不同预制体炭/炭复合材料在髋关节模拟试验机中的磨损颗粒表征(英文)

采用髋关节模拟试验机检测穿刺碳布预制体和碳毡预制体炭/炭复合材料的磨损行为。分离提取产生的磨损颗粒,检测颗粒形貌和尺寸分布并提出颗粒的演化过程。结果表明:炭/炭复合材料磨损颗粒的尺寸分布在亚微米至数十微米之间,颗粒形貌呈现破损纤维状、纤维碎片状、片状和球状。穿刺碳布预制体炭/炭复合材料比碳毡预制体炭/炭复合材料的磨损颗粒尺寸分布范围更广泛,磨损颗粒中的破损碳纤维状和片状形貌较多。热解碳颗粒的演变主要是其表面的规则化过程,而碳纤维颗粒的演变主要与髋关节模拟试验机提供的应力方向有关。     

C／C坯体对RMI C／C—SiC复合材料组织的影响

以PAN基炭纤维（Cf）针刺整体毡为预制体，用化学气相渗透（CVI）、浸渍炭化（IC）方法制备了不同炭纤维增强炭基体的多孔C／C坯体，采用反应熔渗（RMI）法制备C／C—SiC复合材料，研究了渗Si前后坯体的密度和组织结构。结果表明：不同C／C坯体反应溶渗硅后复合材料的物相组成为SiC相、C相及单质Si相；密度低的坯体熔融渗硅后密度增加较多；密度的增加与开口孔隙度并不是单调增加的关系，IC处理的坯体开口孔隙度低，但渗硅后复合材料的密度增加较多；IC坯体中分布分散的树脂C易与熔渗Si反应，CVI坯体中的热解C仅表层与熔渗Si反应，在Cf和SiC之间有热解C存在；坯体密度相同时，IC处理的坯体中SiC量较多，单质Si相含量少且分散较好，而CVI坯体中SiC量较少，单质Si相的量较多；制备方法相同时，高密度的C／C坯体，渗硅后C相较多。     

Preparation and mechanical properties of carbon/carbon composites with high textured pyrolytic carbon matrix

Short carbon fiber felts with an initial porosity of 89.5% were deposited by isobaric, isothermal chemical vapor infiltration using natural gas as carbon source. The bulk density of the deposited carbon/carbon (C/C) composites was 1.89 g/cm³ after depositing for 150 h. The microstructure and mechanical properties of the C/C composites were studied by polarized light microscopy, X-ray diffraction, scanning electron microscopy and three-point bending test. The results reveal that high textured pyrolytic carbon is deposited as the matrix of the composites, whose crystalline thickness and graphitization degree highly increase after heat treatment. A distinct decrease of the flexural strength and modulus accompanied by the increase of the toughness of the C/C composites is found to be correlated with the structural changes in the composites during the heat treatment process.     

添加BN对光滑层热解炭结构的C/C复合材料摩擦性能的影响

通过粉末层铺法向全网胎炭纤维预制体中添加六方氮化硼粉末和化学气相沉积热解炭增密制备C/C-BN复合材料。在MM 1000摩擦试验机上对其摩擦磨损性能进行测试,并对摩擦表面进行光学形貌观察以及对材料的组织结构和磨屑进行SEM形貌观察。结果表明:与C/C复合材料相比,C/C-BN复合材料的线性磨损率降低了40%,质量磨损率降低了70%;摩擦表面中的六方BN在摩擦过程中始终保持稳定,BN的存在使光滑层热解炭结构的C/C复合材料的摩擦因数曲线变得平稳、波动小并且对刹车压力响应迅速,摩擦表面上形成了一层薄的摩擦膜。     

Densification mechanism of chemical vapor infiltration technology for carbon/carbon composites

Carbon/carbon composites were fabricated using pressure-gradient chemical vapor infiltration（CVI） technology with propane （C3H6） as the carbon precursor gas and nitrogen （N2） as the carrier gas. The chemical process of deposition of pyrolytic carbon was deduced by analyzing the component of molecules in gas phase and observing the microstructure of deposition carbon. The results show that the process of deposition starts from the breakdown of C-C single bond of propene （C3H6）, and forms two kinds of active groups in the heterogeneous gas phase reaction. Afterwards, these active groups form many stable bigger molecules and deposit on carbon fiber surface. At the same time, hydrogen atoms of the bigger molecules absorbed on carbon fiber surface are eliminated and the solid pyrolytic carbon matrix is formed in the heterogeneous reaction process.     

