复合硅烷化预处理对铝合金/环氧胶粘剂粘接强度的影响

研究了铝合金表面复合硅烷化预处理对铝合金与环氧胶粘剂粘接强度和粘接耐久性的影响,并与铬酸盐预处理进行了比较。用反射吸收红外光谱和透射电镜分析观察铝合金表面复合硅烷化膜层的结构,分别用扫描电镜、X-射线光电子能谱和俄歇能谱分析了不同粘接件断裂表面。结果表明,铝合金经复合硅烷化预处理能明显提高铝合金基体与环氧胶粘剂的粘接强度和粘接耐久性。搭接件断面呈现一层层撕开的破坏现象,而铬酸盐处理的搭接断裂件的断面较平齐。硅烷化处理的楔子试样断裂件的断裂面也呈现明显的韧性断裂,表明在铝合金与胶粘剂界面区域形成的Al-O-Si和硅氧烷共价键网络和复合硅烷化膜层表面的环氧基团起着明显的界面和表面改性作用。     

改性环氧树脂光固化速粘胶的粘接应用研究

采用玻璃纤维布/光固化胶粘剂复合材料补片,实现对铝合金片的快速粘接与固化。考察了国产UV胶粘剂预聚物和进口UV胶的粘接性能、耐温性能以及粘接强度随胶粘剂相对分子质量及其分布的变化规律。结果表明:进口光固化胶/玻璃纤维布复合材料补片与铝合金片的剪切强度在14.5～23.1MPa之间,国产光固化胶体系剪切强度在11.3～16.6MPa之间,两者均高于铆接强度(10.3MPa);作为胶粘剂基体树脂,相对分子质量分布越宽越有利于粘接强度的提高;此外,-40℃低温与100℃高温对体系粘接强度的影响很小(不超过10%)。     

铝合金表面阳极化处理及其胶接性能分析

采用磷酸电解质对铝合金板进行了阳极化处理并测试了其胶接性能,测试了阳极化过程中铝合金板的基本力学性能,观察了阳极化处理后的铝合金板的表面形貌,分析了阳极化处理后铝合金粘接副的胶接界面、拉伸剪切失效模式.结果表明,铝合金板经过酸洗、碱洗和阳极化等过程后,其破坏强度、屈服强度、弹性模量和断裂延伸率等力学性能基本保持不变.阳极化后铝合金板表面形成了一层凹凸不平、多孔结构氧化膜,胶接时胶黏剂能渗透进入该氧化膜,形成一层胶接过渡层,阳极化处理提高了铝合金粘接副之间的拉伸剪切强度,其拉伸剪切强度最大可提高1.76倍.阳极化处理后的铝合金板粘接副之间的破坏模式为混合破坏,即存在胶黏剂的剪切破坏,同时存在粘接界面的剥离破坏.     

铝合金表面复合硅烷化处理

西北工业大学研究了铝合金表面复合硅烷化处理对铝合金与环氧胶粘剂粘接强度和粘接耐久性的影响，并与铬酸盐处理方法进行了对比。实验结果表明，在铝合金与环氧胶粘刘界面区域形成的Al-O-Si和硅氧炕共价键网络及复合硅烷化膜层表面的环氧基团，起着明显的界面和表面改性作用。     

铝合金表面粘接技术研究进展

综述了铝合金粘接技术的研究进展,介绍了作为粘接构件的铝合金在粘接前需进行的表面前处理方法,铝合金与橡胶粘接中胶粘剂的选用方法以及粘接工艺的操作,重点介绍了提高铝合金表面粘接性能的措施。     

国产水性胶和聚氨酯胶粘剂对地板布的粘接性能测试

选择两种国产水性胶（Ⅰ型和Ⅱ型）以及一种双组分聚氨酯胶粘剂,将地板布粘接到不同材质的地板上,即铝合金和木质地板,测试粘接剥离强度,对比分析了在不同地板基材上的粘接破坏形式。研究结果表明：Ⅰ型胶粘剂在铝合金和木地板上的剥离强度分别为1.182和1.731 N/mm,不但具有一定的粘接强度,还能满足动车组地板布拆除的要求,且适用于动车组导槽处地板布的粘接。而水性Ⅱ型胶在铝合金和木地板基材上的剥离强度值分别为0.355和1.172 N/mm,不适合作为动车地板布粘接胶。国产双组分聚氨酯胶在铝合金、木地板基材上的剥离强度分别为3.089和2.698 N/mm,均有较高的粘接强度,适合用作城轨车地板布胶粘剂。     

