SiC基体结构及其对C/SiC复合材料性能的影响研究
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1.航天材料及工艺研究所,北京 100076;2.北京临近空间飞行器系统工程研究所,北京 100076

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TB332

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Study on the Structure of SiC Matrix and Its Effect on the Properties of C/SiC Composites
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1.Aerospace Research Institute of Material & Processing Teachnology,Beijing 100076;2.Beijing Institute of Near Space Vehicle’s Systems Engineering, Beijing 100076

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    摘要:

    采用聚碳硅烷作为前驱体,在800、1 000、1 200 ℃下烧结得到SiC基体,研究了温度对SiC基体密度、结晶程度的影响。结果表明基体随着温度的提高,基体密度提高,结晶程度逐渐提高,Si含量比例升高。在800 ℃时,基体密度为2.30 g/cm3,所得基体结构接近无定型态,在1 000和1 200 ℃下的密度分别为2.50和2.56 g/cm3,晶粒尺寸分别为2.6和4.1 nm。再以聚碳硅烷为前驱体,以碳纤维织物为增强体,采用PIP工艺制备C/SiC复合材料,热解最高温度同样为800、1 000、1 200 ℃,得到三组C/SiC复合材料,对复合材料进行了力学性能测试和断口微观结构观察,分析了基体结构对复合材料力学性能的影响。研究结果表明,在一定范围内提高热解温度,有利于改善基体特性和提高复合材料的致密化效率,从而使复合材料的力学性能有所提升,特别是弯曲、层间剪切和压缩性能提高作用明显。

    Abstract:

    SiC matrix was obtained by sintering polycarbonsilane at 800, 1 000, 1 200 ℃, and the effect of temperature on the density and crystallization degree of SiC was studied. With the increase of temperature, the crystallization degree, the density of the matrix and the proportion of Si increases. At 800 ℃, the density of the matrix is 2.30 g/cm3, and the matrix structure is close to the amorphous state . At 1 000 ℃ and 1 200 ℃, the densities of the matrix are 2.50 and 2.56 g/cm3 , and the grain sizes are 2.6 and 4.1 nm, respectively. C/SiC composites are prepared by PIP process with polycarbosilane as precursor and carbon fiber fabric as reinforcement, the maximum pyrolysis temperatures in the whole pyrolysis process are also 800 , 1 000 and 1 200 ℃. The effect of matrix structure on the mechanical behavior of the composites is studied by mechanical properties test and microstructures observation. The results show that increasing the pyrolysis temperature in a certain range is beneficial to improve the properties of the matrix and the matrix’s densification efficiency ,which make the mechanical performance of the material improved, and especially has obvious effect on improving the bending strength , interlaminar shear strength and compression strength of C/SiC composites.

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房金铭,李钰梅,龚晓冬,张家华,李军平. SiC基体结构及其对C/SiC复合材料性能的影响研究[J].宇航材料工艺,2022,52(4):49-53.

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  • 收稿日期:2021-01-16
  • 最后修改日期:2022-07-05
  • 录用日期:2021-05-06
  • 在线发布日期: 2022-09-02
  • 出版日期:
第十一届航天复合材料成形与加工工艺技术中心交流会 征文通知

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