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炭基体结构状态对C/C复合材料抗烧蚀性能的影响 总被引:12,自引:2,他引:12
碳基体在C/C复合材料的组成中占有很大的比重,因此炭基体不同的结构状态往往对C/C复合材料的各项性能有显著的影响。本文利用不同的原料和加工工艺制备出了三种具有不同炭基体的C/C复合材料,这三种碳基体分别是热解炭,沥青炭以及解热炭-树脂炭混合炭基体。对这三种材料多项性能的测试结果表明,炭基体的结构状态如石墨化度,炭片层结构的取向度的不同对C/C复合材料的各项性能均有显著的影响;基本趋势是C/C材料的石墨化度越高,材料的导电性能,导热性能以及抗烧蚀性能越好,压缩强度越低。三种炭基体中沥青炭基体沿纤维轴向的取向度最低,其抗烧蚀性能最差。 相似文献
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炭布叠层为预制体,采用等温CVI工艺制备出炭/炭(C/C)复合材料。通过调节丙烯与氢气的比例得到热解炭结构分别为粗糙层(RL),光滑层(SL),各向同性(ISO)的三种C/C复合材料,研究了热解炭组织结构对C/C复合材料热导率的影响,讨论了C/C复合材料的导热机理。结果表明:RL织构C/C复合材料的热导率无论是在平行方向还是在垂直方向上都明显高于SL和ISO织构C/C复合材料,在两个方向上,RL织构C/C复合材料的最大热导率比SL织构C/C复合材料分别大41.0%和31.7%,是ISO织构C/C复合材料的2倍多,且3种C/C复合材料的热导率随温度的升高呈现不同的变化趋势。 相似文献
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以T300炭纤维无纬布、网胎为原材料,层叠针刺成型炭纤维预制体,并采用化学气相沉积工艺对预制体进行致密,制成密度为1.55 g/cm3的针刺C/C复合材料。对针刺C/C复合材料的微观结构进行了观察分析,并对材料力学性能进行了测试。结果表明:化学气相沉积致密的针刺C/C复合材料呈现出以层间大量垂直纤维束为节点的类钉板状网状结构,这种特殊结构使材料层间结合更好,材料整个结构更加紧密;针刺C/C复合材料内部纤维被沉积形成的热解炭所包裹,热解炭的织构类型为光滑层(SL)和粗糙层(RL)并存;针刺C/C复合材料的各项力学性能均达到了较高水平,并且高温力学性能比常温力学性能有了很大幅度的提高。 相似文献
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以2D叠层炭布为增强体的炭/炭(C/C)复合材料作为多晶硅炉用热场盖板,对其在硅液/硅蒸汽共同作用下的硅化腐蚀失效机理进行了研究。通过多功能密度测试仪、扫描电子显微镜(SEM)和X射线衍射仪(XRD)分析了硅化作用对C/C复合材料致密度、微观结构及物相组成的影响,并对侵蚀后的C/C复合材料失效机理进行了分析。结果表明:硅化侵蚀后的C/C复合材料致密度高,存在大量的Si元素,生成了大量的β-SiC,且微观缺陷较多,层间开裂严重,呈现脆性断裂模式。理论分析发现,高温下单位摩尔质量的热解炭和单位摩尔质量的硅发生反应生成单位摩尔质量的SiC后,总体积膨胀约为单位摩尔热解炭体积的6.3倍,不同物相间的热失配导致热应力集中,引起C/C复合材料变形开裂失效,裂纹产生的扩散通道加剧了硅液/硅蒸汽对C/C复合材料的硅化侵蚀作用。 相似文献
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化学气相渗(CVI)C/SiC复合材料性能控制 总被引:1,自引:0,他引:1
本研究用化学气相渗技术制备了四种C/SiC复合材料:在CH3SiCl3+H2(普通)+Ar(高纯)系统中制各了两种材料:材料A为1K炭布层叠无热解炭界面层,材料B为1K炭布层叠有热解炭界面层;在CH3SiCl3+H2(高纯)+Ar(高纯)系统中制备了另两种材料:材料C和材料D分别为1K、T300炭布层叠有热解炭界面层.分别对其中每两种材料进行了相互比较,研究了骨架纤维、界面层及基体对整个复合材料性能的影响;通过控制上述三方面因素可以对C/SiC复合材料的总体结构进行设计从而控制其材料最终性能。 相似文献
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C/C多孔体对C/C-SiC复合材料微观结构和弯曲性能的影响 总被引:2,自引:0,他引:2
以4种纤维含量相同(32%,体积分数,下同),用化学气相渗透(chemical vapor infiltration,CVI)法制备了4种密度的碳纤维增强碳(carbon fiber reinforced carbon,C/C)多孔体,基体炭含量约20%~50%.利用液相渗硅法(liquid silicon infiltration,LSI)制备了C/C-SiC复合材料,研究了C/C多孔体对所制备的C/C-SiC复合材料微观结构和弯曲性能的影响.结果表明:不同密度的C/C多孔体反应渗硅后,复合材料的物相组成均为SiC,C及单质Si;随着C/C多孔体中基体炭含量的增加,C/C-SiC复合材料中SiC含量逐渐减少而热解炭含量逐渐增加.C/C-SiC复合材料弯曲强度随着材料中残留热解炭含量增加而逐渐增加,热解炭含量为约42%的C/C多孔体所制备的C/C-SiC复合材料的弯曲强度最大,达到320 MPa. 相似文献
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Densification rate and mechanical properties of carbon/carbon composites with layer-designed preform
In this work, carbon fiber needle-punching preforms were designed into two structure according to the density change along the thickness direction. One structure is designed to two layers with low-density layer and high-density layer, and the other is to three layers with low-density exterior layer and high-density interior layer. Then the effect of the preform with different structure on the densification rate and compressive properties of C/C composites was investigated. The results show that both two designed preforms can effectively avoid surface blocking, and lead to the faster densification rate of C/C composites during the chemical vapor infiltration processes. These results are attributable to the change of pore