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材料研究学报  2010, Vol. 24 Issue (5): 471-477    
  研究论文 本期目录 | 过刊浏览 |
炭/炭复合材料摩擦膜的显微结构研究
王禹1,雷宝灵2,贺连龙1,易茂中2
1.中国科学院金属研究所 沈阳 110016
2.中南大学粉末冶金重点实验室 长沙 410083
Study on the Microstructure of C/C Composite Brakes Worn Surface
WANG Yu1, LEI Baoling2, HE Lianlong1, YI Maozhong2
1.Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016
2.State Key Laboratory for Powder Metallurgy, Central South University, Changsha 410083
引用本文:

王禹 雷宝灵 贺连龙 易茂中. 炭/炭复合材料摩擦膜的显微结构研究[J]. 材料研究学报, 2010, 24(5): 471-477.
, , , . Study on the Microstructure of C/C Composite Brakes Worn Surface[J]. Chin J Mater Res, 2010, 24(5): 471-477.

全文: PDF(1078 KB)  
摘要: 用扫描电子显微镜(SEM)和透射电子显微镜(TEM)分析CVD增密和2300℃热处理炭/炭复合材料刹车片在模拟飞机正常刹车状况下的摩擦表面形貌和显微结构, 研究了摩擦膜结构对摩擦磨损性能的影响。结果表明: 在模拟飞机正常着陆的试验中, 在炭/炭复合材料的摩擦表面形成一层低织构热解炭的摩擦膜, 片层厚度约为1 μm。  
关键词 复合材料  炭/炭复合材料  摩擦磨损性能  摩擦膜  磨屑    
Abstract:The morphology and microstructure of the worn surface of carbon-carbon (C/C) composites, which were fabricated by CVD process and finally heat treated after 2300℃, were studied using scanning electron microscopy and transmission electron microscope. Most pyrolytic carbon around the fiber is high-textured pyrolytic, and there is a 1 μm thick low-textured pyrolytic intergrade layer between the fiber and the high-textured pyrolytic. The wear tests were simulating the normal landing of aircraft braking. The results showed that a compacted low-textured pyrolytic carbon friction film which is about 1 μm thick covered the worn surface after the wear tests.
Key wordscomposites    carbon-carbon composites(C/C)     friction and wear properties     friction film     wear debris
收稿日期: 2010-05-19     
ZTFLH: 

TG113

 
基金资助:

国家重点基础研究发展计划2006CB600905资助项目。

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