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陶瓷基复合材料在航空发动机热端部件上的应用 被引量:21

Application of CMC on Thermal Parts of Aeroengine
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摘要 介绍了适应未来先进航空发动机需求的陶瓷基复合材料在国外航空发动机热端部件上的应用现状,并展望了陶瓷基复合材料在国内航空发动机热端部件上的应用前景。 The applications of CMC which can meet the requirements of high performance aeroengines is introduced and the possible utilization of this material in developing domestic engines is presented.
出处 《航空制造技术》 2009年第S1期4-7,共4页 Aeronautical Manufacturing Technology
关键词 陶瓷基复合材料 航空发动机 涡轮叶片 燃烧室 Ceramic matrix composites Aeroengine Turbine blade Combustion chamber
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参考文献4

  • 1Zhu Dongming,,Miller R A.Hafnia-based materials development for advanced thermal/environmental barrier coating applications. NASA/TM-2004-212729 .
  • 2Morscher G N.Modeling the stress strain behavior of woven ceramic matrix composites[].th Annual American Ceramic Society Conference.
  • 3Zhu Dongming,Miller R A,Fox D S.Thermal and environmental barrier coating development for advanced propulsion engine systems. NASA/TM—2008-215040 .
  • 4Zhu,D.,Bansal,N.P.,Miller,R.A.Thermal Conductivity and Stability of Hafnia and Zirconate-Based Materials for 1650°C Thermal/Environmental Barrier Coating Applications[].Ceram Trans.2003

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