多壁碳纳米管改性环氧树脂胶黏剂实验研究

将一种环氧树脂和表面羟基化的多壁碳纳米管(MWCNTs)按照质量比100∶0.1进行配比, 以超声波分散法制备MWCNTs/环氧树脂胶黏剂, 考察了两种硅烷偶联剂KH550和KH560对MWCNTs改性效果的影响。采用FTIR、 DSC、 DMA、 流变仪研究了MWCNTs对胶黏剂固化行为和流变特性的影响, 并结合断口形貌观察, 测试分析了MWCNTs对胶黏剂拉伸剪切强度和冲击强度的影响。结果表明: 硅烷偶联剂能与MWCNTs表面的羟基发生缩合反应, 增强了MWCNTs与环氧树脂基体的亲和性, 从而影响胶黏剂固化反应及黏度-剪切速率曲线; 经KH550改性的MWCNTs明显提高了胶黏剂与金属的界面粘结性, Al-Al拉伸剪切强度较无MWCNTs的胶黏剂提高了46.4%; 添加MWCNTs使胶黏剂的冲击断面更为粗糙, 开裂面积更大; 添加MWCNTs+KH550的胶黏剂冲击强度提高了44.1%, 说明MWCNTs/环氧树脂间界面性能对发挥MWCNTs的增韧效果非常重要。      

固化剂混掺对高温下CFRP板-钢板界面黏结性能的影响

针对单一固化剂难以兼顾耐热性和韧性的不足,研究了耐热性能较好的缩胺105和韧性较好的聚醚胺D230两种固化剂混掺对纳米SiO₂环氧胶黏剂玻璃转变温度及高温下基本力学性能的影响。按一定固化条件制作了30个胶黏剂拉伸试件、21个碳纤维增强树脂复合材料(CFRP)板-钢板双搭接试件,进行了高温及常温下的准静态拉伸试验、拉伸剪切试验,测试了相应胶黏剂的动态热机械性能,并与常用商品胶的耐热性能与力学性能进行比较,得到以下结论:随混掺固化剂中聚醚胺D230比重的增加,胶黏剂高温下的拉伸强度及弹性模量逐渐降低,断裂伸长率及应变能先增加后减小,缩胺105与聚醚胺D230两种固化剂混掺的推荐比例为1∶2。随固化温度的升高,具有固化剂混掺较佳比例的胶黏剂的玻璃转变温度有所提升,综合技术与经济因素,推荐(较佳)固化条件为90℃、2 h。推荐比例与推荐固化条件的纳米SiO₂环氧胶黏剂在环境温度20~70℃之间的拉伸强度及韧性均大大优于常用商品胶黏剂。基于推荐比例与推荐固化工艺的纳米SiO₂胶黏剂粘结的CFRP板-钢板搭接接头,在70℃服役温度下的荷载-位移曲线存在屈服段,承载能力(较采用单一缩胺105和单一聚醚胺D230固化剂的搭接试件分别提升了104.03%、64.43%)和延性(为采用单一缩胺105固化剂的搭接试件的2.5倍以上)均大幅提升。高温和常温下的黏结-滑移本构均为三线性四边形。胶黏剂在满足耐热性的同时,需尽可能提升其韧性,才能有效提升CFRP-钢搭接界面的力学性能。相比于常用商品胶黏剂,研制的推荐胶黏剂粘结的CFRP板-钢板搭接接头具有优越得多的承载能力和界面断裂能。      

