RETRACTED: Coating thickness and roughness effect on stress distribution of A356.0 under thermo-mechanical loadings (Retracted Article)

被引:18
作者
Moridi, A. [1 ]
Azadi, M. [1 ]
Farrahi, G. H. [1 ]
机构
[1] Sharif Univ Technol, Sch Mech Engn, Mat Life Estimat & Improvement Lab, Tehran 111558639, Iran
来源
11TH INTERNATIONAL CONFERENCE ON THE MECHANICAL BEHAVIOR OF MATERIALS (ICM11) | 2011年 / 10卷
关键词
Cast aluminium-silicon alloy; Thermal barrier coating; Thermo-mechanical loading; Fatigue; THERMAL BARRIER COATINGS; RESIDUAL-STRESSES; BEHAVIOR;
D O I
10.1016/j.proeng.2011.04.228
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Cast aluminium-silicon alloy, A356.0, is widely used in automotive components such as diesel engine cylinder heads and also in aerospace industries because of its outstanding mechanical, physical, and casting properties. Thermal barrier coatings are applied to combustion chamber in order to reduce fuel consumption and pollutions and also improve fatigue life of components. However, studies on behaviour of A356.0 with thermal barrier coating are still rare. The purpose of the present work is to simulate stress distribution of A356.0 under thermo-mechanical cyclic loadings, using a two-layer elastic-visco-plastic model of ABAQUS software. The results of stress-strain hysteresis loop are validated by an out of phase thermo-mechanical fatigue test. Then, ceramic coating thickness effect on stress distribution of test specimens is investigated. Different thicknesses from 300 to 800 microns of top coat and also roughness of the interfaces are simulated to get best stress gradient which can cause an improvement of fatigue life. Studying realistic interface roughness shows the critical area of tensile stress which results in crack initiation. Furthermore increasing TC thickness results in stress growth. (C) 2011 Published by Elsevier Ltd. Selection and peer-review under responsibility of ICM11
引用
收藏
页码:1372 / 1377
页数:6
相关论文
共 16 条
[1]  
[Anonymous], 1996, COAT HIGH TEMPR STRU, P30
[2]   Modelled and measured residual stresses in plasma sprayed thermal barrier coatings [J].
Bengtsson, P ;
Persson, C .
SURFACE & COATINGS TECHNOLOGY, 1997, 92 (1-2) :78-86
[3]   Finite element analysis of stress distribution in thermal barrier coatings [J].
Bialas, Marcin .
SURFACE & COATINGS TECHNOLOGY, 2008, 202 (24) :6002-6010
[4]   The effect of thermal barrier coatings on diesel engine performance [J].
Hejwowski, T ;
Weronski, A .
VACUUM, 2002, 65 (3-4) :427-432
[5]   Residual stresses in thermal barrier coatings: effects of interface asperity curvature/height and oxide thickness [J].
Hsueh, CH ;
Fuller, ER .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2000, 283 (1-2) :46-55
[6]  
KM Zhao, 2011, J MATER PROCESS TECH, V122, P6
[7]   Experimental and numerical life prediction of thermally cycled thermal barrier coatings [J].
Liu, Y ;
Persson, C ;
Wigren, J .
JOURNAL OF THERMAL SPRAY TECHNOLOGY, 2004, 13 (03) :415-424
[8]  
P Ramu, 2009, 2009011435 SAE INT
[9]   Impact of the non-homogenous temperature distribution and the coatings process modeling on the thermal barrier coatings system [J].
Ranjbar-Far, M. ;
Absi, J. ;
Shahidi, S. ;
Mariaux, G. .
MATERIALS & DESIGN, 2011, 32 (02) :728-735
[10]   Simulation of the effect of material properties and interface roughness on the stress distribution in thermal barrier coatings using finite element method [J].
Ranjbar-Far, M. ;
Absi, J. ;
Mariaux, G. ;
Dubois, F. .
MATERIALS & DESIGN, 2010, 31 (02) :772-781