Volume 33 Issue 7
Jul.  2018
Turn off MathJax
Article Contents
Effects of oxide layer non-uniform growth on thermal barrier coating stress distribution[J]. Journal of Aerospace Power, 2018, 33(7): 1606-1611. doi: 10.13224/j.cnki.jasp.2018.07.008
Citation: Effects of oxide layer non-uniform growth on thermal barrier coating stress distribution[J]. Journal of Aerospace Power, 2018, 33(7): 1606-1611. doi: 10.13224/j.cnki.jasp.2018.07.008

Effects of oxide layer non-uniform growth on thermal barrier coating stress distribution

doi: 10.13224/j.cnki.jasp.2018.07.008
  • Received Date: 2016-12-20
  • Publish Date: 2018-07-28
  • Thermal barrier coatings (TBCs) with different oxidation time were observed using scanning electron microscopy. It was found that the thermally grown oxide layers (TGO) did not grow uniformly. Assuming that the shape of the thermally grown oxide layer was sinusoidal, the basic geometrical parameters of the thermally grown oxide layer could be obtained by statistical processing of scanning electron micrographs. Then the two-dimensional axisymmetric finite element models of single waveform were established and the stress states were calculated and analyzed. Results showed that the trend of the axial, shear and Mises stress components of the non-uniform growth model were consistent with those of the uniform growth model under the same temperature, but the maximum stress components of the inhomogeneous growth model were smaller than those of the homogeneous growth model.

     

  • loading
  • [1]
    ROBERT A M.Current status of thermal barrier coatings:an overview[J].Surface and Coatings Technology,1987,30(1):1-11.
    [2]
    韩萌,黄继华,陈树海.热障涂层应力与失效机理若干关键问题的研究进展与评述[J].航空材料学报,2013,33(5):83-98.HAN Meng,HUANG Jihua,CHEN Shuhai.Research progress and review on key problem of stress and failure mechanism of thermal barrier coating[J].Journal of Aeronautical Materials,2013,33(5):83-98.(in Chinese)
    [3]
    SCHULZ U,LEYENS C,FRITSCHER K,et al.Some recent trends in research and technology of advanced thermal barrier coatings[J].Aerospace Science and Technology,2003,7(1):73-80.
    [4]
    XU Huibin,GUO Hongbo,LIU Fushun,et al.Development of gradient thermal barrier coatings and their hot-fatigue behavior[J].Surface and Coatings Technology,2000,130(1):133-139.
    [5]
    刘纯波,林锋,蒋显亮.热障涂层的研究现状与发展趋势[J].中国有色金属学报,2007,17(1):1-13.LIU Chunbo,LIN Feng,JIANG Xianliang.The present situation and the development trend of thermal barrier coatings[J].The Chinese Journal of Nonferrous Metals,2007,17(1):1-13.(in Chinese)
    [6]
    EPSTEIN A H,GREITZER E M,KERREBROCK J L.Aircraft and rocket turbines:advances in physics and design[M].Wexford:Wexford College Press,2008.
    [7]
    HE M Y,MUMM D R,EVANS A G.Criteria for the delamination of thermal barrier coatings:with application to thermal gradients[J].Surface and Coatings Technology,2004,185(2/3):184-193.
    [8]
    齐红宇,马立强,李少林,等.等离子热障涂层构件高温热疲劳寿命预测研究[J].材料工程,2014,21(7):67-72.QI Hongyu,MA Liqiang,LI Shaolin,et al.High temperature thermal fatigue life prediction of p1asma sprayed thermal barrier coatings structure[J].Journal of Materials Engineering,2014,21(7):67-72.(in Chinese)
    [9]
    郭洪波,宫声凯,徐惠彬.先进航空发动机热障涂层技术研究进展[J].中国材料进展,2009,28(9/10):18-26.GUO Hongbo,GONG Shengkai,XUE Huibin.Progress in thermal barrier coatings for advanced aeroengines[J].Materials China,2009,28(9/10):18-26.(in Chinese)
    [10]
    徐惠彬,宫声凯,刘福顺.航空发动机热障涂层材料体系的研究[J].航空学报,2000,21(1):7-12.XU Huibin,GONG Shengkai,LIU Fushun.Recent development in materials design of thermal barrier coatings for gas turbine[J].Acta Aeronautica et Astronautica Sinica,2000,21(1):7-12.(in Chinese)
    [11]
    杨晓光,耿瑞,周燕佩.热障涂层氧化和热疲劳寿命实验研究[J].航空动力学报,2003,18(2):195-200.YANG Xiaoguang,GENG Rui,ZHOU Yanpei.An experimental study of oxidation and thermal fatigue of TBC[J].Journal of Aerospace Power,2003,18(2):195-200.(in Chinese)
    [12]
    SCHLICHTING K W,PADTURE N P,JORDAN E H,et a1.Failure models in plasma-sprayed thermal barrier coatings[J].Materials Science and Engineering:A,2003,342(1/2):120-130.
    [13]
    BUSSO E P,LIN J,SAKURAI S,et a1.A mechanistic study of oxidation-induced degradation in a plasma-sprayed thermal barrier coating system:Part Ⅰ model formulation[J].Acta Materialia,2001,49(9):1515-1528.
    [14]
    BUSSO E P,LIN J,SAKURAI S,et a1.A mechanistic study of oxidation induced degradation in a plasma sprayed thermal barrier coating system:Part Ⅱ life prediction model[J].Acta Materialia,2001,49(9):1529-1536.
    [15]
    CHEN W R,WU X,DUDZINSKI D.Influence of thermal cycle frequency on the TGO growth and cracking behaviors of an APS-TBC[J].Journal of Thermal Spray Technology,2012,2l(6):1294-1299.
    [16]
    SHEFFLER K D,GUPTA D K.Current status and future trends in turbine application of thermal barrier coatings[J].Journal of Engineering for Gas Turbines and Power,1988,110(4):605-609.
    [17]
    王亚梅.热障涂层破坏机理及寿命分析方法的研究[D].北京:北京航空航天大学,2009.WANG Yamei.Research of failure mechanism and life prediction method of thermal barrier coatings[D].Beijing:Beijing University of Aeronautics and Astronautics,2005.(in Chinese)
    [18]
    郝勇,齐红宇,马立强.高温氧化对EB-PVD热障涂层内部应力场分布影响的数值模拟[J].航空动力学报,2014,29(7):1520-1526.HAO Yong,QI Hongyu,MA Liqiang.Numerical simulation of effect of high temperature oxidation on stress field distribution of EB-PVD thermal barrier coating[J].Journal of Aerospace Power,2014,29(7):1520-1526.(in Chinese)
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1069) PDF downloads(807) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return