碳纤维含量对短碳纤维－铜复合材料性能的影响

用粉末冶金法制造了碳纤维分布均匀的碳纤维一铜复合材料，测定了复合材料的力学性能和物理性能，表明在碳纤维与铜基体之间存在界面结合，碳纤维含量对复合材料性能影响极大。     

国产碳纤维与东丽碳纤维与PP复合材料性能的对比研究

分别采用国产永煤及日本东丽未处理过的碳纤维及经浓硝酸处理的碳纤维,制备了碳纤维增强聚丙烯(PP)复合材料。通过测量复合材料的力学性能表明加入少量未处理的国产永煤碳纤维,CF/PP复合材料的力学性能有了很大的提高,反之未处理的东丽碳纤维增强效果不明显。通过SEM分析了表面处理前后碳纤维复合材料界面的变化,结果表明对日本东丽碳纤维进行硝酸表面处理后可显著改善基体与碳纤维的界面粘结性能,进而提高CF/PP复合材料的力学性能。     

碳纤维改性环氧树脂复合材料研究进展

介绍最近几年碳纤维增强环氧树脂复合材料研究的前沿动向,重点叙述了碳纤维表面处理方法以及碳纤维在环氧树脂的应用,综述了环氧树脂/碳纤维复合材料的研究发展。     

碳纤维截面特性对碳纤维/环氧树脂复合材料压缩强度的影响

基于压拉平衡为特征的新一代先进复合材料的需求,开展了碳纤维截面形状和尺寸对碳纤维/环氧树脂复合材料压缩强度的影响研究。有限元模拟和试验结果均表明,增大碳纤维直径可以提高复合材料压缩强度。另外碳纤维截面形状也对复合材料压缩强度有影响,圆形截面优于椭圆形截面。      

碳纤维不同分布的碳纤维-铜复合材料的电导率

将碳纤维按不同方式分布与铜粉混合热压, 制取复合材料, 测定了碳纤维含量与分布方式对复合材料电导率的影响。给出了测定结果, 为复合材料的结构设计提供了一定的依据。      

碳纤维丝束结构对碳纤维/酚醛复合材料烧蚀性能的影响EI北大核心CSCD

以酚醛树脂为基体,以平纹碳布和短切碳纤维两种结构形式的碳纤维为增强剂,制备碳纤维增强的碳/酚醛复合材料。采用氧/乙炔烧蚀实验对复合材料的耐烧蚀性能进行了对比性研究,采用电子拉力试验机对复合材料的弯曲性能进行表征,采用扫描电镜对复合材料烧蚀形面进行观察,并通过固体火箭发动机对复合材料的烧蚀性能进行考核验证。研究结果表明:以这两种结构形式的碳纤维为增强剂制备的碳/酚醛复合材料,其氧乙炔质量烧蚀率的大小与碳纤维丝束的大小具有正相关的特性,碳纤维丝束越小碳纤维质量烧蚀率越低,当碳纤维增强剂处于单丝状态时,复合材料的氧乙炔质量烧蚀率达到最低为0.046 g/s,并且碳纤维的型号规格对复合材料氧乙炔质量烧蚀率的影响变小。固体火箭发动机实验表明,单丝状态下的碳纤维/酚醛复合材料的抗烧蚀冲刷性能明显优于束状碳纤维/酚醛复合材料。     

碳纤维复合材料力学性能研究进展

目的 综述碳纤维复合材料这一热结构材料的力学性能研究进展，推进碳纤维复合材料的研制和应用。方法 采用文献调研法，梳理和汇总国内外有关碳纤维复合材料力学性能的研究内容，对二维复合材料、针刺复合材料及三维编织复合材料3种结构进行性能影响因素分析。结论 影响碳纤维复合材料静态和动态力学性能的因素主要有温度、应变率、密度等，提出应进一步开展碳纤维复合材料在多因素耦合及高温动态性能方面的研究。     

碳纤维增强铜基复合材料研究进展

本文综述了碳纤维在铜基复合材料中的作用及其表面处理技术的发展现状。总结了近年来碳纤维表面改性方法以及存在的主要问题,分析了碳纤维对铜基复合材料组织的形成及其性能的影响。最后展望了碳纤维的发展前景。     

碳纤维复合材料低温热导率测试方法

针对碳纤维复合材料在X、Y、Z 3个方向的各向异性特点,分析其传热机理,讨论分析了碳纤维复合材料低温热导率测试方法.采用两种不同方法分别测试出碳纤维复合材料3个方向的低温热导率数据.根据测试结果,讨论了影响测试精度的主要因素,如温度、试样装配、试样厚度的影响等,给出了部分碳纤维复合材料低温热导率与温度关系曲线.     

