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材料导报  2024, Vol. 38 Issue (3): 22060154-10    https://doi.org/10.11896/cldb.22060154
  无机非金属及其复合材料 |
SiC-ZrC复相超高温陶瓷改性C/C复合材料的研究进展
张倩玮, 陈意高, 崔红*, 吴小军
西安航天复合材料研究所,西安 710025
Research Progress of SiC-ZrC Multiphase Ultra-high Temperature Ceramic Modified C/C Composites
ZHANG Qianwei, CHEN Yigao, CUI Hong*, WU Xiaojun
Research Institute of Xi'an Aerospace Composites Materials, Xi'an 710025, China
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摘要 SiC-ZrC复相超高温陶瓷改性C/C复合材料的制备工艺原理与单一陶瓷相改性C/C复合材料的工艺原理基本相同,但SiC-ZrC复相陶瓷具有耐高温、温域宽(1 600～2 500 ℃)、抗氧化、工艺适应性好等优点,在测试和应用中表现出优异的力学性能和抗烧蚀性能,能够有效填补目前高温段热防护材料的空缺,因此已经成为C/C复合材料基体掺杂改性的重要选择,在航天飞行器防热领域极具应用潜力。本文针对C/C-SiC-ZrC复合材料的发展潜力和应用空间,从制备工艺、结构特征以及性能特点三个方面综述了C/C-SiC-ZrC复合材料当前的研究进展,分析了制备工艺对复合材料微结构和性能的影响规律,提出了基于工程应用C/C-SiC-ZrC防热材料的发展建议。
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张倩玮
陈意高
崔红
吴小军
关键词:  C/C复合材料  SiC-ZrC复相陶瓷  基体改性    
Abstract: C/C-SiC-ZrC composites have better mechanical properties and ablation resistance than single ceramic phase modified C/C composites. Both of the two modification methods have the same process principle. SiC-ZrC multiphase ceramics have the advantages of high temperature resistance, oxidation resistance in a wide temperature range(1 600—2 500 ℃), and good process adaptability. Therefore SiC-ZrC multiphase ceramics have become an important component of C/C composite matrix doping modification, and have great application potential in the field of spacecraft thermal protection. In order to provide reference for subsequent research, this paper not only summarizes the current research progress of C/C-SiC-ZrC composites from three aspects:preparation process, structural characteristics, and performance characteristics, but also analyzes the influence of the preparation process on the microstructure and properties of the composites, and puts forward the development proposal of C/C-SiC-ZrC thermal protective materials based on engineering applications.
Key words:  C/C composite    SiC-ZrC multiphase ceramic    matrix modification
出版日期:  2024-02-10      发布日期:  2024-02-19
ZTFLH:  TB332  
基金资助: 国家自然科学基金(U1837201)
通讯作者:  *崔红,2000 年获得西北工业大学材料学博士学位,2004 年评聘为西安复合材料研究所研究员。中国电工学会炭-石墨专业委员会副主任委员、《复合材料学报》《固体火箭技术》《宇航材料工艺》编委、享受政府特殊津贴、陕西省有突出贡献专家、航天十佳科技青年、陕西省国防十大杰出青年,获2005—2007 年度航天奖。主要从事航天发动机用炭/炭复合材料技术基础、抗烧蚀炭/炭复合材料研究,在相关领域发文百余篇。cuih1969@163.com   
作者简介:  张倩玮,2020年毕业于武汉理工大学材料科学与工程学院,获得工学学士学位。现为西安航天复合材料研究所硕士研究生,在崔红研究员的指导下进行研究。目前主要研究领域为高温材料及其制造。
引用本文:    
张倩玮, 陈意高, 崔红, 吴小军. SiC-ZrC复相超高温陶瓷改性C/C复合材料的研究进展[J]. 材料导报, 2024, 38(3): 22060154-10.
ZHANG Qianwei, CHEN Yigao, CUI Hong, WU Xiaojun. Research Progress of SiC-ZrC Multiphase Ultra-high Temperature Ceramic Modified C/C Composites. Materials Reports, 2024, 38(3): 22060154-10.
链接本文:  
https://www.mater-rep.com/CN/10.11896/cldb.22060154  或          https://www.mater-rep.com/CN/Y2024/V38/I3/22060154
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