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1.
对多壁碳纳米管(MWCNTs)进行改性处理,得到表面接枝1,3,5-苯三甲酸的碳纳米管(B-MWCNTs)。分别将MWCNTs和B-MWCNTs分散在环氧树脂基体及上浆剂中,通过缠绕成型法制备含有MWCNTs的碳纤维增强环氧树脂预浸料,并采用热压成型工艺制备MWCNTs/碳纤维环氧树脂复合材料层合板。结果表明,B-MWCNTs在环氧树脂基体和上浆剂中的分散状态明显优于MWCNTs。添加B-MWCNTs后复合材料的玻璃化转变温度(Tg)和失重5%时对应的温度均有所提高。而且,添加B-MWCNTs可以明显提高碳纤维环氧树脂复合材料的力学性能。当MWCNTs含量为0.5%(质量分数)时,B-MWCNTs/碳纤维环氧树脂复合材料层合板的压缩强度、层间剪切强度和冲击后压缩强度(CAI)分别提高了14.3%,37.1%和23.4%。  相似文献   

2.
采用双酚A型环氧树脂(E-51)改性二氧化双环戊二烯树脂(CDR-0122),以改善其力学性能。首先根据复合材料力学性能选择较好的稀释剂,然后比较树脂基体在改性前后的玻璃纤维(Gf)和炭纤维(Cf)复合材料的基本力学性能和耐热性能。结果表明,环己二醇二缩水甘油醚(CDX-1180)是优于丙酮的一种稀释处理剂。同时用CDX-1180做稀释剂处理时,树脂基体经改性后,所制得的Gf层合板拉伸强度和拉伸模量分别提高了19.1%和16.8%,弯曲强度和弯曲模量分别提高了20.5%和12.6%;所制得的Cf层合板拉伸强度和拉伸模量分别提高了9.7%和8.7%,弯曲强度和弯曲模量分别提高了26.2%和7.0%;E-51改性CDR-0122树脂复合材料相比纯的CDR-0122树脂复合材料的玻璃化转变温度和热稳定性都略有提高。  相似文献   

3.
以汽车内饰用废弃塑料为主要原料,粉碎后通过添加新的接枝改性聚丙烯短切玻璃纤维制备出复合板材,研究了改性PP和短切玻纤对材料力学性能的影响.结果表明,改性PP的加入有利于改善材料的成形性能.添加新的改性聚丙烯后,复合材料的压缩强度和压缩模量增大,随着改性PP含量的提高,弯曲强度大幅提高而弯曲模量稍有降低;随着短切玻璃纤维含量的提高,材料的弯曲强度及弯曲模量均明显提高.  相似文献   

4.
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。  相似文献   

5.
采用真空袋-热压罐工艺制备单向碳纤维增强树脂基复合材料(CFs/EP)层合板,并将高低温试验箱与万能试验机相结合,通过合理使用低温胶和低温引伸计,并在降温过程中实施应力-应变实时调零等关键技术,在室温和液氧超低温度(-183℃)下对单向CFs/EP层合板进行拉伸和弯曲试验,研究了其超低温力学性能,并根据室温和超低温试验后试样的微观和宏观特征,揭示了超低温环境下复合材料力学性能变化机制。结果表明,与室温力学性能相比,单向CFs/EP层合板超低温拉伸强度下降约为9.5%,而拉伸模量上升约为6.2%,主要是由于超低温环境下,树脂的收缩使绝大部分碳纤维与树脂间形成了强界面,拉伸后试样呈"劈裂式"破坏形式,无法使每根纤维都充分发挥其强度,拉伸强度下降,同时超低温也限制了树脂大分子链的运动,所以导致单向CFs/EP层合板拉伸模量上升;单向CFs/EP层合板超低温弯曲强度和弯曲模量分别提高约54.75%和11.64%,这是由于单向CFs/EP层合板的常温和超低温的弯曲破坏形式均为分层剪切破坏,超低温下复合材料的界面增强,提高了单向CFs/EP层合板抵抗剪切分层的能力,进而使CFs/EP的弯曲性能得到提高。  相似文献   

6.
采用拉挤成型工艺制备了结构均一有序、外貌光亮顺滑的高性能碳纤维/环氧树脂复合材料板,并对其进行了力学性能测试。研究结果表明:高性能碳纤维/环氧树脂复合材料板,在0°条件下,拉伸强度1889MPa,拉伸模量141GPa,压缩强度1212MPa,压缩模量130GPa,弯曲强度1107MPa,弯曲模量136GPa;在90°条件下,弯曲强度86MPa;层间剪切强度61.834MPa,具有较好的力学性能。  相似文献   