端氨基液体丁腈橡胶/环氧树脂绝缘胶黏剂的制备与性能EI北大核心CSCD

介绍了一种端氨基液体丁腈橡胶(ATBN)增韧改性环氧树脂(EP)的绝缘胶黏剂;借助红外光谱表征胶黏剂固化前后的分子结构变化;通过拉伸与T剥离强度测试表征胶黏剂的黏接性能,借助弯曲与冲击强度测试及冲击断面扫描电镜照片进一步解释胶黏剂的黏接特性;通过击穿场强、体积电阻率以及介电性能测试考核胶黏剂的绝缘性能。研究发现,ATBN分子结构中的活性基团参与了胶黏剂的固化反应;当ATBN添加量为EP的20%时,胶黏剂的拉伸和T剥离强度达到4.92 MPa和9.87 N/mm,分别较纯EP体系提高77%和98%;在此添加量下弯曲强度为113 MPa,冲击强度为18.73kJ/m^2,体积电阻率为1.54×10^(14)Ω·m,击穿场强为25 kV/mm,工频下介电常数为4.53,介电损耗为0.0148。     

端氨基液体丁腈橡胶/环氧树脂绝缘胶黏剂的制备与性能

介绍了一种端氨基液体丁腈橡胶(ATBN)增韧改性环氧树脂(EP)的绝缘胶黏剂;借助红外光谱表征胶黏剂固化前后的分子结构变化;通过拉伸与T剥离强度测试表征胶黏剂的黏接性能,借助弯曲与冲击强度测试及冲击断面扫描电镜照片进一步解释胶黏剂的黏接特性;通过击穿场强、体积电阻率以及介电性能测试考核胶黏剂的绝缘性能。研究发现,ATBN分子结构中的活性基团参与了胶黏剂的固化反应;当ATBN添加量为EP的20%时,胶黏剂的拉伸和T剥离强度达到4.92 MPa和9.87 N/mm,分别较纯EP体系提高77%和98%;在此添加量下弯曲强度为113 MPa,冲击强度为18.73kJ/m~2,体积电阻率为1.54×10~(14)Ω·m,击穿场强为25 kV/mm,工频下介电常数为4.53,介电损耗为0.0148。     

磷酸盐溶液中碳纤维表面电化学改性

对比研究(NH₄)₂HPO₄和NH₄H₂PO₄两种不同电解质对碳纤维电化学改性效果的影响。通过拉丁方试验,研究了各改性参数对纤维表面改性效果的影响程度,采用XPS、AFM、BET技术对纤维表面化学组成、形貌及其比表面积的变化进行了表征分析。结果表明:以(NH₄)₂HPO₄为电解质处理时改性效果主要受相对电流密度的影响,而以NH₄H₂PO₄为电解质时电解液浓度是最主要的影响因素;在(NH₄)₂HPO₄电解液中,纤维表面氧化刻蚀温和,改性效果显著,层间剪切强度可提高到79.8MPa,而在NH₄H₂PO₄电解液中,纤维表面受到较强烈氧化刻蚀,本体强度损失较大,复合材料层间剪切强度仅能提高到70.8MPa。      

纳米SiO2质量分数对胶粘碳纤维增强树脂复合材料板-钢搭接界面黏结性能的影响

胶黏剂力学性能对碳纤维增强树脂复合材料(CFRP)加固钢结构的界面黏结性能影响显著。基于研制的胶黏剂配比,分析了不同纳米SiO₂质量分数对胶黏剂常温固化后基本力学性能及微观结构的影响,制作了31个CFRP板-钢板双搭接试件,对其进行了常温固化后的承载能力、有效黏结长度、传力模式、黏结-滑移本构等试验研究,得出了纳米SiO₂质量分数对CFRP板-钢板搭接试件界面黏结性能的影响规律,并与常用商品胶黏剂进行了比较。研究结果表明:随纳米SiO₂质量分数的增加,胶黏剂应力-应变关系由线性转变为非线性,应变能、断裂伸长率及剪切强度分别最高提升了292.10%、202.88%和133.12%。微观结构分析表明纳米SiO₂的添加使断面粗糙度显著增加,形成了密集的塑性空穴,产生了更多的微裂纹,使胶黏剂的韧性大幅度提高。当纳米SiO₂质量分数从0增至1wt%,搭接试件破坏模式由界面破坏逐渐变为CFRP板层离破坏。掺入纳米SiO₂能显著增加搭接试件的极限承载力(提升256.96%)及界面有效黏结长度(提升3倍),提高CFRP表面的应变及界面剪应力峰值。纳米SiO₂质量分数为0与0.5wt%的搭接试件的黏结-滑移曲线为双线性三角形模型,纳米SiO₂质量分数为1wt%的搭接试件的黏结-滑移曲线为三线性梯形模型,黏结界面韧性大幅提升。CFRP-钢界面承载能力受胶黏剂拉伸强度与断裂伸长率的双重影响,非线性高强度(即具有较高应变能)胶黏剂对应的CFRP-钢搭接接头具有更好的界面性能。      

