期刊文献+

热冲击环境下涂层/基底界面的微观形貌及元素扩散规律研究

Study on Microstructure of Coating/Substrate Interface and Law of Element Diffusion in Thermal Shock Environment
下载PDF
导出
摘要 针对热障涂层在高温环境中长期服役的需求,研究热障涂层在热冲击环境下涂层/基底界面形貌演变及元素扩散规律。通过自主搭建的石英灯加热平台对热障涂层进行热冲击试验。利用SEM和EDS对热冲击后涂层/基底界面的微观形貌及元素分布进行分析,利用Boltzmann-Matano扩散模型计算了涂层/基底界面Al元素的扩散系数。结果表明,沉积态的热障涂层中黏结层(BC)主要由β和γ相组成,并且在涂层/基底界面已经出现扩散区;随着热冲击试验的进行,Al元素快速消耗致使BC层和基底间Al元素浓度梯度转变,Al元素开始向外扩散,部分拓扑密堆(TCP)相中富集的难熔元素可以重新固溶到基底中,最终各元素在界面区的分布逐渐均匀;Al元素的扩散系数在热冲击试验开始前为正值,到600次热冲击循环后为负值,且扩散系数的最大值均出现在涂层/基底界面处,距离界面越大,扩散系数就越低。 In order to meet the requirement of long-term service of thermal barrier coatings(TBCs)in high temperature environment,the morphology evolution of coating/substrate interface and the laws of element diffusion of TBCs in thermal shock environment were studied in this paper.The thermal shock tests of TBCs was carried out by the quartz lamp heating platform.The microstructure and element distribution of the coating/substrate interface after thermal shock were analyzed by SEM and EDS,and the diffusion coefficient of Al element at the coating/substrate interface was calculated by Boltzmann-Matano diffusion model.The results show that the BC layer was mainly composed ofβandγphases,and the diffusion zone has appeared at the coating/substrate interface.With the thermal shock tests,the rapid consumption of Al element caused the gradient shift of Al element concentration between BC layer and substrate,and Al element began to diffuse outward.Some refractory elements enriched in the topologically close-packed(TCP)phase could be solidly dissolved into the substrate again.Finally,the distribution of all elements gradually uniform in the interface region.The diffusion coefficient of Al element was positive before the thermal shock tests and negative after 600 cycles.The maximum diffusion coefficient appears at the coating/substrate interface.And the greater the distance from the interface,the lower the diffusion coefficient.
作者 杨来侠 高伟 赵晋超 高扬 徐超 YANG Laixia;GAO Wei;ZHAO Jinchao;GAO Yang;XU Chao(Xi’an University of Science and Technology,Xi’an 710054,China)
机构地区 西安科技大学
出处 《航空制造技术》 CSCD 北大核心 2023年第19期14-21,共8页 Aeronautical Manufacturing Technology
基金 陕西省教育厅2022年度服务地方专项科研计划(22C053)。
关键词 热障涂层(TBCs) 热冲击 元素扩散 扩散系数 拓扑密堆相(TCP) Thermal barrier coatings(TBCs) Thermal shock Element diffusion Diffusion coefficient Topologically close-packed phase(TCP)
  • 相关文献

参考文献8

二级参考文献121

  • 1苏罗川,张伟旭,王铁军.热障涂层系统内粘结层循环塑性研究[J].固体力学学报,2013,34(S1):99-104. 被引量:1
  • 2骆宇时,李嘉荣,刘世忠,孙凤礼,韩梅,曹春晓.Re对单晶高温合金高温高应力持久性能的影响[J].中国有色金属学报,2005,15(11):1655-1659. 被引量:11
  • 3熊玉明,李明升,李松林.热障涂层与镍基高温合金界面的互扩散行为[J].粉末冶金材料科学与工程,2007,12(2):63-69. 被引量:11
  • 4Matsumoto K, Itoh Y, Kameda T, EB-PVD Process and Thermal Properties of Hafnia-Based Thermal Barrier Coating [ J ]. Science and Technology of Advanced Materials, 2003(4) : 153 - 158.
  • 5Miller R A, Current Status of Thermal Barrier Coatings-an Overview[J]. SurCoat Technol, 1987, 30:1-11.
  • 6Miller R A, Thermal Barrier Coatings for Aircraft Engines : History and Directions[J]. J Thermal Spray Tech, 1997(6) : 35 -42.
  • 7Cao X Q, Vassen R, Stoever D, Ceramic Materials for Thermal Barrier Coatings [ J ]. Journal of the European Ceramic Society, 2004, 24: 1-10.
  • 8Goward G W. Protective Coating Systems for High-Temperature Gas Turbine Components[J~. Mat Sci Tech, 1986(2) : 194 -200.
  • 9Hecht R J, Goward G W, Elam R C. High Temperature NiCoCrAlY Coatings: United States, Patent No. 3928026[ P], 1975.
  • 10Zhu D M, Miller R A, Thermal Conductivity and Sintering Behavior of Advanced Thermal Barrier Coatings [ R ]. Ohio : Ohio Aerospace Institute, Brook Park, Ohio, 2002.

共引文献176

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部