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热障涂层的冲蚀破坏机理研究进展

杨丽,  周益春,  齐莎莎

文章导航 > 力学进展  > 2012 >  42(6): 704-721
杨丽, 周益春, 齐莎莎. 热障涂层的冲蚀破坏机理研究进展[J]. 力学进展, 2012, 42(6): 704-721. doi: 10.6052/1000-0992-12-003
引用本文: 杨丽, 周益春, 齐莎莎. 热障涂层的冲蚀破坏机理研究进展[J]. 力学进展, 2012, 42(6): 704-721. doi: 10.6052/1000-0992-12-003
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YANG Li, ZHOU Yichun, QI Shasha. RESEARCH PROGRESS IN EROSION MECHANISMS OF THERMAL BARRIER COATINGS[J]. Advances in Mechanics, 2012, 42(6): 704-721. doi: 10.6052/1000-0992-12-003
Citation: YANG Li, ZHOU Yichun, QI Shasha. RESEARCH PROGRESS IN EROSION MECHANISMS OF THERMAL BARRIER COATINGS[J]. Advances in Mechanics, 2012, 42(6): 704-721. doi: 10.6052/1000-0992-12-003
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热障涂层的冲蚀破坏机理研究进展

doi: 10.6052/1000-0992-12-003

  • 湘潭大学低维材料及其应用技术教育部重点实验室, 湘潭大学材料与光电物理学院, 湘潭 411105

基金项目: 国家自然科学基金(11272275, 51172192, 11002122), 湖南省自然科学创新研究群体(09JJ7004), 湖南省自然科学基金(11JJ4003), 湖南省科研条件创新专项一般项目(2012TT2040) 资助
详细信息
    作者简介:

    周益春, 男, 1963 年出生, 1985 年、1988 年和1994 年分别在湘潭大学、国防科技大学和中国科学 院力学研究所获得学士、硕士和博士学位, 1998 年12 月{2001 年9 月在日本东北大学做访问教授. 1996 年评为教授, 1998 年在中国科学院力学研究所被评为博士导师. 2002 年教育部" 跨世纪优秀人 才"、2005 年国家杰出青年科学基金、2006 年第二届国家级教学名师、2009 年国际功能材料科学家 奖. 主要从事" 几种特殊的涂层和薄膜的制备, 物理和力学性能分析" 的研究, 获得省部级自然科学奖 一等奖、科技进步一等奖和二等奖各1 项, 国家发明专利15 项. 在Appl. Phys. Lett., Acta Mater等 国际著名刊物发表学术论文150 余篇, 其中SCI 收录的论文130 余篇, 被他人在Science、Nature等 引用700 余次, 30 余次在国际国内学术会议作邀请报告.

    通讯作者:

    杨丽

    周益春

RESEARCH PROGRESS IN EROSION MECHANISMS OF THERMAL BARRIER COATINGS

  • Key Laboratory of Low Dimensional Materials and Application Technology of Ministry of Education, Faculty of Materials, Optoelectronics and Physics, Xiangtan University, Xiangtan 411105, China

Funds: The project was supported by the National Natural Science Foundation of China (11272275, 51172192, 11002122), the Natural Science Foundation of Hunan Province for Innovation Group (09JJ7004),and the Natural Science Foundation of Hunan Province (11JJ4003), andthe Key Project of Scientific Research Conditions in Hunan Province (2012TT2040).
More Information
    Corresponding author: YANG Li; ZHOU Yichun

    摘要
  • 摘要: 耐高温、高隔热的热障涂层(thermal barrier coatings, TBCs) 技术因为能降低基底的工作温度, 提高 发动机的性能与热效率, 已经成为了航空发动机的关键热防护技术. 航空发动机在飞行过程中, 将不可避免地 受到燃烧室内各种杂质及外来颗粒的撞击, 从而发生冲蚀失效, 这一失效已成为制约TBCs 服役性能及其安 全应用的关键问题. 本文介绍了TBCs 冲蚀破坏机理的实验研究、有限元模拟、理论分析、试验模拟系统以及 实验检测技术方面的最新成果, 展望了TBCs 冲蚀机理研究的重点.

     

    Abstract: Thermal barrier coatings (TBCs) with high temperature durability and excellent heat insulation can reduce the metal surface temperature, which results in a significant improvement in performance and high efficiency of gas turbine engines. TBCs have been developed as a key heat protection technique. During flight, TBCs are unavoidably impacted and then eroded by particles from combustion chambers or foreign objects. Erosion of TBCs has become a severe problem in service life and reliability. In this paper, recent developments have been reviewed, including the experimental results, numerical simulations, theoretical analyses, experimental simulations and relevant measurement methods. Finally, development trend in TBCs erosion research is discussed.

     

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  • 收稿日期:  2012-01-16
  • 修回日期:  2012-05-16
  • 刊出日期:  2012-11-25

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