铝合金-BFRP粘接接头的服役高温老化力学性能及失效预测EI北大核心CSCD

选取50℃和80℃的高温老化环境,结合设计的测试夹具测得高温老化0,10,20,30天后铝合金-BFRP(玄武岩纤维增强树脂基复合材料)粘接接头在1 mm/min加载速率下的准静态抗拉强度与剪切强度,并对接头的失效断面进行宏观分析。结果表明:80℃高温老化后,胶黏剂发生后固化反应,力学性能增强,BFRP发生化学键断裂,玻璃化转变温度(T g)降低;老化30天后,接头的抗拉强度下降,剪切强度上升;30天后拉伸接头失效断面出现分层,剪切接头出现胶层内聚与纤维撕裂的混合失效;50℃高温老化后,胶黏剂的力学性能略微上升,拉伸接头的失效强度变化不大,失效模式以纤维撕裂和分层为主;剪切接头的失效强度略微上升,失效模式以胶层内聚为主。根据二次应力准则对抗拉强度和剪切强度进行曲线拟合;根据响应面原理,建立失效准则随老化时间的响应面方程,用以对铝合金-BFRP粘接结构胶层的裂纹产生和扩展进行预测。     

MWCNTs对环氧树脂及多尺度MWCNTs-碳纤维/环氧树脂复合材料力学性能的影响

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%。     

白炭黑补强环氧化溶聚丁苯橡胶

为探究环氧化对白炭黑(SiO₂粒子)在溶聚丁苯橡胶(SSBR)基体中分散性的作用,首先,以SSBR和环氧化溶聚丁苯橡胶(ESSBR)为基体,白炭黑为补强填料,分别制备了SiO₂/SSBR、SiO₂/ESSBR混炼胶和硫化胶;然后,采用FTIR、SEM和其他测试方法研究了材料的结构、形貌、硫化特性、耐磨性能、准静态力学性能和动态力学性能。结果表明:随环氧度从0增大到14.73%,生胶的门尼黏度增大。ESSBR分子链中的环氧基团与SiO₂粒子表面的硅羟基反应形成稳定的化学键,抑制SiO₂粒子团聚,促进其均匀分散;当环氧度为6.87%时, SiO₂粒子在ESSBR中的分散性最好。随环氧度增大, SiO₂/ESSBR硫化胶的拉伸强度先增大后减小、耐磨性能先增强后减弱、断裂伸长率降低、100%和300%定伸强度增大、玻璃化转变温度升高、0℃时的损耗因子显著增大、抗湿滑性增强、60℃时的损耗因子略有增加且滚动阻力增大。因此, SSBR硫化胶经环氧化改性后综合性能提高,当其环氧度在6.87%~8.51%范围内时, SiO₂/ESSBR硫化胶的综合性能最优。      

