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热解碳基C/C复合材料纤维--基体界面的精细结构
引用本文:石荣,胡赓祥,李贺军,康沫狂. 热解碳基C/C复合材料纤维--基体界面的精细结构[J]. 电子显微学报, 1998, 17(6): 722-726
作者姓名:石荣  胡赓祥  李贺军  康沫狂
作者单位:1. 上海交通大学国家教委高温材料及高温测试开放实验室,上海,200030
2. 西北工业大学材料科学与工程系,西安,710072
摘    要:采用JEM-2010型高分辨透射电镜考察了热解碳基碳/碳复合材料的纤维-基体界面结构.实验发现,由化学气相渗透工艺所获得的热解碳并非仅与碳纤表面进行单一的机械粘合,也不是一个简单平面.其间存在具有感应结构的界面层,它是受碳纤维表面微晶感应而形成的由基本平行于表面且更为细小的微晶所组成的厚约数纳米至数十纳米的过渡层,碳纤维微晶越大,取向性越好,则界面层的厚度也越大,取向性也相应提高.由此可定性解释高模量碳纤维与热解碳粘合效果弱于高强碳纤维.

关 键 词:C/C复合材料  界面  热解碳  透射电子显微术

Interfacial Microstructures of Fiber-Matrix in As-received Carbon/Carbon Composites Prepared by CVI
Shi Rong,Hu Gengxiang,Li Hejun,Kang Mokuang. Interfacial Microstructures of Fiber-Matrix in As-received Carbon/Carbon Composites Prepared by CVI[J]. Journal of Chinese Electron Microscopy Society, 1998, 17(6): 722-726
Authors:Shi Rong  Hu Gengxiang  Li Hejun  Kang Mokuang
Abstract:Interfacial microstructures in as-receivedcarbon/carbon composites prepared by CVI were investigated by means of high resolutiontransmission electron microscope(HREM) JEM-2010.It has been found that the pyrolyticcarbon matrix does not merely bond mechanically with carbon fiber surface,and theinterface is not a simple plane yet.There exists a transitional layer with a thickness ofabout several nanometres to several tenfold nanometres between carbon fibre and carbonmatrix because of the induction of basal planes of crystallites on the surface layer ofthe fibers.The transitional layer with an induction sturcture is composed of finercrystallits that are basically parallel to the carbon fibre surface.The bigger in size andthe more regular of orientation of the crystallites on carbon fibre surface,the thickerthe transitional layer and the better orientations of the crystallites.So this can give aqualtative explanation for why there is different bonding effect between pyrolytic carbonmatrix and different kinds of carbon fibres.
Keywords:carbon/carbon composite interface pyrolytic carbontransmission electron microscopy
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