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1)  carbon/silicon composite
炭/硅复合材料
2)  Carbon composites
炭复合材料
1.
Coke particles reinforced pitch-based carbon composites(CRPCCs)with high density and low cost were fabricated under atmospheric environment by an efficient mould pressing and semi-carbonization shaping technologies.
利用模压半炭化成型工艺,在大气环境下制备了焦炭颗粒增强的沥青基炭复合材料,并借助光学显微镜和扫描电镜对其微观组织和断口形貌进行了观察。
3)  carbon composite
复合炭材料
1.
The effects of the weight of natural graphite on the electrochemical properties of carbon composite for the anode of lithium ion cells were studied.
以煤焦油为原料在天然石墨球表面包覆一层中间相炭材料制备出一种复合炭材料。
2.
The electrochemical performances of mesocarbon,natural graphite and carbon composite for the anode of lithium ion cells were comparatively studied,and the effects of heat-treated temperature on the characteristics of carbon graphite were investigated.
以煤焦油为原料在天然石墨球表面包覆一层中间相炭制备复合炭材料,研究中间相炭、天然石墨球和复合炭材料作为锂离子二次电池炭负极材料的电化学性能,并考察不同温度热处理得到的复合炭材料的电化学性能。
4)  C/C composite
炭/炭复合材料
1.
Influence of texture of C/C composites on the shape of magnetoresistance-orientation angles curves;
炭/炭复合材料的结构对磁电阻—位向曲线形状的影响(英文)
2.
Influence of infiltrating Si on friction properties of two dim ension weaving C/C composites;
熔融渗硅对二维编制炭/炭复合材料摩擦特性的影响
3.
Effect of graphitization degree on the mechanical properties of C/C composites;
石墨化度对炭/炭复合材料力学性能的影响
5)  Carbon/Carbon composite
炭/炭复合材料
1.
A study on ablation properties of carbon/carbon composites manufactured by chemical liquid deposition;
化学液相沉积制备的炭/炭复合材料烧蚀性能研究
2.
Simulation of temperature field of carbon/carbon composite during braking;
炭/炭复合材料制动过程中温度场的仿真
3.
Process of preparing new type of heat insulation carbon/carbon composite
新型隔热炭/炭复合材料的制备工艺
6)  C/C composites
炭/炭复合材料
1.
Fast densification Study of C/C composites with multi-coupling fields CVI;
多元耦合场CVI法快速致密化炭/炭复合材料研究
2.
Effect of fiber volume fraction on friction and wear properties of C/C composites;
纤维体积分数对炭/炭复合材料摩擦磨损性能的影响
3.
Study of melting and infiltrating Si for the C/C composites;
炭/炭复合材料熔融渗Si研究
补充资料:氮化硅晶须补强碳化硅陶瓷复合材料
分子式:
CAS号:

性质:以碳化硅陶瓷为基体,以氮化硅晶须为增强体的复合材料。它既保留了碳化硅陶瓷优良的耐高温、抗蠕变、抗氧化、抗化学腐蚀、耐磨等性能,又具有比碳化硅陶瓷更高的强度和韧性,最高使用温度可达1400℃以上。由于氮化硅晶须与碳化硅陶瓷基体具有较好的物理相容性,化学性质相近,界面的结合力较强。该复合材料的烧结温度高,界面控制困难,成本高,主要用于航空、航天领域的高温部件。

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