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预制体结构对C/C喷管出口锥材料力学性能的影响
引用本文:张晓虎,李贺军,郝志彪,崔红,嵇阿琳.预制体结构对C/C喷管出口锥材料力学性能的影响[J].固体火箭技术,2006,29(5):380-383.
作者姓名:张晓虎  李贺军  郝志彪  崔红  嵇阿琳
作者单位:西北工业大学材料学院,西安,710072;西安航天复合材料研究所,西安,710025
基金项目:国家高技术研究发展计划(863计划) , 国家自然科学基金
摘    要:设计了3种用于制备喷管用C/C出口锥材料的炭纤维增强预制体,即炭布铺层骨架(P型预制体)、炭布叠层原位针刺骨架(N型预制体)、炭纤维整体编织骨架(B型预制体),并对比研究了预制体结构对C/C出口锥材料力学性能的影响。结果表明,对同密度水平的C/C出口锥,用P型预制体制备的C/C材料的层剪强度最低,N型预制体制备的材料的层剪强度最高,B型预制体制备的材料的层剪强度居中。3种预制体制备的C/C材料的高温弯曲性能差别不大,N型预制体结构更适合于C/C出口锥材料的制备成型。

关 键 词:C/C复合材料  预制体结构  喷管出口锥  力学性能
文章编号:1006-2793(2006)05-0380-04
收稿时间:2005-08-08
修稿时间:2006-04-06

Effects of preform structure on mechanical properties of carbon-carbon composite for nozzle exit cone
ZHANG Xiao-hu,LI He-jun,HAO Zhi-biao,CUI Hong,JI A-lin.Effects of preform structure on mechanical properties of carbon-carbon composite for nozzle exit cone[J].Journal of Solid Rocket Technology,2006,29(5):380-383.
Authors:ZHANG Xiao-hu  LI He-jun  HAO Zhi-biao  CUI Hong  JI A-lin
Abstract:Three types of carbon fiber reinforced preforms such as carbon cloth ply preform(P preform),needled caborn cloth preform(N preform)and braided carbon fiber preform(B preform)were designed to prepare carbon-carbon exit cone of nozzle,and the effects of the preform structures on the mechanical properties of carbon-carbon composite were compared and investigated.The results show that for same density C/C exit cone composite,interlaminar shear strength(ILSS) of C/C composite prepared by P preform has the lowest value,but ILSS of C/C composite prepared by N preform reaches the highest value.The high-temperature bending properties of C/C composite prepared by three types of preforms are almost the same,and N preform structure is more appropriate for preparation and forming of C/C exit cone composite.
Keywords:carbon-carbon composites  preform structure  nozzle exit cone  mechanical properties
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