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介绍了空间氧化环境和低温环境对C/SiC复合材料性能的影响.研究表明:空间原子氧环境对C/C-SiC材料中的C相剥蚀严重;原子氧氧化对C/SiC复合材料的力学性能影响较小.原子氧与分子氧的叠加氧化对C/SiC复合材料的性能影响较大.在空间低温条件下,C/SiC复合材料的拉伸强度会先降低,然后又逐渐恢复;该材料破坏模式与其高温条件下的破坏模式相同.同时提出了当前研究中存在的问题,并展望了未来的研究方向.

参考文献

[1] 张立同,成来飞.连续纤维增韧陶瓷基复合材料可持续发展战略探讨[J].复合材料学报,2007(02):1-6.
[2] 鲁芹,姜贵庆,罗晓光,胡龙飞.X-37B空天飞行器轻质非烧蚀热防护新技术[J].现代防御技术,2012(01):16-20.
[3] 杨亚政,杨嘉陵,方岱宁.高超声速飞行器热防护材料与结构的研究进展[J].应用数学和力学,2008(01):47-56.
[4] 韩媛媛,张宇民,韩杰才.碳化硅反射镜技术的研究现状[J].材料导报,2005(04):5-8.
[5] Kaneda H;Nakagawa T;Onaka T;Enya K;Makiuti S;Takaki J;Haruna M;Kume M;Ozaki T .Cryogenic optical measurements of 12-segment-bonded carbon-fiber-reinforced silicon carbide composite mirror with support mechanism[J].Applied optics,2008(8):1122-1128.
[6] 蔡风震;田安平.空天战场与中国空军[M].北京:解放军出版社,2004:337.
[7] 朱光武,李保权.空间环境对航天器的影响及其对策研究[J].上海航天,2002(04):1-7.
[8] 徐宏强,吕川.空间环境对空间系统维修性设计的影响[J].上海航天,2003(05):38-41.
[9] 许滨;武占成;郝永锋.航天器在轨空间环境研究[J].河北科技大学学报,2011(z2):9.
[10] 都亨;叶宗海.低轨道航天器空间环境手册[M].北京:国防工业出版社,1996
[11] 黄志澄.空天飞机的防热系统[J].气动实验与测量控制,1992(02):1.
[12] Noor AK.;Paul DB.;Hopkins MA.;Venneri SL. .Structures technology for future aerospace systems[J].Computers & structures,2000(5):507-519.
[13] Hui Mei;Laifei Cheng .Comparison of the mechanical hysteresis of carbon/ceramic- matrix composites with different fiber preforms[J].Carbon: An International Journal Sponsored by the American Carbon Society,2009(4):1034-1042.
[14] Michael C. Halbig;James D. McGuffin-Cawley;Andrew J. Eckel .Oxidation Kinetics and Stress Effects for the Oxidation of Continuous Carbon Fibers within a Microcracked C/SiC Ceramic Matrix Composite[J].Journal of the American Ceramic Society,2008(2):519-526.
[15] Cheng LF.;Zhang LT.;Gao R.;Xu YD. .Effect of glass sealing on the oxidation behavior of three dimensional C/SiC composites in air[J].Carbon: An International Journal Sponsored by the American Carbon Society,2001(8):1127-1133.
[16] Cheng L F;Xu Y D;Zhang L T et al.Effect of carbon interlayer on oxidation behavior of C/SiC composites with a coating from room temperature to 1500 ℃[J].Materials Science and Engineering A:Structural Materials Properties Microstructure and Processing,2001,300(1-2):219.
[17] Laifei Cheng;Yongdong Xu;Litong Zhang;Xingang Luan .Oxidation and defect control of CVD SiC coating on three-dimensional C/SiC composites[J].Carbon: An International Journal Sponsored by the American Carbon Society,2002(12):2229-2234.
[18] Berton B;Bacos M P;Demange D et al.High-temperature oxidation of silicon carbide in simulated atmospheric reentry conditions[J].Journal of Materials Science,1992,27(12):3206.
[19] 殷小玮 .3DC/SiC复合材料的环境氧化行为[D].西北工业大学,2001.
