Thermomechanical simulations of the transient coupled effect of thermal cycling and oxidation on residual stresses in thermal barrier coatings

被引:15
作者
Lim, L. Y. [1 ]
Meguid, S. A. [1 ]
机构
[1] Univ Toronto, Mech & Aerosp Design Lab, 5 Kings Coll Rd, Toronto, ON M5S 3G8, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Thermal barrier coating; Residual stresses; Thermal cycling; Transient coupled; FINITE-ELEMENT SIMULATION; GROWN OXIDE THICKNESS; FAILURE-MECHANISM; PHOTOLUMINESCENCE PIEZOSPECTROSCOPY; TBC SYSTEM; DEFORMATION; INSTABILITY; ROUGHNESS; LIFETIME; BONDCOAT;
D O I
10.1016/j.ceramint.2021.10.087
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Failures in thermal barrier coatings (TBCs) are associated with the build-up of residual stresses that result from thermal cycling, growth strain, and stress relaxation associated with high temperatures. To address these highly coupled processes, three aspects were examined. The first was concerned with the effect of thermal cycling and thermal gradients on the resulting residual stress fields. The second with the dynamic growth of thermally grown oxide (TGO) layer using novel finite volume-finite element algorithms. In the third, we examined the effect of stress relaxation on the (TC/TGO) interface. We modelled these highly coupled processes using transient thermomechanical finite element simulations. The temperature profile and state of oxidation variation with time were imported as a predefined field and solved in ANSYS nonlinear platform. Our results revealed that stress relaxation of the TGO stresses at high temperatures leads to a reduction in the TC/TGO interfacial stresses. They also revealed that the use of the isotropic hardening rule limits the increase in plastic deformation of the bond coat (BC), while the use of kinematic hardening rule leads to ratcheting. Furthermore, we highlighted the importance of considering uneven growth of TGO on the resulting stress field.
引用
收藏
页码:3133 / 3147
页数:15
相关论文
共 52 条
[1]  
Baker M., PARAMETRIC STUDY STR, DOI [10.1016/j.actamat.2004.10.004, DOI 10.1016/J.ACTAMAT.2004.10.004]
[2]  
Bedworth R.E., 1923, J I MET
[3]   Finite element analysis of stress distribution in thermal barrier coatings [J].
Bialas, Marcin .
SURFACE & COATINGS TECHNOLOGY, 2008, 202 (24) :6002-6010
[4]   Modeling of interface failure in a thermal barrier coating system on Ni-based superalloys [J].
Burov, Andrey ;
Fedorova, Elena .
ENGINEERING FAILURE ANALYSIS, 2021, 123
[5]   The influence of bondcoat and topcoat mechanical properties on stress development in thermal barrier coating systems [J].
Busso, E. P. ;
Qian, Z. Q. ;
Taylor, M. P. ;
Evans, H. E. .
ACTA MATERIALIA, 2009, 57 (08) :2349-2361
[6]   Influence of inhomogeneous thermally grown oxide thickness on residual stress distribution in thermal barrier coating system [J].
Chen, Zhi ;
Huang, Hongmei ;
Zhao, Kai ;
Jia, Wenbin ;
Fang, Lei .
CERAMICS INTERNATIONAL, 2018, 44 (14) :16937-16946
[7]   Modeling oxidation induced stresses in thermal barrier coatings [J].
Freborg, AM ;
Ferguson, BL ;
Brindley, WJ ;
Petrus, GJ .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1998, 245 (02) :182-190
[8]   High-Temperature Mechanical Behavior of End-of-Life Cryomilled NiCrAlY Bond Coat Materials [J].
Funk, M. ;
Ma, K. ;
Eberl, C. ;
Schoenung, J. M. ;
Goeken, M. ;
Hemker, K. J. .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2011, 42A (08) :2233-2241
[9]   Influence of Topcoat-Bondcoat Interface Roughness on Stresses and Lifetime in Thermal Barrier Coatings [J].
Gupta, M. ;
Skogsberg, K. ;
Nylen, P. .
JOURNAL OF THERMAL SPRAY TECHNOLOGY, 2014, 23 (1-2) :170-181
[10]   Simulation of stresses and delamination in a plasma-sprayed thermal barrier system upon thermal cycling [J].
He, MY ;
Hutchinson, JW ;
Evans, AG .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2003, 345 (1-2) :172-178