刘昌鹏,雷伟,冉旭东,张菲玥.TaSi2改性ZrB2/SiC复合粉末制备及涂层抗氧化性能研究[J].表面技术,2023,52(10):350-359.
LIU Chang-peng,LEI Wei,RAN Xu-dong,ZHANG Fei-yue.Preparation of ZrB2/SiC Composite Powder Modified by TaSi2 and the Antioxidant Property of Its Coating[J].Surface Technology,2023,52(10):350-359
TaSi2改性ZrB2/SiC复合粉末制备及涂层抗氧化性能研究
Preparation of ZrB2/SiC Composite Powder Modified by TaSi2 and the Antioxidant Property of Its Coating
投稿时间:2022-10-18  修订日期:2023-02-26
DOI:10.16490/j.cnki.issn.1001-3660.2023.10.030
中文关键词:  C/C复合材料  ZrB2/SiC  TaSi2  大气等离子喷涂  涂层致密度  抗氧化烧蚀
英文关键词:C/C composites  ZrB2/SiC  TaSi2  atmospheric plasma spraying  coating density  anti-oxidation ablation
基金项目:
作者单位
刘昌鹏 西南技术工程研究所,重庆 400000 
雷伟 西南技术工程研究所,重庆 400000 
冉旭东 西南技术工程研究所,重庆 400000 
张菲玥 西南技术工程研究所,重庆 400000 
AuthorInstitution
LIU Chang-peng Southwest Institute of Technology and Engineering, Chongqing 400000, China 
LEI Wei Southwest Institute of Technology and Engineering, Chongqing 400000, China 
RAN Xu-dong Southwest Institute of Technology and Engineering, Chongqing 400000, China 
ZHANG Fei-yue Southwest Institute of Technology and Engineering, Chongqing 400000, China 
摘要点击次数:
全文下载次数:
中文摘要:
      目的 提高ZrB2/SiC涂层的致密性及抗氧化烧蚀能力。方法 设计向ZrB2/SiC涂层中掺杂TaSi2,以提升ZrB2/SiC涂层的致密度和抗氧化性能。首先通过喷雾造粒法制备了4种不同成分配比的复合团聚粉,然后采用大气等离子喷涂(APS)在C/C基体表面制备了4种团聚粉复合涂层,最后使用氧-乙炔火焰法对所制备的涂层进行了烧蚀考核。结果 通过涂层致密度对比发现,随着TaSi2的增加,涂层共晶区会有所增加,涂层致密度得到了明显改善。通过烧蚀考核发现,TaSi2的加入能够增加SiO2的含量,并产生热稳定性好的TaZr2.75O8。此外致密TaZr2.75O8的产生还能够有效改善涂层的抗氧化烧蚀性能。结论 最终得出的ZrB2/SiC涂层硅化物掺杂改性方案为30%TaSi2/42%ZrB2/28%SiC(体积分数)大气等离子喷涂制备的抗氧化烧蚀涂层,其在1 600 ℃烧蚀5 min后的质量损失率为‒1.70×10‒4 g/s。
英文摘要:
      Because of its excellent performance, hypersonic vehicle has become the commanding point of military strategy and technology of military powers. C/C composites with high strength, light weight and good seismic performance have attracted wide attention. C/C composites not only have good electrical conductivity, thermal conductivity and light weight characteristics, but also have good friction resistance, high temperature resistance, thermal shock resistance and corrosion resistance, especially because of their excellent high temperature mechanical properties, so they become one of the ideal materials for hypersonic aircraft. However, due to the complex service environment of hypersonic vehicle (high temperature, water and oxygen environment), oxidation and ablation of C/C composites under high temperature and aerobic conditions have become the bottleneck of its wide application. The preparation of ZrB2/SiC coatings on C/C composites by atmospheric plasma spraying (APS ) is one of the effective methods to improve the anti-oxidation ablation performance and prolong the service life of C/C composites. However, the coatings still have some shortcomings such as difficult densification, low emissivity and fast heating rate, so they cannot be widely used.
查看全文  查看/发表评论  下载PDF阅读器
关闭

关于我们 | 联系我们 | 投诉建议 | 隐私保护 | 用户协议

您是第20626137位访问者    渝ICP备15012534号-3

版权所有:《表面技术》编辑部 2014 surface-techj.com, All Rights Reserved

邮编:400039 电话:023-68792193传真:023-68792396 Email: bmjs@surface-techj.com

渝公网安备 50010702501715号