起始温度对Cf/C-陶瓷摩擦副摩擦性能影响
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航天材料及工艺研究所,先进功能复合材料技术重点实验室,北京 100076

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魏金花,1991年出生,博士,高级工程师,研究方向为纤维增强陶瓷基复合材料摩擦学性能评价及复合材料装配工艺技术,E-mail: 15222527210@163.com

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TH117

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Effect of Initial Temperature on the Tribological Property of Cf/C-Ceramics
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Aerospace Research Institute of Materials & Processing Technology, Science and Technology on Advanced Functional Composites Laboratory, Beijing 100076

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    摘要:

    目前,针对Cf/C-ZrO2和Cf/C-Si3N4组成的摩擦副的摩擦性能研究较少,尤其是温度对其摩擦性能的影响,因此,本文进行了起始温度对这两种摩擦副摩擦性能的研究,开展了Cf/C复合材料分别与氧化锆(ZrO2)和氮化硅(Si3N4)组成的销盘摩擦副的摩擦试验,研究了摩擦因数、磨损量、摩擦界面在200~700℃起始温度条件下的变化趋势。结果表明,低于400℃,Cf/C-ZrO2的平均摩擦因数小于Cf/C-Si3N4,两种摩擦副的磨损形式为磨粒磨损和黏着磨损的混合磨损;高于400℃,Cf/C-ZrO2的平均摩擦因数大于Cf/C- Si3N4,磨损形式转变为磨粒磨损和氧化磨损的混合磨损。在各个起始温度下ZrO2盘的磨损率均小于Si3N4;随着起始温度的升高,因Cf/C销的氧化磨损加剧,因此磨损率也逐渐增大。当起始温度高于800℃,Cf/C复合材料无法保持稳定的宏观编织结构,受热氧化,发生破坏。

    Abstract:

    Currently, there is limited research on the tribological properties of frictional pairs composed of Cf/C-ZrO₂ and Cf/C-Si₃N₄, particularly regarding the influence of temperature on their friction behavior. Therefore,the effect of initial temperature on the tribological performance of these two pairs were investigated in this work. Friction tests were conducted using pin-on-disc configurations where Cf/C composites were paired with zirconia (ZrO₂) and silicon nitride (Si₃N₄),respectively. The variations in friction coefficient, wear loss, and friction interface morphology under initial temperatures ranging from 200℃ to 700℃ were systematically analyzed.The results indicate that below 400℃, the average friction coefficient of the Cf/C-ZrO₂ pair is lower than that of the Cf/C-Si₃N₄ pair, with both pairs exhibiting mixed wear mechanisms dominated by abrasive wear and adhesive wear. Above 400℃, the average friction coefficient of the Cf/C-ZrO₂ pair surpasses that of the Cf/C-Si₃N₄ pair, and the wear mechanism transitions to a combination of abrasive wear and oxidative wear. Under all tested temperatures, the wear rate of the ZrO₂ disc is consistently lower than that of the Si₃N₄ disc. As the initial temperature increases, the oxidative wear of the Cf/C pin intensifies, leading to a gradual rise in wear rate. When the initial temperature exceeds 800℃, the Cf/C composite fails to maintain its stable macroscopic woven structure, undergoing thermal oxidation and structural degradation.

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引用本文

魏金花,胡志远,康鹏飞,王凯,李军平.起始温度对Cf/C-陶瓷摩擦副摩擦性能影响[J].宇航材料工艺,2025,55(2):78-85.

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  • 收稿日期:2023-02-20
  • 最后修改日期:2023-06-12
  • 录用日期:2023-06-13
  • 在线发布日期: 2025-05-12
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《宇航材料工艺》2025年青年编委招募启事

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