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热、力耦合作用下热障涂层的失效机制

徐惠彬 宫声凯 陈立强 张春霞

徐惠彬, 宫声凯, 陈立强, 等 . 热、力耦合作用下热障涂层的失效机制[J]. 北京航空航天大学学报, 2004, 30(10): 919-924.
引用本文: 徐惠彬, 宫声凯, 陈立强, 等 . 热、力耦合作用下热障涂层的失效机制[J]. 北京航空航天大学学报, 2004, 30(10): 919-924.
Xu Huibin, Gong Shengkai, Chen Liqiang, et al. Failure process of thermal barrier coatings under thermal and mechanical loading[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(10): 919-924. (in Chinese)
Citation: Xu Huibin, Gong Shengkai, Chen Liqiang, et al. Failure process of thermal barrier coatings under thermal and mechanical loading[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(10): 919-924. (in Chinese)

热、力耦合作用下热障涂层的失效机制

基金项目: 国家自然科学基金资助项目(50171003); 航空科学基金资助项目(03H51025)
详细信息
    作者简介:

    徐惠彬(1959-),男,吉林大安人,教授, xuhb@buaa.edu.cn.

  • 中图分类号: TG 174444

Failure process of thermal barrier coatings under thermal and mechanical loading

  • 摘要: 针对热障涂层服役环境中热物理化学环境与机械载荷耦合作用的特点,采用交流阻抗谱法与声发射法对热障涂层在恒定外载荷(高温蠕变)以及交变载荷(高温低周疲劳)作用下的失效过程进行了考察分析,研究发现,交流阻抗谱中低频段阻抗值的变化可以有效地反映热障涂层热氧化层内横向裂纹的萌生及扩展;有无外机械载荷作用下热障涂层的热循环失效的模式截然不同,在高温蠕变条件下,热障涂层的裂纹并不产生在热氧化层内,而是产生在热氧化层与柱状晶之间的等轴晶区;而在高温低周疲劳条件下裂纹是在粘结层与高温合金基体的扩散层处.

     

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出版历程
  • 收稿日期:  2004-04-28
  • 网络出版日期:  2004-10-31

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