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Effects of high-temperature annealing on the microstructure and properties of C/SiC-ZrB_2 composites

机译:高温退火对C / SiC-ZrB_2复合材料组织和性能的影响

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摘要

C/SiC-ZrB_2 composites prepared via precursor infiltration and pyrolysis (PIP) were treated at high temperatures ranging from 1200 ℃ to 1800℃. The mass loss rate of the composites increased with increasing annealing temperature and the flexural properties of the composites increased initially and then decreased reversely. Out of the four samples, the flexural strength and the modulus of the specimen treated at 1400 ℃ are maximal at 216.9 MPa and 35.5 GPa, suggesting the optimal annealing temperature for mechanical properties is 1400 ℃. The fiber microstructure evolution during high-temperature annealing would not cause the decrease of fiber strength, and moderate annealing temperature enhanced the thermal stress whereas weakened the interface bonding, thus boosting the mechanical properties. However, once the annealing temperature exceeded 1600 ℃, element diffusion and carbothermal reduction between ZrO_2 impurity and carbon fibers led to fiber erosion and a strong interface, jeopardizing the mechanical properties of the composites. The mass loss rate and linear recession rate of composites treated at 1800 ℃ are merely 0.0141 g/s and 0.0161 mm/s, respectively.
机译:通过前驱体渗透和热解(PIP)制备的C / SiC-ZrB_2复合材料在1200℃至1800℃的高温下进行处理。复合材料的质量损失率随着退火温度的升高而增加,并且复合材料的挠曲性能开始时先增加,然后相反地降低。在这四个样品中,在1400℃下处理的试样的弯曲强度和模量在216.9 MPa和35.5 GPa时最大,表明机械性能的最佳退火温度为1400℃。高温退火过程中纤维的微观组织演变不会引起纤维强度的降低,适度的退火温度会增加热应力,而削弱界面结合,从而提高机械性能。然而,一旦退火温度超过1600℃,ZrO_2杂质与碳纤维之间的元素扩散和碳热还原作用将导致纤维侵蚀和牢固的界面,从而损害复合材料的机械性能。 1800℃处理的复合材料的质量损失率和线性衰退率分别仅为0.0141 g / s和0.0161 mm / s。

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  • 来源
    《Materials & design》 |2014年第1期|791-796|共6页
  • 作者单位

    Science and Technology on Advanced Ceramic Fibers and Composites Laboratory, National University of Defense Technology, Changsha 410073, Hunan Province, China;

    Science and Technology on Advanced Ceramic Fibers and Composites Laboratory, National University of Defense Technology, Changsha 410073, Hunan Province, China;

    Science and Technology on Advanced Ceramic Fibers and Composites Laboratory, National University of Defense Technology, Changsha 410073, Hunan Province, China;

    Science and Technology on Advanced Ceramic Fibers and Composites Laboratory, National University of Defense Technology, Changsha 410073, Hunan Province, China;

    Science and Technology on Advanced Ceramic Fibers and Composites Laboratory, National University of Defense Technology, Changsha 410073, Hunan Province, China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Ceramic matrix composites; High-temperature annealing; Microstructure; Mechanical property; Ablation property;

    机译:陶瓷基复合材料;高温退火;微观结构机械性能烧蚀性能;

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