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作 者:刘红林[1] 金志浩[1] 郝志彪[2] 曾晓梅[2]
机构地区:[1]西安交通大学材料强度国家重点试验室,西安710049 [2]西安航天复合材料研究所,西安710025
出 处:《固体火箭技术》2007年第6期529-533,共5页Journal of Solid Rocket Technology
摘 要:简述了制备炭/炭复合材料的新工艺——化学液相沉积(CLD)的沉积原理。利用工业燃油作为裂解炭前驱体,炭纤维毡作为增强体,通过工艺参数控制得到低成本炭/炭复合材料。CLD工艺所得材料沉积密度1.6 g/cm3,轴向压缩强度92 MPa,等离子烧蚀率0.06 mm/s,与CVD工艺所得材料相近。与常规CVD工艺相比,CLD工艺制备的C/C复合材料在制备时间上缩短了4/5,致密速率快5倍多。所得基体裂解炭为粗糙层与光滑层结构(大部分为粗糙层结构)。基体炭与炭纤维接合界面适中,且呈洋葱状分布,从而材料具有一定韧性。The densification mechanism of chemical liquid deposition (CLD) process was introduced. Taking industrial fuel as the precursor for carbon matrix and carbon fiber felt as the reinforcement, a low-cost C/C composite (C/C) was prepared. The resuits show that the properties of CLD C/C are the same as those of CVD C/C, i.e. the bulk density is up to 1.6 g/cm^3 , the axial compressive strength can be up to 92 MPa, and the plasma ablation rate can be less than 0.06 mm/s. Compared with CVD process, the densification rate of CLD process can be increased about 5 times. Consequently, the deposition period can be shortened about 4/5. CLD carbon matrix includes rough laminar pyrocarbon ( RL Pyc) and smooth laminar pyrocarbon ( SL Pyc) ( mainly RL Pyc). The carbon matrix with an onion structure bonds with carbon fiber moderately, that is to say, the matrix/fiber interface of CLD C/C is better. So it can be predicated that the mechanical properties of CLD C/C can be improved.
分 类 号:TB332[一般工业技术—材料科学与工程]
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