碳纤维-玻璃纤维层内混杂单向增强环氧树脂复合材料拉伸性能

采用不同混杂比的碳纤维-玻璃纤维层内经向混编单轴向织物制备了混杂纤维增强环氧树脂复合材料, 研究了不同混杂结构和不同混杂比的碳纤维-玻璃纤维/环氧树脂复合材料拉伸性能的变化及破坏形式。0°拉伸结果表明:同种混杂织物的不同混杂结构中, 碳纤维相对集中的完全对齐结构强度最高, 不同混杂比织物的完全对齐结构强度相当;碳纤维-玻璃纤维/环氧树脂复合材料的模量遵循混合定律。90°拉伸结果表明:纤维与树脂间的界面结合强度为碳纤维/树脂>玻璃纤维/树脂, 碳纤维-玻璃纤维/环氧树脂复合材料的强度、模量与材料厚度方向上界面的不同形式(单一或交替界面、碳纤维或玻璃纤维的分布位置等)有关, 与碳纤维的含量基本无关。      

单向连续碳纤维-玻璃纤维层间混杂增强环氧树脂基复合材料的力学性能

为了研究连续单向纤维的层间混杂方式对复合材料力学性能及破坏方式的影响,采用碳纤维-玻璃纤维体积比为1∶1,以拉-挤成型法制备了具有不同层间混杂结构的连续单向纤维增强环氧树脂基复合材料,并研究了不同层间混杂结构的连续单向碳纤维-玻璃纤维增强环氧树脂基复合材料的力学性能及破坏形式。结果表明：具有层间混杂结构的复合材料抗拉强度处于纯碳纤维/环氧树脂复合材料和纯玻璃纤维/环氧树脂复合材料之间,复合材料的拉伸断裂方式为劈裂;具有层间混杂结构的复合材料的层间剪切强度均优于纯碳纤维/环氧树脂复合材料和纯玻璃纤维/环氧树脂复合材料,复合材料的剪切断裂方式为层间断裂。     

管道修复用涤纶-苎麻复合机织物性能试验

针对传统管道内衬修复材料施工中易出现内壁塌陷等问题,结合目前快速发展的绿色纤维复合材料,提出在涤纶机织物内衬材料中加入苎麻纱线,制作涤纶-苎麻复合机织物材料来提高树脂对管道修复用内衬机织物的浸透性能,增强内衬材料和管壁的粘结性能。以纤维外观、抽拔实验后纤维断面形貌的电镜观察,并通过树脂与织物接触角的测试、粘结实验,综合分析了涤-麻复合机织物的树脂浸透性,同时对涤纶-苎麻复合机织物力学性能进行测试来保障内衬复合材料满足强度的要求。实验结果表明,采用上述涤-麻复合织造的方法,可以显著提高树脂的浸透性能,有利于携带更多的树脂粘结剂提高树脂与管壁的粘结性,减少塌陷发生的可能性。同时加入麻复合的机织物,拉伸顶破性能都满足高压燃气管道的修复要求。     

快速固化碳纳米管/苎麻纤维/环氧树脂复合材料层板的制备与性能

针对植物纤维/树脂基复合材料高性能化问题,本研究以羟基化碳纳米管/无水乙醇分散液预先浸渍苎麻纤维织物,得到了碳纳米管分散均匀的碳纳米管/苎麻纤维多尺度复合织物,并进一步以快速固化环氧树脂为基体,采用真空辅助树脂灌注成型工艺(VARI)制备了碳纳米管改性的苎麻纤维/环氧树脂基复合材料层板(PRFC)。研究结果表明,相比未采用碳纳米管改性的苎麻纤维/环氧树脂复合材料(RFC),PRFC的弯曲强度提高14.7%,冲击强度提高20.9%。相比碳纳米管预先分散于环氧树脂基体中制备的碳纳米管改性苎麻纤维/环氧树脂复合材料(MRFC),PRFC的力学性能提高更显著。同时,PRFC的吸湿性能比MRFC和RFC的明显降低。     

C/C复合材料拉伸强度与针刺成型参数相关性研究

采用Design-expert软件设计预制体不同针刺成型参数组合试验, 研究预制体针刺成型参数对针刺碳/碳(C/C)复合材料拉伸强度的影响, 并构建了响应曲面数学模型, 实现对针刺C/C复合材料拉伸强度的优化与预测, 其模型显著性P=0.0206, 各试验实测值与预测值相对误差≤10.82%, 模型具有较高的拟合度。响应曲面回归分析表明: 针刺深度对拉伸强度有极显著影响, 针刺密度对拉伸强度有显著影响, 在本研究的针刺成型参数取值范围内, 拉伸强度的预测区间为42.31~91.87 MPa。通过模型优化出的针刺成型参数组合为: 针刺密度11 pin/cm²、针刺深度 11 mm、网胎面密度50 g/m², 相应拉伸强度预测值为88.62 MPa, 验证值为90.71 MPa, 相对误差2.36%。     

