Oxide growth and damage evolution in thermal barrier coatings

被引:88
作者
Hille, T. S. [1 ,2 ]
Turteltaub, S. [1 ]
Suiker, A. S. J. [1 ]
机构
[1] Delft Univ Technol, Fac Aerosp Engn, NL-2600 GB Delft, Netherlands
[2] M2i, NL-2628 CD Delft, Netherlands
关键词
TBC systems; Multi-physics; Oxide growth; Partition-of-unity method; Cohesive law; FINITE-ELEMENT-METHOD; NICOCRALY BOND COATS; STABILIZED ZIRCONIA; MECHANICAL-PROPERTIES; INTERFACE ROUGHNESS; FAILURE MECHANISMS; CYCLIC OXIDATION; SYSTEMS; MODEL; DELAMINATION;
D O I
10.1016/j.engfracmech.2011.04.003
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Cracking in thermal barrier coatings (TBC) is triggered by the development of a thermally-grown oxide (TGO) layer that develops during thermal cycling from the oxidation of aluminum present in the bond coat (BC). In the present communication a numerical model is presented that describes the interactive development of the TGO morphology and the fracture processes in TBC systems in a mesh-independent way. The evolution of the TGO-BC mixture zone is described by an oxygen diffusion-reaction model. The partition-of-unity method is employed for the simulation of discrete cracking, where cracks can nucleate and propagate across finite elements at arbitrary locations and orientations. The validity of the model is demonstrated through the analysis of a representative TBC system subjected to a specific thermal cycling process. A parametric analysis demonstrates the sensitivity of the response of the TBC system to the fracture strength of the top coat. The simulation results indicate that cracks appear primarily at the current location of the BC-TGO interface and may nucleate at early stages of thermal cycling. These results are in good agreement with recent experimental observations reported in the literature. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2139 / 2152
页数:14
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