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热处理温度对针刺C/C复合材料热力学性能的影响(英文)

Effect of high temperature treatment on performances of needling carbon/carbon composite

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【作者】 白侠嵇阿琳崔红程文

【Author】 BAI Xia 1,2,JI A-lin 1,2,CUI Hong 1,2,CHENG Wen 1,2(1.Xi’an Aerospace Composites Research Institute,Xi’an 710025,China;2.National and Local Union Engineering Research Center of High-performance Carbon Fiber Manufacture and Application,Xi’an 710089,China)

【机构】 西安航天复合材料研究所高性能碳纤维制造及应用国家地方联合工程研究中心

【摘要】 对炭布叠层针刺C/C复合材料分别进行了不同温度的高温热处理,研究了热处理温度对C/C复合材料热学、力学和抗热震等性能的影响。结果表明,经过高温热处理,针刺C/C复合材料的导热率升高,线膨胀系数降低,材料的抗热震因子从未处理的42 kW/m提高到70 kW/m以上,表明热处理后材料具有更佳的热稳定性,但材料的弯曲强度随热处理的升高从126 MPa降到70 MPa,且经过2 000℃及更高温度处理后弯曲强度降低幅度较大。

【Abstract】 The effects of heat treatment temperature on the thermal properties,mechanical properties and thermal shock resistance of needling carbon / carbon composites were studied in this paper.The results show that after high-temperature treatment,thermal conductivity of C / C composites increase,while their coefficient of thermal expansion decrease.The thermal stress factor is found to be improved from 42 kW / m to above 70 kW / m in this process.Thus heat treatment is helpful for improving the thermal shock resistance of needling carbon / carbon composites.However,the flexural strength of needling carbon / carbon composites decrease gradually from 126 MPa to 70 MPa with the increasing heat treatment temperature,especially treated at 2 000 ℃ or even higher temperature.

【基金】 Supported by the National Defence Foundational Research of China(C0320110006);General Armament Department Foundational of China(9140A28011012HT43325)
  • 【文献出处】 固体火箭技术 ,Journal of Solid Rocket Technology , 编辑部邮箱 ,2013年01期
  • 【分类号】V250.2
  • 【被引频次】6
  • 【下载频次】164
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