苎麻纤维布和玻璃纤维布混杂铺层复合材料的力学性能

利用真空吸注成型(vacuum resin absorbable molding,VRAM)工艺制备苎麻纤维布与玻璃纤维布混杂铺层的环氧树脂基复合材料。测定复合材料的损耗因子、储能模量的温度谱和力学性能;利用单悬臂梁共振实验测量复合材料的共振频率和自由振动衰减曲线并计算出了阻尼因子。用有限元软件对其共振频率和自由振动衰减实验进行仿真分析。结果表明:通过苎麻纤维布/玻璃纤维布的混杂铺层,能够实现材料阻尼性能和力学性能的可控调节,充分发挥复合材料可设计性强的优势。其中RGR铺层的复合材料的损耗因子比纯玻璃纤维板提高了1.4倍,而拉伸强度比纯苎麻纤维板提高了3倍多;自由振动的有限元模拟曲线和实验曲线基本吻合,表明可以通过模拟软件实现复合材料的虚拟振动测试,从而为材料性能预测和设计提供方便。     

苎麻骨基复合材料制备与阻燃抑烟特性分析

为拓展苎麻资源的高值清洁利用,以苎麻骨粉末为基材,以纳米氧化铜和环氧树脂粉末为强化因子,通过温压成形法制备苎麻骨基复合材料;采用响应面试验设计方法,优化成形工艺参数与强化因子;借助锥形量热仪与扫描电镜等研究苎麻骨基复合材料的阻燃抑烟特性。结果表明,苎麻骨基复合材料的最优工艺参数与最佳强化因子分别为:成形温度为180℃,成形压力为70 MPa,保温保压时间为30 min,环氧树脂质量分数为9.2%,纳米氧化铜质量分数为30.8%;制备的苎麻骨基复合材料强度高、疏水性好,静曲强度高达90.12 MPa,吸水率仅为0.51%;苎麻骨基复合材料具有延迟着火、迟缓火焰扩散、抑制燃烧热释放、抑制烟气释放的能力;其燃烧残余物炭层结构紧凑、致密,可以有效抑制炭层的爆裂。     

硅溶胶改性处理对碳纤维/环氧树脂复合材料拉伸性能的影响

用溶胶-凝胶法制备硅溶胶对碳纤维进行表面改性,观测了环氧树脂液滴在单向排列碳纤维集束表面的铺展过程;以环氧树脂为基体制备单向排列的碳纤维/环氧树脂复合材料,研究了硅溶胶改性处理碳纤维对其拉伸性能的影响。结果表明:碳纤维经过硅溶胶改性处理后,Si—o—Si,-NH₂等极性官能团的引入改善了环氧树脂对其的浸润性能,从而改善了碳纤维与环氧树脂间的界面粘结性能,使碳纤维/环氧树脂复合材料的横向拉伸强度显著改善,但纵向拉伸强度影响不大;与未经过表面处理的复合材料相比,经过硅溶胶改性处理的碳纤维/环氧树脂复合材料其横向拉伸强度提高了62.74%;与用硝酸处理的碳纤维制备的复合材料相比,用硝酸处理后再用硅溶胶处理的碳纤维所制备的复合材料,其横向拉伸强度提高了35.27%。     

苎麻纤维/碳纤维/聚乙烯复合材料的性能研究

将苎麻纤维(RF)、短切碳纤维(SCF)混杂加入低密度聚乙烯(LDPE)树脂中,考察了纤维混杂方式、马来酸酐接枝物添加方式对LDPE/RF/SCF(100/10/5)复合材料力学性能的影响。结果表明:以SCF/LDPE为表层,以RF/LDPE为芯层的夹芯结构LDPE/RF/SCF(100/10/5)复合材料拉伸强度较LDPE/RF(100/15)复合材料提高了49%,冲击强度提高78%;体系中添加3份的马来酸酐接枝物(LDPE-g-MAH)后,复合材料冲击强度提高了8%,马来酸酐接枝物改善复合材料冲击强度比改善拉伸强度更有效。扫描电镜结果表明LDPE-g-MAH能改善麻纤维、碳纤维与基体间的界面结合。     

