coatings. Isothermal soaking in an oxidative environment was used to simulate a combustion environment to determine the feasibility of the corrosive/ thermal barrier coating system and its effects on the flexural behavior of SiC/ SiC 5-harness satin weave composites. The experimental investigation consists of studying the load- displacement behavior of virgin to thermally soaked to coated materials, and understanding the failure mechanisms of SiC/ SiC composites during four- point bend testing. The specimens experienced both high temperature gradients and hygrothermal soaking. The load- displacement data from the laser four- point flexural test demonstrates that the coating ratio 1.5:1 combination outperforms the 0.6:l coating ratio in the mechanical behavior of the composite specimens. The scanning electron microscope micrographs demonstrate that hygrothermal soaking degrades the material, causing a reduction in mechanical strength.