size distribution and pyrocarbon thickness, which was caused by fiber architecture designs. Meanwhile, these structural changes can improve the compressive strength of C/C composites, especially for the three-layer preforms. When the density of preforms is 0.45?g/cm3, C/C composites with three-layer preform has the highest compressive strength. The damage of most C/C composites with two and three-layer preforms is caused by shear or delamination failure, while that of C/C composites with common preforms usually caused by matrix collapse. Cracks in C/C composites with two and three-layer preforms always happened on the low-density layer, and consequently ceased or changed propagation direction in the interface between two layers. 相似文献
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The catalytic effect of boric acid on the graphitization and surface structure of polyacrylonitrile-based carbon fibers was investigated by dipping fibers in boric acid before heating at 2500 °C. The thermal conductivity of carbon/carbon composites produced from the modified carbon performs by chemical vapor infiltration was also studied. The results show that the treatment by boric acid has a catalytic-graphitization effect on the fibers that increases the crystallinity and changes the surface state of carbon fibers during high temperature treatment. The modified carbon fibers induce the deposition of pyrocarbon with high crystallinity and an obvious transition interface between the carbon fiber and pyrocarbon during chemical vapor infiltration. By changing the microscopic structure of the carbon fibers, the interface bonding between fibers and pyrocarbon is improved and the microstructure of pyrocarbon is regulated. The thermal conductivity of the carbon/carbon composites is therefore improved, especially that in the direction perpendicular to fiber axis. 相似文献
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B4C/C复合材料高温氧化过程中的结构变化模型的研究 总被引:5,自引:0,他引:5
在用混合磨碎法制备B4C/C复合材料的基础上,考察了不同条件对复合材料氧化失重速率的影响,然后讨论了上述各因素对复合材料抗氧化性能的影响机制,并对复合材料结构与其自愈合功能的性进行了分析,在此基础上建立了复合材料高温氧化过程的结构变化模型。 相似文献
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《Carbon》2013
Silicon carbide nanofibers (SiCNFs) used as the second reinforcements of carbon/carbon composites were grown radially on the carbon fiber surface. The microstructure of SiCNFs and their effects on the microstructure and flexural properties of C/C composites were investigated. Results show that there are many defects such as twin crystals and stacking faults in SiCNFs which were grown by catalytic chemical vapor deposition. During the same process, the skin region of carbon fiber has changed. Several SiC layers are formed and the arrangement of the graphite layers around SiC layers is more orderly. In the next chemical vapor infiltration, due to the induction of SiCNFs, the middle textural pyrocarbon were formed firstly and then is the high textural pyrocarbon. The existence of SiCNFs also contributes to the three-phase interface between pyrocarbon, SiCNFs and carbon fibers, resulting in a good bond between carbon fiber and matrix. Those structural changes lead the better flexural properties of SiCNF–C/C composites compared with C/C composites. 相似文献