C/SiC复合材料在典型模拟环境下高温拉伸性能研究
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航天材料及工艺研究所,北京 100076

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TB33

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Study on High Temperature Tensile Properties of C/SiC Composites Under Typical Simulated Environments
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Aerospace Research Institute of Materials & Processing Technology,Beijing 100076

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    摘要:

    以先驱体浸渍裂解(PIP)工艺制备的C/SiC复合材料为对象,研究了C/SiC复合材料在典型模拟环境下的高温拉伸性能,首次获得了约3 000 s时间不同变状态条件下材料的高温拉伸性能数据,探讨了不同条件下C/SiC复合材料高温承载行为及其变化规律。研究结果表明,C/SiC复合材料经历约3 000 s复杂阶梯热环境后拉伸强度仍保持60%左右;经历大温度梯度热震后,C/SiC复合材料的高温拉伸性能保持率反而提高,最高保持率超过80%;热震温差越大,热震后保温时间越长,对材料的高温拉伸性能保持和提高越有利。

    Abstract:

    The high temperature tensile properties under the typical simulated environment of C/SiC composites prepared via polymer infiltration and pyrolysis (PIP) method were investigated.The high temperature tensile property data of the C/SiC composites under different variable conditions (about 3 000 s) were obtained.The high temperature bearing behavior and its variation law of the C/SiC composites under different variable conditions were discussed. The results show that the tensile strength of C/SiC composite material can still maintain about 60% after about 3 000 s complex step heating. The high temperature tensile property retention of C/SiC composite material increases after thermal shocks with large temperature difference. The highest temperature tensile property retention exceeds 80%. The larger thermal shock temperature variation and longer holding time after thermal shock, which is more beneficial to maintian and improve the high temperature tensile properties of C/SiC composites.

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唐君,袁泽帅,黄汝超,袁建宇,徐林,李军平,卢鹉. C/SiC复合材料在典型模拟环境下高温拉伸性能研究[J].宇航材料工艺,2023,53(2):85-90.

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历史
  • 收稿日期:2022-12-11
  • 最后修改日期:2023-03-29
  • 录用日期:2023-02-24
  • 在线发布日期: 2023-04-26
  • 出版日期: 2023-04-30
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