碳纤维及其复合材料的新进展

本文简要介绍先进复合材料对发开高技术和新一代武器装备的重要意义,美国国防部已把复合材料收入国防关键技术计划.碳纤维是发展复合材料的基础,对碳纤维的发展国外给予高度重视,每年取得很多进展.本文介绍近年来碳纤维与复合材料的新进展,包括:高模、高强碳纤维及其复合材料;混杂纤维及其复合材料;纤维/聚亚胺颗粒;隐身用的特种碳纤维.     

短碳纤维-铜复合材料的研制

研究了用粉未冶金方法制造短碳纤维-铜复合材料,对这种复合材料的力学性能及物理性能进行了测试,证明该复合材料中,碳纤维与铜基体间存在着界面结合。     

Experimental description of thermomechanical properties of carbon fiber-reinforced TiC matrix composites

Titanium carbide ceramic is a good potential material used in high temperature environment for its good strength, erosion resistance and thermal stability. Unfortunately, the low thermal shock resistance and low fracture toughness are the well-known impediments to its application as high temperature structure components. In order to extend the application of TiC ceramics at high temperature, 20 vol.% short carbon fiber was added into TiC matrix to improve the thermomechanical properties. With the incorporation of carbon fiber, the thermal expansion coefficient of TiC composites was decreased and the thermal conductivity was increased slightly below 900 °C. The flexural strength was improved from 471 MPa for monolithic TiC to 593 MPa for TiC composites, and the strengthening effect of carbon fiber became more prominent at high temperatures. The addition of fiber decreased the elastic modulus of TiC composite. The elastic modulus of the composite decreased with increasing temperature. The improvement of high temperature strength and thermal conductivity and the decrease of thermal expansion will benefit the application of TiC composites in high temperature environment where the temperature usually varies.     

碳纤维增强水泥基复合材料的制备及热电性能研究

将不同含量(0.5%,1.0%,1.5%(质量分数))的碳纤维掺入到硫铝酸盐水泥基体中,制备了碳纤维增强水泥基复合材料。通过SEM、阿基米德排水测试法、四探针法等手段,研究了碳纤维含量对增强水泥基复合材料断面结构、抗弯强度、孔隙率、电导率、热导率和塞贝克系数的影响,并模拟太阳辐射进行了能量收集实验。结果表明,碳纤维均匀地分布在水泥基体中形成网格结构,碳纤维与水泥基体有很强的结合力。当碳纤维含量由0.5%(质量分数)增加到1.5%(质量分数)时,水泥基复合材料的抗压强度由71.36 MPa增加到106.51 MPa,增长了49.26%;孔隙率由0.8%增加到2.0%,增长了150.0%;电导率由0.0214 S/m增加到0.2408 S/m,增长了1025%;热导率由0.261 W/(m·K)减小到0.210 W/(m·K),减少了19.54%;塞贝克系数迅速增大,最大为1.22×10^4μV/K。当碳纤维含量为1.5%(质量分数)时,厚度为20 mm的水泥基复合材料每1 m^2可输出5~6μW的功率;在400 min辐照下,试样表面温度迅速达到70℃左右,1 m^2水泥基复合材料面板上收集到的能量高达8.1×10^-6 J。由此可知,碳纤维含量的增加,极大地提高了碳纤维增强水泥基复合材料的热电性能。     

密度对C/C复合材料热力学性能的影响

采用针刺预制体经化学气相沉积与沥青浸渍-高压碳化致密工艺制备C/C复合材料,通过控制沥青浸渍-高压碳化致密次数,获得了密度分别为1.70g/cm~3、1.82g/cm~3、1.89g/cm~3的三种C/C材料,测试材料的力学、热学性能。结果表明材料拉伸强度随密度升高而降低。当密度较低时,纤维/基体界面结合强度相对较低,可以延缓纤维断裂的发生;拉伸断口显示出假塑性断裂特征,有利于材料拉伸强度的提高。材料的压缩强度与剪切性能密切相关,且均随密度升高表现出先升后降的趋势。材料的热膨胀系数随密度升高而增大,材料中微晶之间的空隙在受热过程中可以吸收一部分膨胀量,因此对于C/C材料,降低密度有利于降低热膨胀系数。材料导热系数随密度升高而明显增大,且随密度升高,微晶尺寸增大,有利于晶格振动的传递,从而使得导热系数增大。热应力因子随密度升高而先升后降,作为热结构件使用时,采用密度为1.82g/cm~3的C/C材料可以获得相对较高的抗热震能力。在C/C材料研究开发中,可以综合对材料力学、热学性能的要求来对C/C材料密度指标进行设计。     