7.
用硅烷偶联剂对磨碎玻璃纤维表面进行改性,并制备玻璃纤维/环氧树脂复合材料,采用超声分散对复合材料分散处理,探讨不同磨碎玻璃纤维粉质量比对环氧树脂基复合材料压缩、拉伸性能的影响。研究表明,添加磨碎玻璃纤维后,环氧树脂的强度和硬度显著增强。当磨碎玻璃纤维掺量在15%~25%之间时,复合材料的综合力学性能最好,其压缩强度、压缩模量、拉伸强度最高达到67.1 MPa、1.68 GPa、57.6 MPa,与纯环氧树脂相比提高了24%、35%、34%;断裂伸长率随着掺量的增加逐渐降低,当含量达到30%时比纯环氧树脂的降低了48%,表明添加玻璃纤维粉后环氧树脂脆性增强。目数小粒径较大的玻璃纤维粉对环氧树脂力学性能增强效果更优,但影响程度不如含量对复合材料力学性能的影响大。  相似文献   

8.
通过对胺基化多壁碳纳米管(MWCNTs-NH2)进行改性,得到改性MWCNTs悬浮液(MWCNTs-NH2(M))。分别将羧基化MWCNTs (MWCNTs-COOH)和MWCNTs-NH2(M)分散在环氧树脂(EP)中,采用热熔法制备了多尺度MWCNTs-碳纤维(CF)/EP复合材料。研究了MWCNTs对EP模量、韧性及EP与CF之间界面黏结强度的影响,并分析了MWCNTs与CF上浆剂的作用,评价了多尺度MWCNTs-CF/EP复合材料的力学性能。结果表明:官能团化的MWCNTs可对EP的模量和韧性起到更好的增强作用。MWCNTs接枝的-COOH或-NH2可与CF上浆剂中的环氧基团发生化学反应,提高EP与CF之间的界面剪切强度。MWCNTs-NH2(M)对多尺度MWCNTs-CF/EP复合材料力学性能的增强效果优于MWCNTs-COOH,当MWCNTs-NH2(M)的含量为1wt%时,多尺度复合材料的0°压缩强度、90°压缩强度、弯曲强度、弯曲模量、冲击后压缩强度(CAI)分别提高了16.7%、16.3%、40.9%、30.3%、20.6%。  相似文献   

9.
将羧基化多壁碳纳米管(MWCNTs)添加到TDE85环氧树脂中,然后与碳纤维非褶皱无纺布(C-NCF)复合,制备成[0°/90°/+45°/-45°]S层合板。采用三点弯曲、短梁剪切和单边切口弯曲测试方法以及动态力学性能分析方法,研究了不同含量的MWCNTs对层合板弯曲性能、层间剪切强度(ILSS)、Ⅱ型层间断裂韧性(GⅡC,以及玻璃态转变温度(Tg)的影响。并采用SEM对Ⅱ型试样的断面进行分析。结果表明,MWCNTs的加入显著提高了NCF层合板的力学性能。与空白试样相比,当MWCNTs在树脂中的质量分数为2.0%时,弯曲强度和模量分别提高了约26%和6%;当MWCNTs的质量分数为0.5%时,ILSS、GⅡC、Tg分别提高约14%、27%和14%。  相似文献   

10.
不同孔隙率CFRP层合板静态力学性能研究   总被引:3,自引:2,他引:1  
为了研究孔隙率对织物碳纤维/环氧树脂复合材料层合板静态力学性能的影响规律,分别测量了孔隙率为0.33%至1.50%的CFRP层合板的弯曲强度和层间剪切强度,并进行有限元模拟.在适用于复合材料单向板的改进Hashin失效准则基础上,建立了适用于织物纤维增强复合材料静态力学强度的失效准则.通过引入复合材料基本强度参数预测不同孔隙率CFRP层合板的力学性能,结合刚度突然退化模型,采用ABAQUS软件建立了有限元模型.试验结果表明,随着孔隙率的增加,复合材料层合板的弯曲强度和层间剪切强度均呈下降趋势.有限元模型较为准确地预测了不同孔隙率织物碳纤维/环氧树脂复合材料层合板的弯曲强度和层间剪切强度.  相似文献   

