Ablation behavior of Hf-Zr-modified silicon-based ceramic coatings prepared by polymer derived ceramics and gaseous silicon infiltration

IF 6.9 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Lingxiang Guo, Yue Dong, Yuqi Wang, Shiwei HUANG, Laura Feldmann, Ralf Riedel, Jia Sun
{"title":"Ablation behavior of Hf-Zr-modified silicon-based ceramic coatings prepared by polymer derived ceramics and gaseous silicon infiltration","authors":"Lingxiang Guo, Yue Dong, Yuqi Wang, Shiwei HUANG, Laura Feldmann, Ralf Riedel, Jia Sun","doi":"10.1016/j.cja.2025.104010","DOIUrl":null,"url":null,"abstract":"To improve the ablation resistance of C/C composite at temperatures exceeding 2000 °C, a (Hf-Zr)C-SiC Ultra-High Temperature Ceramic (UHTC) coating was prepared by Polymer Derived Ceramics (PDCs) and Gaseous Silicon Infiltration (GSI). The linear ablation rate of the coated C/C composites was as low as 0.27 μm/s, maintaining a level as low as 10 -4 mm/s. This low R l is attributed to the formation of a well-bonded double-layered oxide scale with high thermal stability, consisting of an exterior SiO 2 glass layer and an interior Hf-Zr-Si-O complex oxide layer. Meanwhile, the dissipation of the residual Si and the C phase relieves heat accumulation, ensuring that the recorded surface temperature remains below 2000 °C, thereby enhancing the ablation resistance. Additionally, a cyclic evolution of linear ablation rate was found, due to the alternating dominant role of oxidation and mechanical denudation on the coating during ablation. This study provides theoretical and experimental support for the long-term anti-ablation design of highly dense UHTC coatings.","PeriodicalId":55631,"journal":{"name":"Chinese Journal of Aeronautics","volume":"1 1","pages":"104010-104010"},"PeriodicalIF":6.9000,"publicationDate":"2025-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Chinese Journal of Aeronautics","FirstCategoryId":"0","ListUrlMain":"https://doi.org/10.1016/j.cja.2025.104010","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

To improve the ablation resistance of C/C composite at temperatures exceeding 2000 °C, a (Hf-Zr)C-SiC Ultra-High Temperature Ceramic (UHTC) coating was prepared by Polymer Derived Ceramics (PDCs) and Gaseous Silicon Infiltration (GSI). The linear ablation rate of the coated C/C composites was as low as 0.27 μm/s, maintaining a level as low as 10 -4 mm/s. This low R l is attributed to the formation of a well-bonded double-layered oxide scale with high thermal stability, consisting of an exterior SiO 2 glass layer and an interior Hf-Zr-Si-O complex oxide layer. Meanwhile, the dissipation of the residual Si and the C phase relieves heat accumulation, ensuring that the recorded surface temperature remains below 2000 °C, thereby enhancing the ablation resistance. Additionally, a cyclic evolution of linear ablation rate was found, due to the alternating dominant role of oxidation and mechanical denudation on the coating during ablation. This study provides theoretical and experimental support for the long-term anti-ablation design of highly dense UHTC coatings.
聚合物衍生陶瓷和气态硅浸润制备hf - zr改性硅基陶瓷涂层的烧蚀行为
为了提高C/C复合材料在2000℃以上的耐烧蚀性能,采用聚合物衍生陶瓷(PDCs)和气态硅渗透(GSI)制备了一种(Hf-Zr)C- sic超高温陶瓷(UHTC)涂层。涂层C/C复合材料的线性烧蚀速率低至0.27 μm/s,保持在10 ~ 4 mm/s的水平。这种低的R -l是由于形成了一种结合良好的双层氧化层,具有很高的热稳定性,由外部的sio2玻璃层和内部的Hf-Zr-Si-O复合氧化层组成。同时,残余Si和C相的耗散减少了热量的积累,确保记录的表面温度保持在2000℃以下,从而增强了抗烧蚀性。此外,由于在烧蚀过程中涂层的氧化和机械剥蚀交替起主导作用,发现了线性烧蚀速率的循环演变。本研究为高密度UHTC涂层的长期抗烧蚀设计提供了理论和实验支持。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics 工程技术-工程:宇航
CiteScore
10.00
自引率
17.50%
发文量
3080
审稿时长
55 days
期刊介绍: Chinese Journal of Aeronautics (CJA) is an open access, peer-reviewed international journal covering all aspects of aerospace engineering. The Journal reports the scientific and technological achievements and frontiers in aeronautic engineering and astronautic engineering, in both theory and practice, such as theoretical research articles, experiment ones, research notes, comprehensive reviews, technological briefs and other reports on the latest developments and everything related to the fields of aeronautics and astronautics, as well as those ground equipment concerned.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信
小红书