帮助 关于我们

返回检索结果

C_f/SiC复合材料表面抗氧化涂层研究进展
Research progress in oxidation resistant coatings on C_f/SiC composites

查看参考文献66篇

汤素芳 1 *   杨嘉 2   唐鹏举 1   胡成龙 1  
文摘 C_f/SiC复合材料因其低密度,高比强度,优异的抗热震、抗氧化和抗烧蚀性能以及高温强度保持率,被认为是高速飞行器的重要热防护材料之一。然而,由于碳纤维在500℃以上发生显著氧化导致材料逐渐失效,因此需对其进行有效的氧化防护。抗氧化涂层被认为是实现C_f/SiC复合材料长时氧化防护的有效手段。本文基于热防护系统对C_f/SiC复合材料抗氧化性能的苛刻要求,综述了现有C_f/SiC复合材料表面抗氧化涂层的研究进展,着重对抗氧化涂层制备技术及涂层体系进行了梳理。提升C_f/SiC复合材料抗氧化涂层使用温度(≥1800℃)及结合强度是当前需要重点解决的问题,制备更长服役时间、更高服役温度同时兼具抗氧化、抗水蒸气腐蚀乃至较好隔热性能的多功能涂层是未来发展的重要方向。
其他语种文摘 C_f/SiC composites are considered as one of the most important candidates for aerospace thermal protection systems because of their low density,high specific strength,good thermal shock, oxidation and ablation resistance,and excellent high temperature strength retention.However,C_f/SiC composites are prone to oxidize at a temperature above 500℃due to inevitable fabrication defects. So it is necessary to carry out effective oxidation protection for the composites.Oxidation resistant coating is an efficient technology to realize long-term oxidation protection.Based on harsh requirement of thermal protection systems,the research progress of anti-oxidation coatings for C_f/SiC composites was summarized,mainly focusing on the coating material systems and their preparation technologies. Improving the service temperature(≥1800℃)and bonding strength of the coatings is an important issue to be solved at present.The preparation of multi-functional coating with longer service time and higher service temperature,as well as oxidation resistance,water vapor corrosion resistance and even good heat insulation performance is an important direction for future development.
来源 材料工程 ,2023,51(3):17-28 【核心库】
DOI 10.11868/j.issn.1001-4381.2021.001123
关键词 抗氧化涂层 ; C_f/SiC复合材料 ; 超高温陶瓷 ; 氧化 ; 烧蚀 ; 热防护
地址

1. 中国科学院金属研究所, 沈阳, 110016  

2. 北京动力机械研究所, 北京, 100074

语种 中文
文献类型 综述型
ISSN 1001-4381
学科 航空
基金 国家自然科学基金项目 ;  国家重点研发计划
文献收藏号 CSCD:7445140

参考文献 共 66 共4页

1.  Tobe R J. Hypersonic vehicle thermal protection system model optimization and validation with vibration tests. Aerospace Science and Technology,2013,28(1):208-213 CSCD被引 7    
2.  Behrens B. Technologies for thermal protection systems applied on re-usable launcher. Acta Astronautica,2004,55(3/9):529-536 CSCD被引 22    
3.  关春龙. 可重复使用热防护系统防热结构及材料的研究现状. 宇航材料工艺,2003(6):7-11 CSCD被引 18    
4.  鲁芹. X-37B空天飞行器轻质非烧蚀热防护新技术. 现代防御技术,2012,40(1):16-20 CSCD被引 8    
5.  Bianchi D. Coupled analysis of flow and surface ablation in carbon-carbon rocket nozzles. Journal of Spacecraft & Rockets,2009,46:492-500 CSCD被引 13    
6.  Bianchi D. Thermochemical erosion analysis for graphite/carbon-carbon rocket nozzles. Journal of Propulsion &Power,2011,27:197-205 CSCD被引 8    
7.  Thakre P. Chemical erosion of carbon-carbon/graphite nozzles in solid-propellant rocket motors. Journal of Propulsion &Power,2008,24:822-833 CSCD被引 26    
8.  Gajiwala H M. Hybridized resin matrix approach applied for development of carbon/carbon composites-Ⅰ. Carbon,1998,36:903-912 CSCD被引 13    
9.  Jian K. Effects of pyrolysis processes on the microstructures and mechanical properties of Cf/SiC composites using polycarbosilane. Materials Science and Engineering:A,2005,390:154-158 CSCD被引 20    
10.  Christin F. Design,fabrication,and application of thermostructural composites(TSC)like C/C,C/SiC,and SiC/SiC composites. Advanced Engineering Materials,2002,4:903-912 CSCD被引 44    
11.  Chamberlain A. Oxidation of ZrB_2-SiC ceramics under atmospheric and reentry conditions. Refractories Application Transaction,2005,1:1-8 CSCD被引 1    
12.  Yang X. Study development on the oxidation-resistance coating of C/C composites. Carbon,2006,128:16-21 CSCD被引 2    
13.  Zhu Y. Effect of CVD ZrB_2coating thickness on anti-ablation performance of C/SiC composites. Ceramics International,2018,44:8166-8175 CSCD被引 7    
14.  Zhang J. Long-time ablation behavior of the multilayer alternating CVD-(SiC/HfC)_3coating for carbon/carbon composites. Corrosion Science,2021,189:109586 CSCD被引 4    
15.  Ache H. Chemical vapour deposition of hafnium carbide and characterization of the deposited layers by secondary-neutral mass spectrometry. Thin Solid Films,1994,241(1/2):356-360 CSCD被引 3    
16.  Liu Q. Morphologies and growth mechanisms of zirconium carbide films by chemical vapor deposition. Journal of Coatings Technology and Research,2009,6(2):269-273 CSCD被引 8    
17.  Wang Y. Deposition mechanism for chemical vapor deposition of zirconium carbide coatings. Journal of the American Ceramic Society,2008,91(4):1249-1252 CSCD被引 13    
18.  Liu G. Effect of modulation period on the structure and mechanical properties of nanoscale W/ZrB_2 multilayered coatings. Physics Procedia,2011,18:16-20 CSCD被引 2    
19.  Zou B L. Microstructure,oxidation protection and failure mechanism of Yb_2SiO_5/LaMgAl_(11)O_(19) coating deposited on C/SiC composites by atmospheric plasma spraying. Corrosion Science,2012,62:192-200 CSCD被引 5    
20.  Wang R Q. Low-pressure plasma spraying of ZrB_2-SiC coatings on C/C substrate by adding TaSi_2. Surface &Coatings Technology,2021,420:127332 CSCD被引 3    
引证文献 1

1 陈良财 CVD法制备SiC涂层的工艺影响分析 材料保护,2024,57(11):110-117
CSCD被引 0 次

显示所有1篇文献

论文科学数据集
PlumX Metrics
相关文献

 作者相关
 关键词相关
 参考文献相关

版权所有 ©2008 中国科学院文献情报中心 制作维护:中国科学院文献情报中心
地址:北京中关村北四环西路33号 邮政编码:100190 联系电话:(010)82627496 E-mail:cscd@mail.las.ac.cn 京ICP备05002861号-4 | 京公网安备11010802043238号