期刊文献+

Numerical simulation of TBCs residual stresses by the growth of TGO on typical interface morphology

Numerical simulation of TBCs residual stresses by the growth of TGO on typical interface morphology
下载PDF
导出
摘要 The effect of TGO ( thermally grown oxide ) growth based on typical interface morphology on residual stresses distribution in thermal barrier coatings was analyzed by ABAQUS software. TGO oxidation kinetics, the relationship between TGO thickness and thermal cycles number, and typical morphology including sinusoid , cone and groove were considered in the calculation process. 13 FEM (finite element method) models with different TGO thickness based on uniform interface morphology were established for analysis. The calculation results show that TCC ( top ceramic coating ) /TGO and TGO/BC (bond coating) interface residual stresses are affected significantly by inter)hce morphology and TGO thickness, both of which increase significantly with TGO growth ; the stress level in TCC/TGO interface is greater than that of TGO/BC interface ; each morphology peak exhibits tensile stress while each valley exhibits compressive stress in TCC/TGO interface; stress concentrates in such locations as each morphology center with sharp angle and the stress reaches the maximal value at the tip of each angle. The effect of TGO ( thermally grown oxide ) growth based on typical interface morphology on residual stresses distribution in thermal barrier coatings was analyzed by ABAQUS software. TGO oxidation kinetics, the relationship between TGO thickness and thermal cycles number, and typical morphology including sinusoid , cone and groove were considered in the calculation process. 13 FEM (finite element method) models with different TGO thickness based on uniform interface morphology were established for analysis. The calculation results show that TCC ( top ceramic coating ) /TGO and TGO/BC (bond coating) interface residual stresses are affected significantly by inter)hce morphology and TGO thickness, both of which increase significantly with TGO growth ; the stress level in TCC/TGO interface is greater than that of TGO/BC interface ; each morphology peak exhibits tensile stress while each valley exhibits compressive stress in TCC/TGO interface; stress concentrates in such locations as each morphology center with sharp angle and the stress reaches the maximal value at the tip of each angle.
出处 《China Welding》 EI CAS 2012年第2期64-68,共5页 中国焊接(英文版)
基金 This work was supported by National Natural Science Foundation of China (No. 60879018).
关键词 thermal barrier coatings FEM residual stress interface morphology TGO growth thermal barrier coatings, FEM, residual stress, interface morphology, TGO growth
  • 相关文献

参考文献14

  • 1Ma W, Jarligo M O, Mack D E, et ah New generation perovskite thermal barrier coating materials. Journal of Thermal Spray Technology, 2008, 17 (5 - 6) : 831 - 837.
  • 2Che C, Wu G Q, Qi H Y, et al. Uneven growth of thermally grown oxide and stress distribution in plasma-sprayed thermal barrier coatings. Surface and Coatings Technology, 2009, 203 : 3088 - 3091.
  • 3Karlsson A M, Xu T, Evans A G. The effect of the thermal barrier coating on the displacement instability in thermal barrier systems. Acta Materialia, 2002, 50(5) : 1211 -1218.
  • 4Vaben R, Giesen S, Stover D. Lifetime of plasma-sprayed thermal barrier coatings : comparison of numerical and experimental results. Journal of Thermal Spray Technology, 2009, 18(5 -6) : 835 -845.
  • 5Davis A W, Evans A G. Some effects of imperfection geometry on the cyclic distortion of thermally grown oxides. Oxidation of Metals, 2006, 65 ( 1 - 2) : 1 - 14.
  • 6Chang G C, Pucharoen W, Miller R A. Finite element thermal stress solutions for thermal barrier coatings. Surface and Coatings Technology, 1987, 30( 1 -4) : 307 -325.
  • 7Chen W R, Archer, Huang X, et al. TGO growth and crack propagation in a thermal barrier coating. Journal of Thermal Spray Technology, 2008, 17 (5 - 6) : 858 - 864.
  • 8Trunova O, Beck T, Herzog R, et al. Damage mechanism sand life time behavior of plasma sprayed thermal barrier coating systems for gas turbines. Surface and Coatings Technology, 2008, 202(20): 5027-5032.
  • 9Nissley D M. Thermal barrier coating life modeling in aircraft gas turbine engines. Journal of Thermal Spray Technology, 1997, 6(1) : 91 -98.
  • 10Ni L Y, Liu C, Huang H, et al. Thermal cycles behavior of thermal barrier coatings with HVOF NiCrA1Y bond coat. Journal of Thermal Spray Technology, 2011, 20(5 ) : 1133 - 1138.

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