氧化锆基陶瓷热障涂层的研究进展
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  • 英文篇名:Progress on Zirconia-based Ceramics for Thermal Barrier Coatings
  • 作者:张巍
  • 英文作者:Zhang Wei;Quality Control Department,Plibrico(Dalian)Industries Co.,Ltd.;
  • 关键词:二氧化锆 ; 热障涂层 ; 掺杂 ; 热导率 ; 热膨胀系数
  • 英文关键词:zirconia;;thermal barrier coatings;;doping;;thermal conductivity;;coefficient of thermal expansion
  • 中文刊名:HKGC
  • 英文刊名:Advances in Aeronautical Science and Engineering
  • 机构:派力固(大连)工业有限公司质控课;
  • 出版日期:2018-11-28
  • 出版单位:航空工程进展
  • 年:2018
  • 期:v.9;No.36
  • 语种:中文;
  • 页:HKGC201804004
  • 页数:19
  • CN:04
  • ISSN:61-1479/V
  • 分类号:18-36
摘要
氧化锆基陶瓷热障涂层是航空发动机的关键技术。根据一元氧化物、二元氧化物和多元氧化物掺杂稳定二氧化锆(ZrO_2)热障涂层的相关研究报道,系统地总结了氧化锆基陶瓷热障涂层在相稳定性、服役温度、热循环寿命、热导率、热膨胀系数等方面取得的进展;在此基础上,指出了氧化锆基陶瓷热障涂层的未来研究与发展方向。
        Zirconia-based ceramics for thermal barrier coatings is a key technology of aircraft engine.According to the investigation report of stable zirconia-based ceramics for thermal barrier coatings doped with one component oxide,two component oxides and multi component oxides,the progress on zirconia-based ceramics for thermal barrier coatings in phase stability,service temperature,thermal cycle life,thermal conductivity and coefficient of thermal expansion is systematically summarized.On this basis,the future research and development trend of zirconia-based ceramics for thermal barrier coatings are prospected.
引文
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