功能化MWCNTs网格/环氧树脂复合材料的制备及性能

采用正压过滤法制备了多壁碳纳米管（MWCNTs）网格（巴基纸）,并采用真空辅助RTM工艺制备了MWCNTs网格/环氧树脂复合材料。通过SEM、FTIR、拉伸测试等对MWCNTs网格的微观形貌和性能进行了表征,并研究了MWCNTs网格/环氧复合材料的拉伸性。结果表明,所制备的功能化MWCNTs网格比较均匀,拉伸强度在22~32 MPa之间,拉伸模量约为1 GPa,相比未功能化处理的MWCNTs网格,强度最大提高了约167%。功能化MWCNTs网格/环氧树脂复合材料的拉伸强度和拉伸模量可达到152 MPa和6.48 GPa,相比空白环氧树脂提高了约1倍以上,拉伸试样断面SEM表明,环氧树脂对功能化MWCNTs网格的浸润效果良好,界面结合紧密,有效地提高了复合材料的力学性能。     

Formation of novel thermoplastic composites using bicomponent nonwovens as a precursor

This study focuses on a novel technique to produce thermoplastic composites directly from bicomponent nonwovens without using any resins or binders. Conceptually, the structure of the bicomponent fibers making up these nonwovens already mimics the fiber–matrix structure of fiber reinforced composites. Using this approach, we successfully produced isotropic thermoplastic composites with polymer combinations of polyethylene terephthalate/polyethylene (PET/PE), polyamide-6/polyethylene (PA6/PE), polyamide-6/polypropylene (PA6/PP), and PP/PE. The effects of processing temperature, fiber volume fraction, and thickness of the preform on the formation and structure of the nonwoven composites were discussed. Processing temperatures of 130 and 165 °C for PE and PP matrices, respectively, resulted in intact composite structures with fewer defects, for fiber volume fraction values of up to 51%. Moreover, an insight into the changes on the fine structure of the bicomponent fibers after processing was provided to better explain the mechanics behind the process. It is hypothesized that the composite fabrication process can result in annealing and increases the degree of crystallinity and melting temperature of polymers by thickening lamellae and/or removing imperfections. One of the other outcomes of this study is to establish what combination of mechanical properties (tensile and impact) nonwoven composites can offer. Our results showed that compared to glass mat reinforced thermoplastic composites, these novel isotropic nonwoven composites offer high specific strength (97 MPa/g cm⁻³ for PA6/PE), very high strain to failure (152% for PP/PE), and superior impact strength (147 kJ/m² for PA6/PP) which can be desirable in many critical applications.     

碳纳米管纤维/环氧树脂复合材料的界面剪切强度及微观结构

研究了碳纳米管纤维的微观结构和拉伸性能,并进一步分析了其与环氧树脂形成界面剪切强度及微观结构。采用单丝断裂试验测试了碳纳米管纤维/环氧树脂复合材料体系的界面剪切强度,结合单丝断裂过程中的偏光显微镜照片、复合材料的拉曼谱图和断口扫描电镜照片,研究了碳纳米管纤维/环氧树脂复合材料界面的微观结构。结果表明: 碳纳米管纤维/环氧树脂复合材料的界面剪切强度约为14 MPa;在碳纳米管纤维和环氧树脂形成界面的过程中,环氧树脂可以浸渍纤维,形成具有一定厚度的复合相,这种浸渍过程和界面相的形成都有利于碳纳米管纤维与基体之间的连接。     

Tensile behaviour of nonwoven structures: comparison with experimental results

Nonwoven structures have been recently explored for numerous novel applications ranging from composites to scaffolds. The tensile property of nonwovens is a pre-requisite and indeed, one of the main parameters to determine their performance for such applications. In the first part, a modified micromechanical model describing the tensile behaviour of thermally bonded nonwovens was proposed by incorporating the effect of fibre re-orientation during the deformation (Rawal et al., J Mater Sci 45:2274, 2010). In this study, an attempt has been made to compare the theoretical and experimental stress–strain curves of thermally bonded and spunbonded nonwoven structures. These theoretical findings have been obtained from the most popular analytical tensile models of nonwovens available in the literature in addition to our modified tensile model. Poisson’s ratio has also been determined experimentally in order to predict the stress–strain behaviour of nonwoven, and its relationship with longitudinal strain has clearly distinguished between the randomly and preferentially orientated types of structures. In thermally bonded nonwovens, the tensile strength in various test directions is computed through pull-out stress and a comparison is made with the experimental results.     