铺层方式对CFRP-铝合金单搭接胶接接头低速冲击损伤及剩余拉伸性能的影响

采用热压罐成型方法制备铺层方式为[+45/-45]_4s、[0/+45/-45/90]_2s和[0/90]_4s的碳纤维复合材料层合板,通过胶黏剂与铝合金板进行粘接获得异质材料单搭接胶接接头。利用落锤冲击试验机和万能电子试验机分别对三种接头进行低速冲击与冲击后静态拉伸测试,获得接头接触力-时间曲线和拉伸强度。通过CT扫描技术和数字图像相关(DIC)方法表征接头冲击损伤模式及表面应变演化过程,研究了铺层方式对接头抗冲击性能、冲击损伤模式以及剩余拉伸性能的影响。结果表明,复合材料铺层方式为[+45/-45]_4s时,接头在冲击载荷作用下具有较高的抗冲击性能,但胶层界面脱粘损伤较为严重。与胶层界面脱粘相比,接头剩余强度对层合板分层损伤更为敏感。相较于[+45/-45]_4s,[0/+45/-45/90]_2s和[0/90]_4s铺层方式接头的胶层界面脱粘范围与冲击后失效载荷退化程度较小,同时接头冲击后拉伸载荷主要集中于临近胶层的0°铺层且失效模式较为复杂...     

服役低温老化对铝合金-玄武岩纤维增强树脂复合材料粘接接头力学性能的影响及失效预测

为了给铝合金-玄武岩纤维增强树脂(BFRP)复合材料粘接结构在汽车工业中的应用提供参考和指导,加工了铝合金-BFRP复合材料粘接接头。结合汽车服役中的温度区间,选取?10℃和?40℃的低温老化环境,对接头进行0、10、20、30天的老化。对老化后的粘接接头进行准静态拉伸试验和剪切试验,得到不同老化时间下铝合金-BFRP粘接接头的准静态失效强度。结合DSC和FTIR分析低温老化对BFRP复合材料的影响,并对粘接接头的失效断面进行宏观分析和SEM分析。结果表明:在低温老化环境中,胶粘剂与BFRP复合材料的化学性质受低温老化作用影响不大,BFRP中的官能团与玻璃化转变温度(T_g)没有发生明显的变化,接头的失效强度和失效模式主要受胶粘剂与粘接基材的热应力影响。对于拉伸接头,随着低温老化时间的增加,BFRP复合材料纤维与树脂基体间的结合力降低,铝合金-BFRP复合材料接头的失效断面中纤维撕裂的比例逐渐减少,拉伸接头失效强度逐渐下降。老化后剪切接头仍为内聚失效,BFRP复合材料的低温老化对铝合金-BFRP复合材料剪切接头的失效强度几乎没有影响,剪切接头失效强度的下降主要是胶粘剂与粘接基材热膨胀系数不一致引起的热应力的影响。采用二次应力准则公式对?10℃和?40℃低温环境下,拉应力、剪应力值随老化时间的变化规律进行了拟合,在此失效准则的基础上,根据响应面原理,建立接头失效强度随老化时间变化的三维曲面,为粘接技术在车身结构中的工程应用提供参考。      

基于遗传算法的碳纤维增强树脂复合材料层合板单搭胶接结构的多目标优化

基于遗传算法对碳纤维增强树脂复合材料(CFRP)层合板单搭胶接结构进行了多目标优化,以提高其结构性能.首先,通过三维Hashin准则和三角形内聚力模型建立三维有限元模型来预测CFRP层内损伤过程、层间失效和胶层损伤过程,并通过试验验证其有效性.其次,利用拉丁超立方抽样(LHS)方法和二次多项式响应面法(RSM),基于搭...     

Chemical functionalization of composite surfaces for improved structural bonded repairs

In terms of lightweight design, aerodynamics and structural integrity, bonded repairs represent the preferred approach for repairing composite structures in aircraft applications. In this work the influence of crucial surface parameters including roughness, polarity and chemical composition on the performance of bonded repairs is studied. Besides mechanical and physical interactions, the study aims at the surface modification of carbon-fiber reinforced polymers (CFRP) to tailor chemical interactions with the adhesive. Reactive epoxy and mercapto derivatives are attached onto the CFRP surface by a 2-step functionalization route to ensure optimized adhesion and covalent bonding to epoxy-based adhesives. The performance of bonded coupon joints is determined by single lap shear tests (tensile-shear loading) and fracture mechanical tests (mode I loading). The results give evidence that chemical interactions play a key role in the quality of bonded repair systems. By controlling the chemical surface properties improved bond strength, homogenous crack growth and cohesive failure patterns are achieved.     

