Effects of interface roughness on the life estimation of a thermal barrier coating layer

被引：5
作者：
Ragupathy, R. [1 ]
Panigrahi, S. K. [2 ]
Mishra, R. K. [1 ]
机构：
[1] CEMILAC, RCMAE, HAL Engine Div, Bangalore 560093, Karnataka, India
[2] Def Inst Adv Technol, Dept Mech Engn, Pune 411025, Maharashtra, India
来源：
INTERNATIONAL JOURNAL OF SURFACE SCIENCE AND ENGINEERING | 2013年 / 7卷 / 03期
关键词：
thermal barrier coating; TBC; finite element analysis; FEA; gas turbine engine; interface roughness;
D O I：
10.1504/IJSURFSE.2013.056438
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
Methodology development for life estimation of thermal barrier coating (TBC) applied on a gas turbine engine combustor liner has been undertaken using finite element method. 3-D finite element analyses (FEA) are performed using ABAQUS followed by fatigue analysis through FESAFE for life estimation of a TBC layer. Analysis considers a typical mission cycle of a gas turbine engine while modelling the transition liner of a reverse flow combustion chamber. This paper presents the influence of interface roughness on the life of TBC layer. Three different cases of interface roughness have been studied. Roughness is found to affect TBC life adversely. In addition to effect of interface roughness, the life estimation methodology is also discussed.
引用
收藏
页码：269 / 284
页数：16
相关论文
共 50 条
  • [41] A physics-based life prediction methodology for thermal barrier coating systems
    Busso, E. P.
    Wright, L.
    Evans, H. E.
    McCartney, L. N.
    Saunders, S. R. J.
    Osgerby, S.
    Nunn, J.
    ACTA MATERIALIA, 2007, 55 (05) : 1491 - 1503
  • [42] Effect of Supersonic Fine Particles Bombarding on the Service Life of Thermal Barrier Coating
    Lin Xiaoping
    Dong Yun
    Wang Zhiping
    Liu Shiqiang
    Ren Zhimin
    Ding Kunying
    CHINESE JOURNAL OF MECHANICAL ENGINEERING, 2011, 24 (05) : 911 - 916
  • [43] Effect of Supersonic Fine Particles Bombarding on the Service Life of Thermal Barrier Coating
    LIN Xiaoping1
    Chinese Journal of Mechanical Engineering, 2011, 24 (05) : 911 - 916
  • [44] Influence of surface roughness of thermal barrier coating on the cooling performance of a film-cooled turbine vane
    Song, Xiaoyu
    Liu, Feng
    Yan, Yan
    Wang, Wen
    Wang, Yaning
    Sun, Wei
    Cui, Jiahuan
    CASE STUDIES IN THERMAL ENGINEERING, 2025, 65
  • [45] Coupled effects of temperature gradient and oxidation on thermal stress in thermal barrier coating system
    Zhou, YC
    Hashida, T
    INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2001, 38 (24-25) : 4235 - 4264
  • [46] The effect of the thermal barrier coating on the displacement instability in thermal barrier systems
    Karlsson, AM
    Xu, T
    Evans, AG
    ACTA MATERIALIA, 2002, 50 (05) : 1211 - 1218
  • [47] Thermal conductivity of a zirconia thermal barrier coating
    Slifka A.J.
    Filla B.J.
    Phelps J.M.
    Bancke G.
    Berndt C.C.
    Journal of Thermal Spray Technology, 1998, 7 (1) : 43 - 46
  • [48] Effects of Thermal Barrier Coating on Temperature and Stress of Turbine Rotor Blade
    Zhang Z.-X.
    Zeng W.
    Bian X.-D.
    Gao G.-L.
    Xiao B.
    Tuijin Jishu/Journal of Propulsion Technology, 2023, 44 (05):
  • [49] Detection of thermally grown oxide layer in thermal barrier coating for gas turbines by photoluminescence
    Fukuchi, Tetsuo
    Eto, Shuzo
    Okada, Mitsutoshi
    Fujii, Tomoharu
    IEEJ Transactions on Fundamentals and Materials, 2013, 133 (07) : 402 - 407+3
  • [50] Development of a Portable System for Detection of Thermally Grown Oxide Layer in Thermal Barrier Coating
    Fukuchi, Tetsuo
    Okada, Mitsutoshi
    Fujii, Tomoharu
    ELECTRONICS AND COMMUNICATIONS IN JAPAN, 2017, 100 (02) : 76 - 82
12345