期刊文献+

Effect of Sintering on Thermal Conductivity and Thermal Barrier Effects of Thermal Barrier Coatings 被引量:9

Effect of Sintering on Thermal Conductivity and Thermal Barrier Effects of Thermal Barrier Coatings
原文传递
导出
摘要 Thermal barrier coatings (TBCs) are mostly applied to hot components of advanced turbine engines to insulate the compo- nents from hot gas. The effect of sintering on thermal conductivity and thermal barrier effects of conventional plasma sprayed and nanostructured yttria stabilized zirconia (YSZ) thermal barrier coatings (TBCs) are investigated. Remarkable increase in thermal conductivity occurs to both typical coatings after heat treatment, The change of porosity is just the opposite. The grain size of the nanostructured zirconia coating increases more drastically with annealing time compared to that of the conventional plasma sprayed coating, which indicates that coating sintering makes more contributions to the thermal conductivity of the nanostructured coating than that of the conventional coating. Thermal barrier effect tests using temperature difference technique are performed on both coatings. The thermal barrier effects decrease with the increase of thermal conductivity after heat treat- ment and the decline seems more drastic in low thermal conductivity range. The decline in thermal barrier effects is about 80℃ for nanostructured coating after 100 h heat treatment, while the conventional coating reduces by less than 60 ℃ compared to the as-sprayed coating. Thermal barrier coatings (TBCs) are mostly applied to hot components of advanced turbine engines to insulate the compo- nents from hot gas. The effect of sintering on thermal conductivity and thermal barrier effects of conventional plasma sprayed and nanostructured yttria stabilized zirconia (YSZ) thermal barrier coatings (TBCs) are investigated. Remarkable increase in thermal conductivity occurs to both typical coatings after heat treatment, The change of porosity is just the opposite. The grain size of the nanostructured zirconia coating increases more drastically with annealing time compared to that of the conventional plasma sprayed coating, which indicates that coating sintering makes more contributions to the thermal conductivity of the nanostructured coating than that of the conventional coating. Thermal barrier effect tests using temperature difference technique are performed on both coatings. The thermal barrier effects decrease with the increase of thermal conductivity after heat treat- ment and the decline seems more drastic in low thermal conductivity range. The decline in thermal barrier effects is about 80℃ for nanostructured coating after 100 h heat treatment, while the conventional coating reduces by less than 60 ℃ compared to the as-sprayed coating.
出处 《Chinese Journal of Aeronautics》 SCIE EI CSCD 2012年第5期811-816,共6页 中国航空学报(英文版)
基金 National Natural Science Foundation of China (50771009, 50731001, 51071013)
关键词 thermal barrier coatings (TBCs) SINTERING thermal conductivity thermal insulation laser flash method thermal barrier coatings (TBCs) sintering thermal conductivity thermal insulation laser flash method
  • 相关文献

参考文献1

二级参考文献2

  • 1杨世铭.传热学基础[M].北京:高等教育出版社,1987.38.
  • 2陈洪荪.金属材料物理性能手册:第一册(金属物理性能及测试方法)[M].北京:冶金工业出版社,1987.109.

共引文献41

同被引文献46

引证文献9

二级引证文献33

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