11.
In this study, two types of thermoplastic matrices (low melting point polyethylene terephthalate (LPET) fiber and polypropylene (PP) fiber) and glass fiber/epoxy resin/multi-walled carbon nanotubes (MWCNTs) were used to fabricate the thermoplastic and thermoset composite materials with 3D biaxial warp-knitted fabrics. Thermoplastic and thermoset composites were fabricated using hot-press and resin transfer molding (RTM) methods. The fabricated samples were tested with tensile and three-point flexural tests. In thermoplastic composites, samples in the 90° direction and LPET matrix showed the best tensile and flexural properties with an improvement of 39 and 21% tensile modulus and strength, 16 and 8% flexural modulus and strength compared to the PP samples in the same direction. In thermoset composites, samples in the 90° direction and MWCNTs showed the best improvement of the flexural modulus and strength with 97 and 58% compared to the samples without MWCNTs. This improvement can most likely be attributed to an increase in interfacial adhesion due to the presence of the carbon nanotubes.  相似文献   

12.
为探究热塑性酚酞基聚醚酮(Polyaryletherketone with Cardo,PEK-C)树脂薄膜及膜厚对层间增韧碳纤维/环氧树脂复合材料力学性能的影响,利用浸渍提拉法制备了三种不同厚度(分别约为1 μm、10 μm、30 μm)的PEK-C膜,通过热压成型制备了层间增韧碳纤维/环氧树脂复合材料层合板,对其进行了Ⅰ型层间断裂韧性、冲击后压缩强度、层间剪切及弯曲性能测试,并利用SEM观察微观形貌及AFM扫描微观相图。结果表明:不同PEK-C膜厚增韧碳纤维/环氧树脂复合材料的Ⅰ型层间断裂韧性、冲击后压缩强度及层间剪切强度有不同程度提高,Ⅰ型层间断裂韧性及层间剪切强度以膜厚为10 μm最佳,分别增大了157.17%和17.57%,冲击后压缩强度以膜厚为30 μm最佳,达到了186.67 MPa,这是由于PEK-C与环氧树脂在热压固化过程中形成了双相结构,改善了材料韧性;但弯曲性能持续下降,强度及模量由未增韧的1 551 MPa、106 GPa分别降至30 μm时的965 MPa、79 GPa,这是由于PEK-C树脂扩散进入环氧树脂中,降低了纤维体积分数及材料刚度。   相似文献   

13.
为改善玻璃纤维增强聚苯硫醚(PPS)复合板材的力学性能,分别以柔性的玻璃纤维布和PPS非织造布作为增强体和基体,采用叠层热压成型法制备出刚性的复合板材,采用力学性能测试、XRD、PLM、SEM研究了热压温度、热压时间、玻璃纤维含量和处理玻璃纤维布的硅烷偶联剂种类对复合板材的力学性能、结晶度、结晶形态和微观形貌的影响。结果表明,在无硅烷偶联剂处理玻璃纤维布时,控制热压温度为320℃,热压时间为30 min,压力为30 MPa,玻璃纤维质量分数为50%,复合板材的拉伸强度和弯曲强度最佳,分别为286.0 MPa和175.0 MPa,缺口冲击强度达到61.6 MPa。使用硅烷偶联剂KH560处理玻璃纤维布,在最佳成型工艺条件下,复合板材力学性能改善最明显,其弯曲强度为394.9 MPa,弯曲模量为23.6 GPa,层间剪切强度为16.4 MPa,缺口冲击强度为81.0 MPa。通过优化实验条件和使用硅烷偶联剂处理玻璃纤维表面,复合板材的力学性能得到了明显提高。  相似文献   

14.
The effect of multi-walled carbon nanotube (MWCNT) addition on mechanical properties of epoxy resin was investigated to obtain the tensile strength, compressive strength and Young’s modulus from load versus displacement graphs. The result shows that the tensile strength, compressive strength and Young’s modulus of epoxy resin were increased with the addition of MWCNT fillers. The significant improvements in tensile strength, compressive strength and Young’s modulus were obtained due to the excellent dispersion of MWCNT fillers in the epoxy resin. The dispersion of MWCNT fillers in epoxy resin was observed by scanning electron microscopy (SEM) and transmission electron microscopy (TEM) analysis.Also, Halpin–Tsai model was modified by considering the average diameter of internal/external of multi-walled nanotube and orientation factor (α) to calculate the Young’s modulus of multi-walled carbon nanotubes (MWCNTs)/epoxy resin composite. There was a good correlation between the experimentally obtained Young’s modulus and modified Halpin–Tsai model.  相似文献   