预制体对C／C复合材料热膨胀系数的影响

以天然气为前驱气体,整体碳毡和2D针刺碳毡为预制体,采用热悌度化学气相渗积技术制备了两种C／C复合材料,其表观密度均为1．74g／cm^3。借助光学显微镜和扫描电子显微镜观察了热解碳基体的生长特征和微观形貌,采用热膨胀仪测量了两种材料的热膨胀系数（CTE）,研究了由不同预制体增强C／C复合材料的CTE,解释了造成材料不同方向CTE差异的主要原因。结果表明,随着温度升高,材料A和B的CTE是逐渐升高的,且Z向CTE值均大于XY向。当两种材料在Z向的纤维体积分数接近时,随着XY方向纤维体积分数增大,材料在Z向的CTE增大,在XY向的CTE降低,两种材料存XY和Z向的CTE旱如下分布：αB—z〉dAz〉αA—xy〉αBxY-C／C复合材料的CTE主要取决于纤维体积分数和排市、碳基体及材料中的孔隙分布情况,前者起决定作用。     

Numerical simulation on thermal expansion coefficient of 3D braided C/C composites简

To effectively get the thermal expansion coefficient(CTE) of three-dimensional(3D) braided C/C composites and study the variations, a VC?? program with graphical user interfaces was obtained, based on the yarn unit model and numerical analysis. With the limited basic properties of carbon fibers and carbon matrix, CTE of 3D braided C/C composites is obtained at 85 °C. The deviation between the simulated and experimental axial CTE of 3D braided C/C composites is no more than 11 %. The effects of different parameters(including the braiding angle of 3D braided preform, the fiber volume fraction and the porosity of 3D braided C/C composites, and the elastic modulus, Poisson's ratio and CTEs of carbon fibers and carbon matrix) were analyzed with the program. The results show that the axial CTE of C/C composites decreases with the increase of the braiding angle, the fiber volume fraction, and the porosity of 3D braided C/C composites. The transverse elastic modulus of carbon fibers has the greatest effect on the axial CTE among the studied mechanical parameters, followed by the elastic modulus and Poisson's ratio of carbon matrix.     

碳纤维表面生长纳米碳管及其增强的炭/炭复合材料

采用化学气相沉积工艺在碳纤维表面生长了纳米碳管,将此种碳纤维作为增强材料,以中间相沥青为基体炭前驱体采用浸渍炭化工艺制备了炭/炭复合材料.观察了所得复合材料断口的微观形貌,测试了抗弯强度及热物理性能.结果表明,碳纤维表面的纳米碳管可以有效地提高纤维与基体的粘结力,复合材料的抗弯性能提高了50%,而对复合材料的导热性能影响较小.     

Improved properties of carbon fiber paper as electrode for fuel cell by coating pyrocarbon via CVD method

The fabrication of a pyrocarbon coated carbon paper and its application to the gas diffusion lay (GDL) of proton exchange membrane (PEM) fuel cell were described. This carbon paper was fabricated by using conventional carbon paper as the precursor, and coating it with pyrocarbon by pyrolyzing propylene via the chemical vapor deposition (CVD) method. For comparison, conventional carbon paper composites were also prepared by using PAN-based carbon fiber felt as the precursor followed by impregnation with resin, molding and heat-treatment. SEM characterization indicates that pyrocarbon is uniformly deposited on the surface of the fiber in the pyrocarbon coated carbon paper and made the fibers of carbon felt bind more tightly. In contrast, there are cracks in matrix and debonding of fibers due to carbonization shrinkage in the conventional carbon paper. Property measurements show that the former has much better conductivity and gas permeability than the latter. In addition, current density-voltage performance tests also reveal that the pyrocarbon coating can improve the properties of carbon paper used for electrode materials of fuel cell.     

高密度预制体制备炭/炭复合材料的弯曲力学性能与断裂机制

以丙烯作为碳源,氮气作为载气,采用初始密度为0.94g/cm3三维正交PAN基12K炭纤维预制体,利用自制的快速CVI炉制备基体热解炭结构为带状结构的C/C复合材料。力学性能测试结果表明,材料的弯曲断裂特征与制备过程中受到的高温热处理次数有关。从载荷-位移曲线来看,当C/C复合材料经过两次热处理时,C/C复合材料呈明显假塑性断裂特征。当C/C复合材料经过三次热处理时,载荷-位移曲线趋于稳定平滑,抗弯强度降低。从C/C复合材料断面的SEM图可以观察到材料断裂可以分为层间断裂和层内断裂,而层内断裂又因热解炭填充密度变化呈明显的分区断裂。由于热解炭和纤维含量在C/C复合材料中分布的差异,材料在不同的区域表现出不同的断裂特征,从而使得材料具备良好的弯曲强度同时具有一定的韧性特征。     