Investigation of the effect of different variables on strength of adhesive joints

In this article, the tensile strength of different adhesive bonded joints under a tensile load was analyzed numerically. The effects of certain parameters, including the bonding length and bonding ratio, were investigated. For this reason, the epoxy adhesive was used. Joints were prepared with aluminum materials. The stress analyses were employed using the Finite Element Method (FEM). ANSYS (v.14.0.1) FEM tool was utilized to investigate the stress distribution characteristics of aluminum lap joint under tensile loading. Numerical results were found to be quite reasonable. The numerical results show that the influences of variations are very notable when the equivalent stresses are between 18 MPa and 20 MPa.     

Shear induced toughening in bonded joints: experiments and analysis

Bonded joint specimens were fabricated from composite adherends and either an epoxy or a urethane adhesive. In mixed-mode fracture experiments, the epoxy bonded specimens generally failed by subinterfacial fracture in the composite, while specimens bonded with urethane failed very close to the adhesive/substrate interface. For the epoxy bonded specimens, fracture toughness did not change significantly with mode-mix, but for urethane bonded joints, fracture toughness increased with increasing shear load. Finite element analysis, which modeled specimens bonded with the two adhesives, showed similar trends. The different toughening behaviors for the two bonded joints can be attributed to dissipation of energy through inelastic deformation, which was insignificant in the epoxy-bonded joints but substantial when the urethane was used as the bonding agent.     

Short-aramid-fiber toughening of epoxy adhesive joint between carbon fiber composites and metal substrates with different surface morphology

Carbon-fiber epoxy composites were bonded to four different types of aluminum substrates with different surface roughness and finish. The four aluminum substrates considered in this study have the following surface conditions: two solid aluminum substrates polished with two different grades of sandpapers, and two porous aluminum foams with two different as-received surface conditions, one with a patterned surface finish and one with rough pore structures. Moreover, the thin epoxy adhesive joints between the carbon-fiber face sheets and aluminum substrates were reinforced by adding short aramid fibers. During the fabrication process of the hybrid laminar, sparsely-distributed short aramid fibers were inserted between the fiber-metal interface to promote bridged fibers for tougher and stronger adhesive bonding, while at the same time to minimize any significant change in the thickness of the adhesive joint. Measurements of the critical energy release rate showed that the toughening effects of the low-density short aramid fibers were influenced by the metal-substrate surface roughness and finish. Further comparison indicated that the interfacial fracture toughness of aramid-fiber interleave adhesive joints increased via increase of surface roughness of metal substrates. The surface-roughness effect of metal substrate mainly depends on whether the free fiber ends of the short aramid fibers were pressed and embedded into the surface cavities of aluminum substrates according to scanning electron microscopy observations. The results indicated that the properties and performances of aramid-fiber interleaved adhesive joints between the carbon-fiber face sheets and aluminum substrates could be improved by surface treatments on the aluminum substrates to achieve appropriately surface roughness.     

基于激光毛化的铝合金/CFRTP激光连接特性研究

目的 针对目前铝合金和碳纤维增强热塑性复合材料(CFRTP)直接连接接头强度低的问题,对铝合金表面进行预处理,以提升异种材料的激光连接强度。方法 通过激光毛化工艺在铝合金表面预制微织构,然后利用光纤激光连接铝合金与CFRTP,研究了激光焊接工艺参数对铝合金与CFRTP焊接接头拉剪性能的影响。结果 当激光功率为750 W、焊接速度为0.2 m/min时,铝合金/CFRTP接头拉剪力达到最大值5 209 N,是未激光毛化的接头拉剪力的2.29倍。通过扫描电镜(SEM)对断口进行分析,发现界面断裂形式主要为CFRTP脱出和剪切断裂。采用SEM及能谱仪(EDS)对接头截面进行分析,发现结合界面处存在微观机械嵌合作用,同时在界面处存在元素过渡层。结论 随着激光功率的增大,焊接接头的拉剪力增大,但焊接功率较大会导致热输入过大,造成树脂发生热分解,导致焊接接头拉剪力降低。随着焊接速度的增大,焊接热输入降低,导致焊接过程中树脂熔化量减少,焊接接头的拉剪力降低。界面的机械嵌合作用使焊接接头具有较高的结合强度。     

