留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

热障涂层热应力影响因素的正交有限元分析

李志永 张建宇 鲍蕊 费斌军

李志永, 张建宇, 鲍蕊, 等 . 热障涂层热应力影响因素的正交有限元分析[J]. 北京航空航天大学学报, 2010, 36(11): 1339-1342.
引用本文: 李志永, 张建宇, 鲍蕊, 等 . 热障涂层热应力影响因素的正交有限元分析[J]. 北京航空航天大学学报, 2010, 36(11): 1339-1342.
Li Zhiyong, Zhang Jianyu, Bao Rui, et al. Finite element analysis of factors to thermal stress in thermal barrier coatings with orthogonal method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(11): 1339-1342. (in Chinese)
Citation: Li Zhiyong, Zhang Jianyu, Bao Rui, et al. Finite element analysis of factors to thermal stress in thermal barrier coatings with orthogonal method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(11): 1339-1342. (in Chinese)

热障涂层热应力影响因素的正交有限元分析

详细信息
    作者简介:

    李志永(1979-),男,河北唐山人,博士生,canyonli@163.com.

    通讯作者:

    李志永

  • 中图分类号: V214.4

Finite element analysis of factors to thermal stress in thermal barrier coatings with orthogonal method

More Information
    Corresponding author: Li Zhiyong
  • 摘要: 利用有限元分析方法,采用Walker粘塑性材料本构模型计算了喷涂于圆管型试件上的热障涂层在室温和高温环境下的热应力.使用试验中常用的正交设计分析方法,分析了热障涂层不同的结构和喷涂工艺中的4种因素在取不同的水平条件时对热障涂层热应力的影响.分析结果表明:对于所考察的危险点,4种因素对热障涂层中热应力的产生都有显著影响,其中以氧化层的厚度对其影响最为严重;4种因素随其各自水平的变化对涂层内部应力变化的影响规律不同.

     

  • [1] Mao W G,Zhou Y C,Yang L,et al.Modeling of residual stresses variation with thermal cycling in thermal barrier coatings[J].Mechanics of Materials,2006,38(12):1118-1127 [2] 马维,潘文霞,吴承康.热障涂层材料性能和失效机理研究进展[J].力学进展,2003,33(4):548-559 Ma Wei,Pan Wenxia,Wu Chengkang.Progress in research on the material properties and failure mechanisms of thermal barrier coatings [J].Advances in Mechanics,2003,33(4):548-559(in Chinese) [3] Liu Aiguo,Wei Yanhong.Finite element analysis of anti-spallation thermal barrier coatings[J].Surface and Coatings Technology,2003,165(2):154-162 [4] Busso E P,Wright L,Evans H E,et al.A Physis-based life prediction methodology for thermal barrier coating systems[J].Acta Material,2007,55(5):1491-1503 [5] Chang G C,Phucharoen W,Miller R A.Finite element thermal stress solutions for thermal barrier coatings[J].Surface and Coatings Technology,1987,32(1/2/3/4):307-325 [6] 耿瑞.热障涂层强度分析及寿命预测研究 .北京:北京航空航天大学能源与动力工程学院,2001 Geng Rui.Thermal barrier coatings strength analysis and life prediction .Beijing:School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,2001(in Chinese) [7] 陈火红,尹伟奇,薛小香.MSC.Marc二次开发指南[M].北京:科学出版社,2004:356-382 Chen Huohong,Yin Weiqi,Xue Xiaoxiang.Redevelop technology guide of MSC.Marc[M].Beijing:Science Press,2004:356-382(in Chinese) [8] Zhou Chungen,Wang Na,Xu Huibin.Comparison of thermal cycling behavior of plasma-sprayed nanostructured and traditional thermal barrier coatings[J].Materials Science and Engineering,2007(452/453):569-574 [9] 韩於羹.应用数理统计[M].北京:北京航空航天大学出版社,2006:433 Han Yugeng.Application mathematical statistic[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2006:433(in Chinese) [9] Rabiei A,Evans A G.Failure mechanisms associated with the thermally grown oxide in plasma-sprayed thermal barrier coatings[J].Acta Mater,2000,48(15):3963-3976
  • 加载中
计量
  • 文章访问数:  3324
  • HTML全文浏览量:  256
  • PDF下载量:  1097
  • 被引次数: 0
出版历程
  • 收稿日期:  2009-09-28
  • 网络出版日期:  2010-11-30

目录

    /

    返回文章
    返回
    常见问答