Enchanced high-temperature performances of SiC/SiC composites by high densification and crystalline structure

We report the enchanced in situ performances of tensile strength and thermal conductivity at elevated temperatures of the PCS-free SiC/SiC composite with a high fiber volume fraction above 50% fabricated by NITE process for nuclear applications. The composite was fabricated by the optimized combination of the fiber coating, the matrix slurry and the pressure-sintering conditions, based on our previous composites’ study history. The composite showed the excellent tensile strength up to 1500 °C, that it retained approximately 88% of the room-temperature strength. Also, the thermal conductivity of the composites represented over 20 W/m K up to 1500 °C, which was enough high to take the advantage of the assumed design value for nuclear applications. Microstructural observation indicated that the excellent high-temperature performances regarding tensile strength and thermal conductivity up to 1500 °C were the contribution to the high densification and crystalline structure in matrix.     

Effects of vacuum thermal cycling on mechanical and physical properties of high performance carbon/bismaleimide composite

The aim of this article was to investigate the effects of vacuum thermal cycling on mechanical and physical properties of high performance carbon/bismaleimide (BMI) composites used in aerospace. The changes in dynamic mechanical properties and thermal stability were characterized by dynamic mechanical analysis (DMA) and thermogravimetric analysis (TGA), respectively. The changes in linear coefficient of thermal expansion (CTE) were measured in directions perpendicular and parallel to the fiber direction, respectively. The outgassing behavior of the composites were examined. The evolution of surface morphology and surface roughness were observed by atomic force microscopy (AFM). Changes in mechanical properties including transverse tensile strength, flexural strength and interlaminar shear strength (ILSS) were measured. The results indicated that the vacuum thermal cycling could improve the crosslinking degree and the thermal stability of resin matrix to a certain extent, and induce matrix outgassing and thermal stress, thereby leading to the mass loss and the interfacial debonding of the composite. The degradation in transverse tensile strength was caused by joint effects of the matrix outgassing and the interfacial debonding, while the changes in flexural strength and ILSS were affected by a competing effect between the crosslinking degree of resin matrix and the fiber-matrix debonding.     

Experimental Study on Tensile Behavior of Carbon Fiber and Carbon Fiber Reinforced Aluminum at Different Strain Rate

In this study, dynamic and quasi-static tensile behaviors of carbon fiber and unidirectional carbon fiber reinforced aluminum composite have been investigated. The complete stress–strain curves of fiber bundles and the composite at different strain rates were obtained. The experimental results show that carbon fiber is a strain rate insensitive material, but the tensile strength and critical strain of the C_f/Al composite increased with increasing of strain rate because of the strain rate strengthening effect of aluminum matrix. Based on experimental results, a fiber bundles model has been combined with Weibull strength distribution function to establish a one-dimensional damage constitutive equation for the C_f/Al composite.     

Matrix and fiber influences on the cryogenic microcracking of carbon fiber/epoxy composites

Cryogenic cycling effects on symmetric carbon fiber/epoxy laminates were examined using model prepreg systems. The properties of the composite materials studied were altered through the introduction of variations in their structure and composition. The curing agent used, matrix backbone flexibility, toughening agents, and longitudinal coefficient of thermal expansion of the reinforcing fibers were changed to investigate their role in cryogenic microcracking. Examination of the laminates after cycling provided insight into the mechanism and origins of thermal stress-induced microcracking. Matrix properties and fiber tensile modulus were shown to have a significant impact on the response of the composite materials to cryogenic cycling. It was found in this study that higher glass transition temperatures of the laminates and the presence of toughening agents in the matrix decreased the microcracking propensity of these laminates. Higher tensile moduli and linear coefficients of thermal expansion of the fibers were found to increase the microcrack density in the laminates studied.     

碳纤维/铝/环氧复合板的初步研究

本文揭示了碳纤维/铝/环氧复合板的显微结构,比重、热胀性能与碳纤维含量的关系,探讨了增强组份的表面处理、碳纤维/铝的叠层结构设计、碳纤维含量、纤维混杂对复合板力学性能的影响。试验表明:碳纤维/铝/环氧复合板具有轻质、低热胀、高强度等特点,当碳纤维增强环氧的含量为55vol%时,它的拉伸,弯曲与剪切强度达到或超过芳纶纤维或玻璃纤维/铝/环氧复合板的相应值。