摘要
制备了一种新型的防热隔热一体化材料-碳-高硅氧纤维增强 C-SiC 复合材料,沿厚度方向从抗烧蚀层渐次过渡到隔热层,其组成依次是致密 C/C-SiC,致密 C/C,多孔 C/C,通过界面处过渡到变密度多孔 HSF/C.这种材料既具有抗烧蚀性能又具有隔热性能.C/C-SiC 复合材料的烧蚀表面平滑,线烧蚀率只有0.028mm/s.烧蚀性能的提高得益于 SiC 颗粒原位氧化生成 SiO_2黏附在碳材料表面,对氧气有一定的阻挡遮蔽作用.密度为0.80 g/cm^3的 HSF/C 材料,热导率为0.59 W/mK.在碳纤维与高硅氧织物的界面处,针刺纤维与热解碳的结合良好,密度为1.69g/cm^3的 C-HSF/C 复合材料界面处的剪切强度达到16.7MPa.
A novel composite, carbon fibers and high-silica fibers reinforced carbon matrix and silicon carbide matrix (C-HSF/C-SiC), was prepared. The material consisted of four layers, which were densified C/C-SiC, densified C/C, porous C/C and porous HSF/C. The two formers act as the heat-protective layers while the two latter the heat-insulated layers. The composite possesses a smooth ablation surface after an ablation test performed on an engine torch and the erosion rate is only 0.028 mm/s. The better anti-ablation properties should attribute to SiO2 formed by SiC oxidation holding up the flame further attack. The thermal conductivity of HSF/C with the density of 0.80 g/cm^3 is 0.59 W/mK, which has a good thermal insulation action. The needling fiber bundles and pyrocarbon have integrated tightly carbon fiber fabric and HSF fabric. The interfacial shear strength between the two fabics is 16.7 MPa.
出处
《材料研究学报》
EI
CAS
CSCD
北大核心
2006年第2期148-152,共5页
Chinese Journal of Materials Research
基金
国家自然科学基金 No.90205017资助项目~~
关键词
复合材料
化学气相渗
防热
隔热
composite, chemical vapor infiltration(CVI), thermal protection, heat insulation