摘要
采用温度脉冲化学气相渗透沉积的方法制备了碳／碳化硅复合材料界面．以六甲基二硅胺烷(Hexam- ethyldisilazane,HMDS)为前驱体,以3k,三维四向的石墨化碳纤维编织体为预制体,通过强制流动热力学梯度化学气相渗透沉积的方法(FCVI)制备出密度为1．98g·cm-3的Cf／SiC复合材料．运用透射电子显微镜(TEM)对复合材料的界面微观结构进行了分析．复合材料的平均弯曲强度为458MPa,平均断裂韧性为19．8MPa·m1／2．应用扫描电子显微镜(SEM)对复合材料的断裂形貌进行了分析研究．
A novel method of temperature-pulsing chemical vapor infiltration （T-pulsing CVI） was introduced. And interracial coatings of silicon carbide （SIC） layer and pyrolytic carbon （PyC） layer were processed via the route. 3D carbon fiber preforms were densified by forced-flow thermal-gradient chemical vapor infiltration （FCVI） with the precursor of hexamethyldisilazane （HMDS）. The microstructure of interphases was investigated by transmission electron microscope （TEM）. The configuration of specimens＇ fracture surface was observed by scanning electron microscope （SEM）. Results show that the density of the composites is 1.98g·cm^-3. The thickness of the SiC layer estimated is 20nm, and 50nm for the PyC layer. The average flexural strength of the composites is 458MPa at room temperature, and the average fracture toughness is 19.8MPa·m^1/2.
出处
《无机材料学报》
SCIE
EI
CAS
CSCD
北大核心
2007年第2期305-310,共6页
Journal of Inorganic Materials
关键词
C/SIC复合材料
化学气相渗透
微观结构
断裂形貌
ceramic-matrix composites （CMCs）
chemical vapor infiltration （CVI）
microstructure
fracture surface morphology
