Thermal-barrier coatings for more efficient gas-turbine engines

被引:9
|
作者
David R. Clarke
Matthias Oechsner
Nitin P. Padture
机构
[1] Harvard University,School of Engineering and Applied Sciences
[2] Center for Structural Materials,School of Engineering
[3] Technische Universitaet Darmstadt,undefined
[4] Brown University,undefined
来源
MRS Bulletin | 2012年 / 37卷
关键词
D O I
暂无
中图分类号
学科分类号
摘要
Gas-turbine engines used in transportation, energy, and defense sectors rely on high-temperature thermal-barrier coatings (TBCs) for improved efficiencies and power. The promise of still higher efficiencies and other benefits is driving TBCs research and development worldwide. An introduction to TBCs—complex, multi-layer evolving systems—is presented, where these fascinating systems touch on several known phenomena in materials science and engineering. Critical elements identified as being important to the development of future TBCs form the basis for the five articles in this issue of MRS Bulletin. These articles are introduced, together with a discussion of the major challenges to improved coating development and the rich opportunities for materials research they provide.
引用
收藏
页码:891 / 898
页数:7
相关论文
共 50 条
  • [21] Erratum to: “Thermal nondestructive testing of thermal-barrier coatings of turbine buckets”
    V. P. Vavilov
    S. Marinetti
    F. Cernuschi
    D. Robba
    Russian Journal of Nondestructive Testing, 2016, 52 : 538 - 538
  • [22] GAS-TURBINE ENGINES
    METZGER, DE
    MAYLE, RE
    MECHANICAL ENGINEERING, 1983, 105 (06) : 44 - 52
  • [23] Measuring thermal-barrier coatings
    不详
    MATERIALS PERFORMANCE, 1999, 38 (04) : 16 - 16
  • [24] Enhancement of the Heat Resistance of Coatings for the Blades of Gas-Turbine Engines
    S. G. Rudenkyi
    E. V. Timofeeva
    A. V. Kunchenko
    A. A. Korneev
    M. A. Bortnitskaya
    V. V. Kunchenko
    Yu. V. Kunchenko
    T. P. Ryzhova
    Materials Science, 2020, 55 : 569 - 576
  • [25] Enhancement of the Heat Resistance of Coatings for the Blades of Gas-Turbine Engines
    Rudenkyi, S. G.
    Timofeeva, E., V
    Kunchenko, A., V
    Korneev, A. A.
    Bortnitskaya, M. A.
    Kunchenko, V. V.
    Kunchenko, Yu, V
    Ryzhova, T. P.
    MATERIALS SCIENCE, 2020, 55 (04) : 569 - 576
  • [26] THE DURABILITY AND PERFORMANCE OF COATINGS IN GAS-TURBINE AND DIESEL-ENGINES
    FAIRBANKS, JW
    HECHT, RJ
    MATERIALS SCIENCE AND ENGINEERING, 1987, 88 : 321 - 330
  • [27] THERMAL BARRIER COATINGS FOR TURBINE APPLICATIONS IN AERO ENGINES
    RHYSJONES, TN
    TORIZ, FC
    HIGH TEMPERATURE TECHNOLOGY, 1989, 7 (02): : 73 - 81
  • [28] GAS SCREEN IN GAS-TURBINE ENGINES
    VARGANOV, IS
    IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1979, (01): : 11 - 16
  • [29] CERAMICS FOR GAS-TURBINE ENGINES
    TORTI, ML
    MATERIALS AND SOCIETY, 1984, 8 (02): : 219 - 220
  • [30] COGENERATION WITH GAS-TURBINE ENGINES
    NAJJAR, YSH
    AKYURT, M
    ALRABGHI, OM
    ALP, T
    HEAT RECOVERY SYSTEMS & CHP, 1993, 13 (05): : 471 - 480