15.
Epoxy resin modified with nanofillers cannot be used alone for high performance structural applications due to their low-mechanical properties. Therefore, the objective of this work is to hybridize unidirectional and quasi-isotropic glass fiber composite laminates with 1.0 wt% multi-walled carbon nanotubes (MWCNTs). Results from flexural and damping characterizations showed that the flexural strength and modulus, storage modulus, and damping ratio of MWCNT/E nanocomposite are improved by about 7% ± 1.5% compared to neat epoxy. The enhancement in the flexural strength of quasi-isotropic laminate (20.7%) is about ten times higher than that for unidirectional laminate (2.1%). The flexural moduli of the nano-hybridized laminates are reduced by about 7.5–10.8%. Accordingly, the ultimate failure strain and damping properties are evidently improved. The improvement in damping ratio in some cases is about 100%. The high correlation coefficient (0.9995) between flexural and storage moduli suggests using the dynamic nondestructive tests for evaluation the elastic properties of composites.  相似文献   

16.
The objective of this study is to compare the mechanical and water absorption properties of kenaf (Hibiscus cannabinus L.) fibre reinforced laminates made of three different resin systems. The use of different resin systems is considered so that potentially complex and expensive fibre treatments are avoided. The resin systems used include a polyester, a vinyl ester and an epoxy. Laminates of 15%, 22.5% and 30% fibre volume fraction were manufactured by resin transfer moulding. The laminates were tested for strength and modulus under tensile and flexural loading. Additionally, tests were carried out on laminates to determine the impact energy, impact strength and water absorption. The results revealed that properties were affected in markedly different ways by the resin system and the fibre volume fraction. Polyester laminates showed good modulus and impact properties, epoxy laminates displayed good strength values and vinyl ester laminates exhibited good water absorption characteristics. Scanning electron microscope studies show that epoxy laminates fail by fibre fracture, polyester laminates by fibre pull-out and vinyl ester laminates by a combination of the two. A comparison between kenaf and glass laminates revealed that the specific tensile and flexural moduli of both laminates are comparable at the volume fraction of 15%. However, glass laminates have much better specific properties than the kenaf laminates at high fibre volume fractions for all three resins used.  相似文献   

17.
通过物理沉积法和静电吸附法在玻璃纤维织物(GF)表面包覆多壁碳纳米管(MWCNTs),制备GF-d-CNTs和GF-a-CNTs两种多尺度增强体,采用真空灌注工艺制备MWCNTs-GF增强环氧复合材料。采用静态、动态力学法、扫描电镜、红外光谱等分析手段,对复合材料的拉伸、弯曲、层间剪切、黏弹性和微观组成结构表征。结果表明:MWCNTs包覆于GF表面形成"倒刺"结构,并通过啮合作用增强了复合材料界面的强度和树脂韧性,提高了复合材料的玻璃化温度(Tg)等;与纯GF复合材料相比,GF-d-CNTs复合材料的拉伸强度和模量分别提高14.5%和37.9%,弯曲强度和模量分别提高26.2%和36.6%,层间剪切强度提高31.5%;GF-a-CNTs复合材料的Tg提高了8.9℃。  相似文献   

18.
通过对碳纤维环氧复合材料试样进行不同湿热环境下的拉伸和压缩实验,分析其吸湿特性、拉压力学性能、破坏后断口形貌以及动态力学性能,探讨湿热对该复合材料的拉伸和压缩性能的影响。结果表明:碳纤维环氧复合材料的吸湿过程满足Fick定律,饱和吸湿率约为0.86%。吸湿后材料表面变得光滑,有少量纤维拔出和树脂破坏发生,但吸湿后没有发生化学反应和新物质生成。吸湿后在130℃下,复合材料的拉伸性能保持率为96%,而压缩性能保持率仅为69%。吸湿后玻璃化转变温度比干态时下降了33℃。  相似文献   

19.
以泡沫SiC陶瓷为基本骨架,以改性酚醛树脂为基体,加入短切高硅氧玻璃纤维制备出陶瓷/纤维/树脂超混杂复合材料(SHCM),研究了泡沫陶瓷骨架和高硅氧纤维对材料力学性能的影响.结果表明,泡沫陶瓷骨架有利于材料的刚度和尺寸稳定性提高.加入泡沫陶瓷骨架后,纤维/树脂/陶瓷超混杂复合材料的压缩强度和压缩模量增大,随着泡沫陶瓷骨架含量的提高,弯曲模量大幅度提高而弯曲强度略有下降;随着高硅氧纤维含量的提高,材料的弯曲强度及弯曲模量均明显提高.  相似文献   

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