Development of the Advanced Combustor Liner Composed of CMC/GMC Hybrid Composite Material

  1. Dr. W. Krenkel2,
  2. Prof. Dr. R. Naslain3,
  3. Prof. Dr. H. Schneider4
  1. Kenichiroh Igashira,
  2. Yoshihiro Matsuda,
  3. Go Matsubara,
  4. Akira Imamura

Published Online: 13 JAN 2006

DOI: 10.1002/3527605622.ch120

Book Title

High Temperature Ceramic Matrix Composites

High Temperature Ceramic Matrix Composites

Additional Information

How to Cite

Igashira, K., Matsuda, Y., Matsubara, G. and Imamura, A. (2006) Development of the Advanced Combustor Liner Composed of CMC/GMC Hybrid Composite Material, in High Temperature Ceramic Matrix Composites (eds W. Krenkel, R. Naslain and H. Schneider), Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim, FRG. doi: 10.1002/3527605622.ch120

Editor Information

  1. 2

    Deutsches Zentrum für Luft- und Raumfahrt e.V., Institut für Bauweisen- und Konstruktionsforschung, Pfaffenwaldring 38–40, 70569 Stuttgart, Germany

  2. 3

    Université de Bordeaux, Laboratoire des Composites Thermostructuraux, 3, Allée de la Boétie, 33600 Pessac, France

  3. 4

    Deutsches Zentrum für Luft- und Raumfahrt e. V., Institut für Werkstoff-Forschung, Linder Höhe, 51147 Köln, Germany

Author Information

  1. Research Institute of Advanced Material Gas-Generator, Tokyo, Japan

Publication History

  1. Published Online: 13 JAN 2006
  2. Published Print: 12 OCT 2001

ISBN Information

Print ISBN: 9783527303205

Online ISBN: 9783527605620

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Keywords:

  • high temperature ceramic matrix composites;
  • advanced combustor liner;
  • development;
  • CMC/GMC hybrid composite material

Summary

In this paper, we describe the results of our evaluation for a CMC/GMC hybrid composite material as a combustor liner based on an evaluation of material properties, an analysis of thermal stress, and an evaluation of an actual CMC/GMC hybrid liner assembled in a combustor and subjected to a combustion test.

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