Residual stresses in environmental and thermal barrier coatings on curved superalloy substrates: Experimental measurements and modelling

被引:11
|
作者
Liu, D. [1 ]
Kyaw, S. T. [2 ]
Flewitt, P. E. J. [1 ,3 ]
Seraffon, M. [4 ,6 ]
Simms, N. J. [4 ]
Pavier, M. [5 ]
Jones, I. A. [2 ]
机构
[1] Univ Bristol, Sch Phys, Interface Anal Ctr, Bristol BS8 1TL, Avon, England
[2] Univ Nottingham, Div Mat Mech & Struct, Nottingham NG7 2RD, England
[3] Univ Bristol, Sch Phys, HH Wills Phys Lab, Bristol BS8 1TL, Avon, England
[4] Cranfield Univ, Cranfield MK43 0AL, Beds, England
[5] Univ Bristol, Dept Mech Engn, Bristol BS8 1TR, Avon, England
[6] Natl Phys Lab, Teddington TW11 0LW, Middx, England
关键词
NONDESTRUCTIVE EVALUATION; GAS-TURBINE; TBC SYSTEM; OXIDATION; DEGRADATION; FAILURE; CREEP; DELAMINATION; TEMPERATURE; PERFORMANCE;
D O I
10.1016/j.msea.2014.03.014
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Residual stresses within thermal barrier coated (TBC) systems are predicted using finite element models and are compared against experimental measurements taken using Raman and photo-stimulated luminescence piezo-spectroscopic methods. Two types of specimens were considered: flat specimens without TBC, and aerofoil shaped specimens with TBC. Comparisons between model predictions and experimentally measured stresses and also the relationship between substrate curvature and residual stresses on subsequent spallation of the aerofoil specimen were made. For the flat specimen, predicted and measured residual stresses are of the same order of magnitude. Both studies have indicated that larger compressive residual stresses arise from higher substrate curvatures. The results improve the understanding of initiation and propagation of TBC cracks which occurs preferentially at locations with high substrate convex curvature. (C) 2014 Elsevier B.V. All rights reserved.
引用
收藏
页码:117 / 126
页数:10
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