Oxidation behavior of C/C composites with the fibre/matrix interface modified by carbon nanotubes grown in situ at low temperature

Carbon nanotubes (CNTs) were grown in situ on the fibre surface of unidirectional carbon fibre preform. The carbon fibre preform with nanotube modified fibres was then densified by chemical vapor infiltration to obtain CNT-reinforced C/C (CNT-C/C) composite. The effects of CNTs on the oxidation kinetics and mechanism of C/C composites were investigated. The results show that due to the growth of CNTs, a more perfect structure of pyrolytic carbon (PyC) and better fibre/PyC interface had been obtained, which in turn result in slower mass loss. Furthermore, higher graphitization degree leads to larger activation energy of CNT-C/C composite, compared with C/C composite.     

The effect of partially carbonized fibers on the mechanical properties of carbon/carbon composites

The carbon/carbon (C/C) composite with satisfactory mechanical properties were obtained through introduction of partially carbonized fibers as a precursor. Applying this procedure the production cost of C/C composites may be significantly reduced. Stabilized PAN fibers were partially carbonized at temperatures ranging from 400 to 1000 °C and reinforced with phenolic resin, resole type. Cured composite were carbonized up to 1000 °C in an inert atmosphere. Monofilament tensile test strength, Young's modulus and tensile strength of partially carbonized fibers were determined. Mechanical properties of carbon/carbon composites (flexural strength and flexural modulus) determined by using three-point bending test. The effect of partially carbonized fibers on the mechanical properties of C/C composites was examined by scanning electron microscope (SEM) through analysis of the fracture surface. The C/C composite reinforced with partially carbonized fibers at 600 °C showed quite satisfactory flexural strength. This confirms assumptions that through co-carbonization of partially carbonized fibers and resin C/C composite with suitable mechanical properties could be obtained.     

挤压铸造制备Cf/ZL109复合材料及其组织观察

采用挤压铸造制备碳纤维增强ZL109复合材料．SEM观察预处理前后的碳纤维以及碳纤维顶制件的形貌．金相显激镜观察纤维在复合材料中的分布结果表明：预处理使碳纤维长径比满足制备合格预制件的要求，并有利于纤维在预制件中的均匀分散及预制件的成型；模压预制件纤维分布均匀．表面无团聚．碳纤维无氧化；挤压铸造制备的Cf／ZL109复合材料中纤维在基体中分市均匀，并具有方向性。     

CeO2在镀镍碳纤维增强铝合金基复合材料中的作用

以稀土氧化物CeO2为添加剂,研究CeO2对镀镍碳纤维增强铝合金基复合材料碳纤维的分布、气孔率以及力学性能的影响,利用扫描电镜分析和拉伸力学性能检测等探讨了CeO2在镀镍碳纤维增强铝合金基复合材料中的行为。结果表明:CeO2能够使碳纤维均匀分布在复合材料中,而不产生分层及团聚;而且能够降低复合材料的气孔率,使轧制态复合材料的抗拉强度、屈服强度分别提高23%和26%。     

短炭纤维增强C/C-SiC制动材料的摩擦磨损性能

采用温压？原位反应法制备C/C-SiC复合材料,利用QDM150型摩擦试验机研究短炭纤维（SCF）长度和纤维体积分数对C/C-SiC制动材料摩擦磨损性能的影响。结果表明：C/C-SiC制动材料能够保持较高且稳定的摩擦因数;SCF的体积分数将影响C/C-SiC制动材料的摩擦磨损性能,纤维体积分数为10%时,材料具有适中的摩擦因数和较低的磨损率;SCF长度对C/C-SiC制动材料的摩擦磨损性能有显著影响,炭纤维长度为12 mm时,材料具有最佳的摩擦磨损性能。     

Compressive strength of carbon nanotubes grown on carbon fiber reinforced epoxy matrix multi-scale hybrid composites

The characteristics of interface between fiber reinforcement and matrix have a strong influence on the properties of a composite material. Multiwalled carbon nanotubes were grown on carbon fibers by catalytic decomposition of acetylene using thermal chemical vapor deposition technique at 700 °C to modify the fiber surface. Unidirectional multi-scale composites were fabricated using these carbon nanotubes grown fibers with epoxy matrix. As the nanotubes were directly grown on the fibers they get strongly attached with the fibers thus modifying their surface condition which in turn alters the fiber/matrix interface. Modification of the fiber/matrix interface is therefore expected to change the properties of composites. The compressive strengths of these composites were measured which showed a significant enhancement of 43% and 94% in the longitudinal and transverse compressive strengths respectively as compared to composites made of carbon fibers which underwent a similar thermal cycle but without carbon nanotubes growth. The morphology of CNTs grown on carbon fibers was examined at nano-level using HRTEM which showed growth of carbon nanotubes with different morphology and diameter ranging from 5-50 nm.     

