...
首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Extreme Temperature Coatings for Future Gas Turbine Engines
【24h】

Extreme Temperature Coatings for Future Gas Turbine Engines

机译:未来燃气涡轮发动机的极端温度涂层

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

The National Energy Technology Laboratory-Regional University Alliance (NETL-RUA) has been developing extreme temperature coating systems that consist of a diffusion barrier coating (DBC), a low-cost wet slurry bond coat, a commercial yttria stabilized zirconia (YSZ) thermal barrier coating (TBC), and an extreme temperature external coating that are deposited along the surface of nickel-based superalloys and single crystal metal substrates. Thermal cyclic testing of these multilayer coatings was conducted in steam-containing environments at temperatures ranging between 1100 and 1550 ℃. This paper discusses the response of these materials during bench-scale testing, and their potential use in advanced H- and J-class land-based gas turbine engines.
机译:美国国家能源技术实验室-地区大学联盟(NETL-RUA)一直在开发极限温度涂层系统,该系统由扩散阻挡涂层(DBC),低成本湿浆粘结涂层,商业氧化钇稳定的氧化锆(YSZ)热沿镍基高温合金和单晶金属基底表面沉积的阻挡涂层(TBC)和极端温度外部涂层。这些多层涂层的热循环测试是在含蒸汽的环境中于1100至1550℃的温度范围内进行的。本文讨论了这些材料在实验室规模测试期间的响应,以及它们在先进的H级和J级陆基燃气涡轮发动机中的潜在用途。

著录项

  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2014年第11期|112102.1-112102.8|共8页
  • 作者单位

    U.S. DOE National Energy, Technology Laboratory, Pittsburgh, PA 15236;

    Coatings For Industry, Souderton, PA 18964;

    Coatings For Industry, Souderton, PA 18964;

    NASA Glenn Research Center, Cleveland, OH 44135;

    University of Pittsburgh, Pittsburgh, PA 15261;

    Corrosion Control Consultants, Inc., Beaver, PA 15009;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号