期刊文献+

热障涂层中热生长氧化层应力及变形研究进展 被引量:2

Progress in Research on Stress and Distortion of Thermally Grown Oxides in TBCs
下载PDF
导出
摘要 从影响热生长氧化层(TGO)变形的因素、计算模型和计算方法方面综述国内外学者近年来在热生长氧化层变形和应力方面的研究成果。详细评述热膨胀失配、蠕变、TGO生长、黏结层相变和界面形貌等因素对TGO变形和应力的影响,并介绍目前研究TGO变形和应力的主要方法和计算模型。提出:基于内聚力模型(CZM)的扩展有限元方法(X-FEM)、(扩展)Voronoi有限元模型可以解决基于传统有限元方法和断裂力学方法在研究TGO裂纹扩展问题、获取TGO临界断裂参数等方面存在的困难,是一种有前途的研究TGO变形、应力及裂纹问题的方法。 Progress in research on the stress and distortion of thermally grown oxides(TGO) was reviewed.The factors affecting the stress and distortion of TGO such as thermal expansion mismatch,creep of bond coat and TGO,growth of TGO,phase transformations of bond coat,interfacial morphology were evaluated.The research method and calculation model including analytical models and finite element models were introduced.In traditional FEM model,the fracture criterion of the TGO is hard to measure,and can't deal with the problem of interaction and growth of multiple cracks.The extended finite element method (X-FEM) coupled with cohesive zone model (CZM) and the Voronoi element model overcomes these shortfalls and shows advantage in simulation of crack problems in TGO without needing of re-meshing and some critical crack parameters which remain experimentally elusive.It will be an effective method in TGO stress,distortion and crack problem.
作者 陈勇
机构地区 上海交通大学
出处 《航空材料学报》 EI CAS CSCD 北大核心 2013年第6期86-95,共10页 Journal of Aeronautical Materials
基金 航空科学基金(20122157007)
关键词 热生长氧化层 应力分析 有限元 扩展有限元 内聚力模型 thermally grown oxides stress analysis finite element method extended finite element method cohesive zone model
  • 相关文献

参考文献105

  • 1郑蕾,郭洪波,郭磊,彭徽,宫声凯,徐惠彬.新一代超高温热障涂层研究[J].航空材料学报,2012,32(6):14-24. 被引量:64
  • 2梁春华,李晓欣.先进材料在战斗机发动机上的应用与研究趋势[J].航空材料学报,2012,32(6):32-36. 被引量:43
  • 3蔡妍,易军,陆峰,陶春虎.热障涂层金属元素扩散阻挡层研究进展[J].材料工程,2011,39(9):92-96. 被引量:6
  • 4SHEFFLER K D. Current status and future trends in tur?bine application of thermal barrier[J]. ASMEJournal of Engine for Gas Turbine and Power, 1988,110 -605.
  • 5梁波,陈煌.氧化锆涂层(薄膜)的应用与研究[J].硅酸盐通报,2003,22(6):63-67. 被引量:34
  • 6EVANS A G, MUMM D R, HUTCHINSONJ W, et at. Mechanisms controlling the durability of thermal barrier coatings[J]. Progr Mater Sci, 2001,46(5): 505 -553.
  • 7MILLER R A. Current status of thermal barrier coatings: an overview[J]. Surf Coat Tech, 1987, 30 ( I ) : I - 11.
  • 8M UMM DR, EVANS A G. Mechanisms controlling the performance and durability of thermal barrier coatings[J]. Key Eng Mat, 2001, 197 - 199.
  • 9ZHU D M, MILLER R A. Thermal and Environmental Bar?rier Coatings for Advanced Turbine Engine Applications[R]. NASA/TM 2005-213437, Boston, United Stated: NASA,2005.
  • 10PADTURE N P, GELL M,JORDAN E H. Thermal barrier coatings for gas-turbine engine applications[J]. Science, 2002, 296 (5566) : 280.

二级参考文献127

共引文献140

同被引文献12

引证文献2

二级引证文献29

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部