AA5052薄板磁脉冲胶焊复合接头动态力学性能研究

目的 研究AA5052铝合金薄板在高速冲击载荷下的磁脉冲胶焊复合接头的动态力学性能,探究不同载荷速率对该胶焊复合接头力学和失效行为的影响规律.方法 利用磁脉冲焊接系统成功制备了胶焊复合连接试件.采用万能拉伸试验机、高速拉伸试验系统,结合全场应变测量系统,获得胶焊复合接头的力学性能规律,以及渐进失效过程和搭接区应变变化....     

搭接长度和铺层方式对CFRP复合材料层合板胶接结构连接性能和损伤行为的影响

针对不同搭接长度和铺层方式的碳纤维增强树脂（CFRP）复合材料层合板单搭胶接结构进行了拉伸试验,观察了试件的受力过程和失效形态,获得了载荷-位移曲线;同时基于连续损伤力学模型和三维Hashin失效准则模拟了CFRP复合材料层合板的层内损伤形成和演化,并利用内聚力模型来模拟层间及胶层的失效损伤,对CFRP复合材料层合板单搭胶接结构在拉伸作用下的失效强度和损伤机制进行了预测,通过对比验证了该数值方法的有效性;通过数值试验比较不同搭接长度和铺层方式的单搭胶接结构及双搭胶接结构的连接强度和损伤行为,并提出了一种优化的CFRP复合材料层合板胶接结构。结果表明:CFRP复合材料层合板胶接结构的极限失效载荷随着搭接长度的增大逐渐增加并趋于稳定值,且结构的失效形式逐渐从胶层自身剪切失效过渡到邻近胶层的层合板层间分层失效;CFRP复合材料层合板胶接结构的连接强度和损伤行为随着铺层方式的不同而改变,通过对3种铺层方式的对比和分析,得到性能最好的铺层方式是[0₃/90₃]_2S;在搭接长度为5~20 mm时,通过对搭接长度进行优化,得到单搭胶接结构的最优搭接长度是17 mm,双搭胶接结构的最优搭接长度是19.3 mm,与搭接长度为20 mm相比,单搭胶接结构和双搭胶接结构的连接强度分别提高了13.26%和0.43%。      

Experimental and numerical investigation of the influence of imperfect bonding on the strength of NCF double-lap shear joints

The influence of imperfect bonding, owing to partial lack of adhesive, on the strength of composite non-crimp fabric (NCF) double-lap shear (DLS) joints was experimentally and numerically investigated. Fabrics were layered and compacted using a thermoplastic veil while infiltration of the preforms was done using the vacuum assisted process. Paste adhesive bonding was carried out by implementing the novel insertion squeeze flow process. Quality of adhesive bonding was tested using X-ray imaging and ultrasonic C-scan inspection. The tensile lap shear strength of the DLS joints was determined experimentally. Digital macrographs revealed that the specimens failed due to shear failure of the adhesive (debonding) and fracture of the composite boundary layer. As a second approach, a mesomechanical model based on the FE method and the (homogenized) progressive failure analysis method was developed. In the model, the areas without adhesion, as detected by the C-scans, were included. Numerical simulations of failure initiation and progression at the NCF joint and the adhesive indicated that it is possible to predict the strength and failure mechanisms of the imperfect bonded DLS joints.