多孔C泡沫预制体液相渗硅制备C/SiC复合材料研究

以多孔C泡沫为预制体,利用液相渗Si工艺制备了C/SiC复合材料。采用酚醛树脂浸渍-裂解工艺对C泡沫预制体的孔隙率进行调整,考察浸渍-裂解周期对C泡沫预制体孔隙率的影响,研究了C泡沫预制体孔隙率对C/SiC复合材料密度、力学性能、组成和结构的影响。结果表明:预制体孔隙率为72%时制备的C/SiC复合材料性能较好,其密度为2.58g/cm3、弹性模量为81.39GPa,抗弯曲强度为83.88MPa;随着预制体孔隙率的降低,复合材料的密度、弹性模量和抗弯曲强度不断降低,预制体孔隙率的降低影响液相Si充分扩散与C反应,造成复合材料内部存在大量闭孔,这是导致C/SiC复合材料性能下降的主要原因。     

碳纤维含量对Al2O3+C/ZL109混杂复合材料摩擦磨损性能的影响

利用挤压铸造法制备了A1203 C／ZLl09短纤维混杂金属基复合材料，并探讨了A1203纤维体积分数为12％时，C纤维含量对该混杂复合材料摩擦磨损性能的影响。结果表明：随着C纤维体积分数的增加，复合材料的摩擦因数和磨损率逐渐降低。12％A1203和4％C短纤维的协同作用使复合材料从轻微磨损到急剧磨损的临界转变载荷比基体合金提高了1倍。当载荷低于临界载荷时，复合材料的主要磨损机制为犁沟磨损和层离，C纤维的加入有利于磨损表面裂纹尺寸的减小。但随着载荷的逐渐增加并发生严重磨损时，基体和复合材料的磨损机制均为严重的粘着磨损甚至局部熔化磨损。     

Structure formation during processing short carbon fiber- reinforced aluminum alloy matrix composites

Nickel- and copper-coated, as well as uncoated, short carbon fibers were dispersed in melts of aluminum or aluminum alloys by stirring followed by solidification of composite melts. Microstructural examina-tion of cast composites indicated extensive damage to the surface of the carbon fibers when uncoated carbon fibers were introduced into the melt under the conditions of the present investigation. When nickel- or copper-coated carbon fibers were used to make composites under similar conditions, the fibers generally did not exhibit observable amounts of fiber surface degradation at the interface, except for small islands of an Al₄C₃ phase. When nickel-coated carbon fibers were used to make composites, the coating reacted with the melt, and NiAl₃ intermetallic phase particles were observed in the matrix away from the fibers, indicating a preference for nucleation of NiAl₃ away from the fiber surfaces. Under a transmission electron microscope (TEM), the NiAl₃ phase was not observed on the surface of carbon fi-bers, except in some regions where the NiAl₃ phase engulfed the carbon fibers during growth. When cop-per-coated carbon fibers were used to make composites, the coating reacted with the melt, and particles of CuAl₂ intermetallic compound were generally dispersed in the matrix away from the fibers, except for a few locations where the CuAl₂ phase was found at the interface under TEM observation. These micro-structures are discussed in terms of nucleation of primary α aluminum and NiAl₃ or CuAl₂ phases and the interaction between short carbon fibers and these phases during growth while the composite was so-lidifying. Additionally, the role of the reaction between nickel or copper coatings and the melt on struc-ture formation is discussed; some of the differences between the nickel and copper coatings are attributed to the fact that nickel dissolves with an exothermic reaction. The differences between solidification of short fiber composites and particle or fiber composite are also discussed.     

添加钛对炭/炭复合材料渗铜的影响

通过铺展实验和渗透实验考查添加钛对铜与C/C复合材料润湿性能的影响。采用真空熔渗的方法成功地将铜合金液渗入到C/C复合材料坯体中。对渗铜后形成的C/C-Cu复合材料进行X射线衍射、金相和扫描电镜分析。结果表明,加入12%~16%(质量分数)的钛元素粉末使铜在C/C复合材料表面有好的铺展性能;含钛铜合金渗入到C/C复合材料中有TiC形成。添加钛元素能改善C/C复合材料渗铜性能的主要原因是改善铜在C/C复合材料中的化学吸附和物理吸附特性;通过毛细管力作用,合金液渗入到C/C复合材料坯体中。