摘要
以碳纤维针刺毡为预制体,采用CVI法或结合液相法制备了热解碳、树脂碳和沥青碳基质的准三维C/C复合材料,并研究了这些材料的弯曲性能及其断裂机理。研究表明:对于热解碳基质,SL基质碳的弯曲强度明显高于RL和SL+RL两种基质碳;弯曲强度随密度增高而增大;致密度越高,基体支撑越强,同时微裂纹和孔隙度越低,弯曲性能越好。
Using needled-carbon fiber felts as perform,quasi-3D C/C composites with pyrolytic carbon(PyC),or/and resin carbon,pitch carbon as matrix,respectively,were fabricated by chemical vapor infiltration method or/and liquid method.In the present paper,the bending property and fracture mechanism of these composites were investigated.The results showed that,the bending strength of the C/C composites with smooth laminar(SL) structural PyC matrix is obviously higher than those with rough laminar(RL) or SL+RL PyC mat...
出处
《航空材料学报》
EI
CAS
CSCD
2006年第4期88-91,共4页
Journal of Aeronautical Materials
基金
国家重点工业试验性项目(计高技〔1998〕1817)
关键词
C/C复合材料
热解碳
弯曲性能
破坏机理
C/C composites
pyrolytic carbon
bending property
fracture mechanism