陶瓷前驱体基高温高辐射涂层制备及表征
DOI:
作者:
作者单位:

航天材料及工艺研究所

作者简介:

通讯作者:

中图分类号:

V468

基金项目:


Preparation and Characterization of Ceramic Precursor BasedHigh-Temperature High Emissivity Coatings
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    以陶瓷前驱体树脂为成膜物,以过渡金属氧化物和硼化物为填料,采用空气喷涂工艺在镍基高
    温合金和 C/ C 基材上制备出了高温散热性能好、抗热震性好的高温高辐射涂层,并用 DSC-TG、光学显微镜和
    风洞对涂层性能进行表征。 结果表明:该涂层室温 ~827℃发射率达到 0. 85 ~0. 92,827℃ ~ 室温抗热震循环
    20 次后涂层不剥离、不脱落;该涂层在 290 kW/ m 2 冷壁热流、300 s 时长的风洞考核条件下,可将镍基高温合金
    基材温度从 686℃降到 646℃,降温 40℃。

    Abstract:

    The high emissivity coatings on the nicke-based alloy and C/ C composite, with good radiating ability
    and good thermal shock resistance ability, were prepared by air spray, using ceramic precursor resin as coating form-
    ing matter and transition metal oxides and borides as high emissivity fillers. The high emissivity coatings were charac-
    terized by DSC-TG, optical microscope, and wind tunnel. The emissivity of the high emissivity coating is 0. 85 to
    0. 92 between room temperature and 827℃. The high emissivity coating has no spalling after thermal shock resistance
    measurement of 20 times between 827℃ and room temperature. The high emissivity coating on the nickel-based alloy
    can make the temperature of the nickel-based alloy decrease from 686 to 646℃, decreasing by 40℃.

    参考文献
    相似文献
    引证文献
引用本文

李俊峰.陶瓷前驱体基高温高辐射涂层制备及表征[J].宇航材料工艺,2016,46(1).

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2016-11-28
  • 出版日期:
第十一届航天复合材料成形与加工工艺技术中心交流会 征文通知

关闭