[20] 栾新刚 .3D C/SiC在复杂耦合环境中的损伤机理与寿命预测[D].西北工业大学,2007.
[21] Chidong Liu;Laifei Cheng;Hui Mei .Influence of oxidation on fatigue life of a carbon/silicon carbide composite in water vapor containing environments[J].CERAMICS INTERNATIONAL,2009(4):1397-1402.
[22] 祝成民,郭颜红,张跃峰,高劭伦.材料原子氧掏蚀效应中的相似律研究[J].航天器环境工程,2008(06):546-548.
[23] 王敬宜;于志战;张景钦.低地球轨道中的原子氧、效应及地面模拟[J].真空与低温,1990(03):16.
[24] Dooling D;Finckenor M M.Material selection guidelines to limit atomic oxygen effects on spacecraft surfaces[M].Washington,D.C.:NASA,1999
[25] Banks B A.Low earth orbital atomic oxygen interactions with materials[A].Providence,Rhode Island:American Institute of Aeronautics and Astronautics,2004
[26] Dever J;Miller S;Messer R.Exposure of polymer film thermal control materials on the materials international space station experiment (MISSE):International space station utilization[M].Cape Canaveral,Florida:National Aeronautics and Space Administration,2001
[27] Koji Fujimoto;Tadashi Shioya;Katsuhiko Satoh .Degradation of carbon-based materials due to impact of high-energy atomic oxygen[J].International journal of impact engineering,2003(1):1-11.
[28] Xiaochong Liu;Laifei Cheng;Litong Zhang .Erosion Behavior of C/SiC Composites in Atomic Oxygen[J].International journal of applied ceramic technology,2013(1):168-174.
[29] Liu, X.;Cheng, L.;Zhang, L.;Mei, H.;Fu, Z.;Zhao, D.;Luan, X.;Hong, Z.;Li, Z..The degradation behavior of C/SiC composites in complex environment[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2012:212-217.
[30] de Rooij A.Corrosion in space[A].American Institute of Aeronautics and Astronautics,2010
[31] Xue W;Ma T;Xie Z et al.Research into mechanical properties of reaction-bonded SiC composites at cryogenic temperatures[J].Materials Letters,2011,65(21-22):3348.
[32] Liu, X.;Cheng, L.;Zhang, L.;Dong, N.;Wu, S.;Meng, Z. .Tensile properties and damage evolution in a 3D C/SiC composite at cryogenic temperatures[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2011(25/26):7524-7528.
[33] 张剑寒,张宇民,韩杰才,赫晓东.空间反射镜材料性能的研究[J].材料导报,2006(02):5-9.
[34] K. Enya;N. Yamada;T. Imai;Y. Tange;H. Kaneda;H. Katayama;M. Kotani;K. Maruyama;M. Naitoh;T. Nakagawa;T. Onaka;M. Suganuma;T. Ozaki;M. Kume;M.R. Krodel .High-precision CTE measurement of hybrid C/SiC composite for cryogenic space telescopes[J].Cryogenics,2012(1):86-89.
[35] Ozaki T;Kume M;Oshima T et al.Mechanical and thermal performance of C/SiC composites for SPICA mirror[J].Optical Fabrication Metrology and Material Advancements for Telescopes Proceedings of the SPIE,2004,5494:366.
[36] 张立同.科学基金--我创新路上的伴侣[J].中国科学基金,2006(02):126-127.
[37] Katoh, Y.;Ozawa, K.;Hinoki, T.;Choi, Y.;Snead, L.L.;Hasegawa, A. .Mechanical properties of advanced SiC fiber composites irradiated at very high temperatures[J].Journal of Nuclear Materials: Materials Aspects of Fission and Fusion,2011(1/3):416-420.
[38] Snead, L.L.;Nozawa, T.;Ferraris, M.;Katoh, Y.;Shinavski, R.;Sawan, M. .Silicon carbide composites as fusion power reactor structural materials[J].Journal of Nuclear Materials: Materials Aspects of Fission and Fusion,2011(1/3):330-339.
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