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合成了硼吖嗪和全氢聚硅氮烷的混杂先驱体并对其结构进行了表征;以混杂先驱体和3D炭纤维编制体为原料,采用先驱体浸渍-裂解(PIP)工艺制得了炭纤维增强氮化物基体的复合材料,并对复合材料基体的抗氧化性以及抗烧蚀性能进行了研究.结果表明:混杂先驱体中含有B-N、B-H、Si-N、Si-H、N-H等结构,无其他杂质;基体材料在空气中具有优良的抗氧化性能,温度升至1000℃时仍未发生明显的质量变化,明显优于C/C复合材料;四个PIP工艺循环所制得的复合材料烧蚀表面平整,氮化物基体比增强炭纤维具有更好的耐烧蚀性能.

A hybrid precursor containing borazine and perhydropolysilazane was synthesized and characterized,and used to produce three-dimensional carbon fiber reinforced nitride matrix composites (3D C_f /Nitrides) through vacuum infiltration of the precursor followed by pyrolysis under inert atmosphere.The oxidation resistance and ablation behavior of the C_f/Nitrides were studied.Results showed that there were several bonds such as B-N,B-H,Si-N,Si-H and N-H in the hybrid precursor and the as-formed matrix had a good oxidation resistance.The matrix weight did not change distinctly when the temperature was increased from room temperature to 1 000 ℃.The surface of the ablated composites was flat and the nitride matrix had a much better ablation resistance than did the carbon fibers.

参考文献

[1] 李贺军.炭/炭复合材料[J].新型炭材料,2001(02):79-80.
[2] 罗瑞盈.航空刹车及发动机用炭/炭复合材料的研究应用现状[J].炭素技术,2001(04):27-29.
[3] 蒋建纯,黄伯云,熊翔.炭/炭复合材料飞机刹车盘表面加工质量对其磨合性能的影响[J].新型炭材料,2002(02):35-40.
[4] A. Samah;D. Paulmier;M. El Mansori .Damage of carbon-carbon composite surfaces under high pressure and shear strain[J].Surface & Coatings Technology,1999(0):636-640.
[5] Y.-J. LEE;H. J. JOO .Investigation on ablation behavior of CFRC composites prepared at different pressure[J].Composites, Part A. Applied science and manufacturing,2004(11):1285-1290.
[6] 罗瑞盈.碳/碳复合材料氧化及其防护性能研究[J].材料工程,2000(08):7-10.
[7] Manocha LM.;Patel KB.;Glogar P.;Manocha S. .Oxidation behaviour of carbon/carbon composites impregnated with silica and silicon oxycarbide[J].Carbon: An International Journal Sponsored by the American Carbon Society,2000(10):1481-1491.
[8] Lee YJ;Joo HJ .Ablation characteristics of carbon fiber reinforced carbon (CFRC) composites in the presence of silicon carbide (SiC) coating[J].Surface & Coatings Technology,2004(0):286-289.
[9] 黄剑锋,李贺军,熊信柏,曾燮榕,李克智,付业伟,黄敏.炭/炭复合材料高温抗氧化涂层的研究进展[J].新型炭材料,2005(04):373-379.
[10] S. Seghi;B. Fabio;J. Economy .Carbon/carbon-boron nitride composites with improved wear resistance compared to carbon/carbon[J].Carbon: An International Journal Sponsored by the American Carbon Society,2004(15):3043-3048.
[11] Kim D P;Economy J.Fabrication of oxidation-resistant carbon fiber/boron nitride matrix composites[J].Chemistry of Materials,1993(05):1216-1220.
[12] Kim DP.;Economy J.;Cofer CG. .FABRICATION AND PROPERTIES OF CERAMIC COMPOSITES WITH A BORON NITRIDE MATRIX[J].Journal of the American Ceramic Society,1995(6):1546-1552.
[13] Cofer C G;Saak A W;Economy J.Carbon/boron nitride composites:an alternativeto carbon/carbon[J].Ceramic Engineering and Science Proceedings,1995(16):663-671.
[14] Steven Seghi;James Lee;James Economy .High density carbon fiber/boron nitride matrix composites: Fabrication of composites with exceptional wear resistance[J].Carbon: An International Journal Sponsored by the American Carbon Society,2005(10):2035-2043.
[15] Hough W V;Guibert C R;Hefferan G T .Method for the synthesis of borazine[P].US Patent:4150097,1979.
[16] Isoda T;Kaya H;Nishii H.Perhydropolysilazane precursors to silicon nitride ceramics[J].Journal of Inorganic and Organometallic Polymers,1992(02):151-160.
[17] Prelas M A;Benedictus A;Lin L S.Diamond based composites and related materials[M].Dordrecht,The Netherlands.Kluwer Academic Publishers,1997
[18] 顾立德.氮化硼陶瓷(GU li-de.Boron Nitride Ceramics[M].Beijing:China Architecture & Buiding Press,1982.)[M].北京:中国建筑工业出版社,1982
[19] 董文麟.氮化硅陶瓷(DONG Wen-lin.Silicon Nitride Ceramics[M].Beijing:China Architecture & Buiding Press,1982.)[M].北京:中国建筑工业出版社,1987
[20] Economy J;Kim D P .Borazine oligomers and composite materials including boron nitride and methods of making the same[P].U S Patent:5399377,1995.
[21] 张巍,张博明,孟松鹤,韩杰才.细编穿刺碳/碳复合材料等离子火炬高温烧蚀性能研究[J].材料工程,2003(05):23-25.
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