Structure,mechanical and thermal properties of BMI/E-44/CNTs ternary composites via amination method

Multi-walled carbon nanotubes(CNTs) were modified by an amination treatment with hexamethylenediamine(HMD), and then bismaleimide(BMI)/epoxy(E-44)/CNTs ternary composites were prepared using modified CNTs as the reinforcement via a simple mixing and curing molding method. The results show that the surfaces of CNTs are grafted polymer with the thickness of 3 nm and the dispersity of surface grafted carbon nanotubes(SG-CNTs) in the resin composites can be improved. The prepared composites contain C-C, C-N, C=O and-COOH groups and can keep a smooth surface. In addition, the composites have the flexural strength of 152 MPa, the tensile strength of 73 MPa and the impact strength of 87 k J m~(-2),respectively, when the weight ratio of BMI to E-44 is 1:8 and the content of SG-CNTs is 2 wt%. However,the thermal stability of the composites with SG-CNTs is a little lower than that of the composites without SG-CNTs.     

高性能针刺碳/碳复合材料的制备与性能

为获得高性能针刺碳/碳复合材料,拓展其应用领域,通过优化针刺工艺参数,设计并研制了不同结构参数的针刺预制体。采用沥青高压致密化工艺将针刺预制体制备成一系列针刺碳/碳复合材料,研究了针刺碳/碳复合材料的微观结构、力学性能和热物理性能。结果表明,针刺预制体的针刺深度、针刺密度以及短/长纤维配比等对碳/碳复合材料的力学性能和热物理性能影响显著。当针刺深度为12mm、针刺密度为22针/cm2、短/长纤维比例为1.0:4.8时,针刺碳/碳复合材料表现出优良的综合性能,拉伸、压缩、弯曲、面内剪切和层间剪切强度分别达到207、228、285、54和28 MPa。     

聚酰亚胺表面处理玻璃纤维/环氧树脂复合材料力学性能

采用浇铸成型工艺制备含0.5wt%、长度分别为1 mm、3 mm、5 mm的短切玻璃纤维/环氧树脂（GF/EP）复合材料,研究含活性酚羟基和不含酚羟基的两种聚酰亚胺（PI）处理GF表面对纤维束拉伸强度及GF/EP复合材料力学性能的影响,并进一步研究PI处理GF对复合材料热性能的影响。研究结果表明,经过PI处理的GF,集束性和拉伸强度得到提高。含活性酚羟基聚酰亚胺（PI1）处理的GF拉伸强度由原丝束的517 MPa提高到1 032 MPa,不含酚羟基聚酰亚胺（PI2）处理的GF提高到986 MPa。当PI1处理的GF长度为3 mm时,GF/EP复合材料的力学性能最好,拉伸强度比未处理的提高23.62%,拉伸模量提高34.03%,弯曲强度提高28.74%,断裂韧性提高13.04%;PI2处理的GF,GF/EP复合材料拉伸强度提高15.87%,拉伸模量提高23.70%,弯曲强度提高14.11%,断裂韧性提高4.05%。此外,PI处理GF对GF/EP复合材料热性能也有一定程度的提高。     

Determination of mechanical behavior of natural fibre based hybrid composites experimentally

This paper deals with the production and the mechanical testing of natural fibre‐based hybrid composites. Hybrid composite is produced by vacuum assisted resin infusion method of woven jute fabric and nonwoven wool felt along with glass fabric. Tensile, flexure and impact properties have been evaluated and compared. The tensile strength and the Young's modulus were found to be 70.66 MPa and is 5.63 GPa, respectively. Flexure and impact tests were performed on both woven jute fabric surface and on nonwoven wool felt surface of the composite specimens. The highest flexural strength was obtained in the specimen loaded at the woven jute fabric surface. Impact test results show that the specimens impacted at the nonwoven wool felt surface were carrying higher loads than the specimens impacted at the woven jute fabric surface.     

Technora纤维表面等离子体处理对其复合材料界面性能的影响

用扫描电子显微镜观察Technora纤维表面物理形貌并测量单丝纤维的拉伸强度以分析等离子体处理对纤维本体性能的影响,再用层间剪切强度和吸水率分别表征复合材料在室温干态和高温湿态下的界面性能,研究了等离子体处理对Technora纤维复合材料界面性能的影响。结果表明,用等离子体处理后纤维表面的物理形貌发生了显著变化,复合材料的层间剪切强度由未处理时的15.74 MPa提高到24.93 MPa,提高的幅度高达58.4%;同时,复合材料的吸水率下降而本体性能基本不受影响。上述结果表明,等离子体对Technora纤维的表面改性能有效地改善其复合材料的界面性能。