Effect of gas pressure on thermal conductivity of zirconia thermal barrier coatings

被引:15
|
作者
Mogro-Campero, A
Johnson, CA
Bednarczyk, PJ
Dinwiddie, RB
Wang, H
机构
[1] GE, Ctr Res & Dev, Niskayuna, NY 12309 USA
[2] Oak Ridge Natl Lab, Oak Ridge, TN 37831 USA
来源
SURFACE & COATINGS TECHNOLOGY | 1997年 / 94-5卷 / 1-3期
关键词
gas pressure; thermal conductivity; zirconia thermal barrier coatings;
D O I
10.1016/S0257-8972(97)00485-4
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The thermal diffusivity thermal barrier coatings (zirconia stabilized with 7-8 wt% yttria) deposited by air plasma spraying has been measured by the laser flash method. Free-standing samples (0.5-0.6-mm thick) polished on both sides wen coated with graphite. Deduced values of thermal conductivity (e.g., 1.5 W m(-1) K-1 at 200 degrees C in 1 atm. of nitrogen) are in the range measured in other studies for this type of thermal barrier coating. The % increase in thermal conductivity in I arm. of gas compared to its value in vacuum was found to be about 10% in nitrogen at 500 degrees C, close to a calculated value of 7% using a model in the literature. A simple extension of the model to higher temperatures and gas pressures predicts a significant rise, so that by 10 atm. of gas pressure the % increase would be 30% (with little sensitivity to temperature). (C) 1997 Elsevier Science S.A.
引用
收藏
页码:102 / 105
页数:4
相关论文
共 50 条
  • [1] Effect of gas pressure on thermal conductivity of zirconia thermal barrier coatings
    GE Research and Development Cent, Niskayuna, United States
    Surf Coat Technol, 1-3 (102-105):
  • [2] Effect of Sintering on Thermal Conductivity and Thermal Barrier Effects of Thermal Barrier Coatings
    Wang Kai
    Peng Hui
    Guo Hongbo
    Gong Shengkai
    CHINESE JOURNAL OF AERONAUTICS, 2012, 25 (05) : 811 - 816
  • [4] Effect of Sintering on Thermal Conductivity and Thermal Barrier Effects of Thermal Barrier Coatings
    WANG Kai PENG Hui GUO Hongbo GONG Shengkai School of Materials Science and Engineering Beihang University Beijing China
    Chinese Journal of Aeronautics, 2012, 25 (05) : 811 - 816
  • [5] Phase composition and thermal conductivity of zirconia-based thermal barrier coatings
    Mazilin, I. V.
    Baldaev, L. Kh
    Drobot, D. V.
    Marchukov, E. Yu
    Zaitsev, N. G.
    INORGANIC MATERIALS, 2016, 52 (08) : 802 - 810
  • [6] Phase composition and thermal conductivity of zirconia-based thermal barrier coatings
    I. V. Mazilin
    L. Kh. Baldaev
    D. V. Drobot
    E. Yu. Marchukov
    N. G. Zaitsev
    Inorganic Materials, 2016, 52 : 802 - 810
  • [7] Thermal conductivity of zirconia for thermal barrier coatings: A perturbed molecular dynamics study
    Yoshiya, Masato
    Matsumoto, Mineaki
    Harada, Akihiko
    Takeuchi, Munetaka
    Matsubara, Hideaki
    SCIENCE OF ENGINEERING CERAMICS III, 2006, 317-318 : 521 - 524
  • [8] ZIRCONIA THERMAL BARRIER COATINGS FOR GAS-TURBINES
    AMMANN, CL
    AMERICAN CERAMIC SOCIETY BULLETIN, 1976, 55 (08): : 744 - 744
  • [9] Thermal conductivity of thermal barrier coatings
    Il'inkov A.V.
    Il'inkova T.A.
    Shchukin A.V.
    Basargin I.V.
    Valiev R.R.
    Russian Aeronautics (Iz VUZ), 2009, 52 (3) : 340 - 346
  • [10] Thermal Conductivity of a Zirconia Thermal Barrier Coating
    A.J. Slifka
    B.J. Filla
    J.M. Phelps
    G. Bancke
    C.C. Berndt
    Journal of Thermal Spray Technology, 1998, 7 : 43 - 46