PTC陶瓷暖风机用导电胶的研制

选用高温树脂,研制导电胶粘接剂,用于PTC陶瓷片与铝合金散热片之问的粘接,能长期在260℃温度下使用,具有导电性能好、粘接强度高等特点,具有良好的应用前景。     

激光表面处理提高铝合金胶接接头强度的研究

粘接作为重要的汽车轻量化连接技术之一,胶接接头的强度和性能是我们关注的重点,胶接接头的强度和性能完全取决于胶粘剂接触的表面类型,因此在粘接之前对基材表面进行一定处理是粘接工艺中最重要的环节之一。金属的表面处理包括溶剂擦拭、机械打磨、化学清洗和酸蚀。激光表面处理是一种新型绿色环保的表面处理工艺,它可以高速有效的清洁材料表面附着物,并且改变材料表面微观结构及材料表面自由能及浸润性。从而提高粘接接头十字拉伸强度、单搭接拉伸剪切强度和接头耐水性能。通过激光处理,所有接头的破坏形式由界面破坏转为内聚破坏。对铝合金环氧结构胶2098G胶接接头而言,十字拉伸强度、剪切强度和水浴剪切强度,激光处理后比溶剂擦拭分别提高了17.8%,133.8%,88.1%。对铝合金聚氨酯结构胶TS6015胶接接头而言,十字拉伸强度、剪切强度和水浴剪切强度,激光处理后比溶剂擦拭分别提高了698%,225%,223%。激光表面处理有效的使铝合金胶接接头的强度达到胶的本体强度的94%~100%,是铝合金粘接的有效表面处理方法。     

磷酸–硫酸阳极氧化对铝合金表面粘接性能的影响

研究了磷酸–硫酸阳极氧化对铝合金2A50表面粘接性能的影响,并与喷砂处理进行比较。阳极氧化液组成与工艺条件为:磷酸70g/L,硫酸50g/L,草酸7g/L,甘油20g/L,温度(22±2)℃,电压20V,时间35min。采用扫描电镜观察经阳极氧化处理和经喷砂处理的铝合金表面、粘接界面、破坏界面的微观形貌,利用能谱仪分析阳极氧化膜的组成。结果表明,磷酸–硫酸阳极氧化可明显提高铝合金粘接副的拉伸剪切强度和粘接耐久性能。分析了磷酸–硫酸阳极氧化的成膜特点及电解液主要成分的作用,解释了阳极氧化处理后铝合金的粘接性能优于喷砂处理的原因。     

室温固化丙烯酸酯胶粘剂粘接性能的研究

室温固化丙烯酸酯胶粘剂应用范围广,需要粘接多种材料,并要在不同的环境条件下长期使用。考察了丙烯酸酯结构胶粘剂对多种金属和非金属材料的粘接强度,测试了不同种类介质条件下丙烯酸酯胶粘剂粘接试片的耐久性,扩展了丙烯酸酯胶粘剂粘接部件的应用环境范围。结果表明:丙烯酸酯胶粘剂粘接不锈钢、冷轧钢试片剪切强度分别为24.12MPa、29.30MPa;粘接PVC、ABS试片剪切强度分别为8.944MPa、6.642MPa;在-18℃冷冻1000h后,丙烯酸酯胶粘剂粘接铝合金、PVC试片剪切强度下降很小,强度保持率分别为92.93%、90.33%。     

提高RTV732硅酮胶剥离强度的试验研究

以RTV732单组分硅酮胶作为硅橡胶/铝合金粘接用胶粘剂,探讨了不同的固化条件对胶接件粘接性能的影响。结果表明:RTV732硅酮胶在不同固化条件下的剥离强度虽有所差异,但硅橡胶/铝合金胶接件经常温固化24 h、130℃固化2 h后的剥离强度明显优于常温固化24 h后的剥离强度。     

The effect of cataphoretic and powder coatings on the strength and failure modes of EN AW-5754 aluminium alloy adhesive joints

The aim of this study is to determine the effect of cataphoretic and powder coatings and also the method of application the primer on the adherends surface on the strength and failure modes of EN AW-5754 aluminium alloy adhesive joints. The study is performed on lap joints made of EN AW-5754 aluminium alloy, subjected to three different types of surface treatment; namely a) polyurethane cataphoretic coating, b) powder coating based on black mat RAL 9005 UL polyester resin and c) no coating. The tested adhesive joints were made using a one-component polyurethane adhesive Terostat 8596, which was dedicated for automotive and cured under a constant load of 0.018 MPa at 20 ± 2 °C. In addition, this study investigates the effect of the application of Terostat 8519P adhesion promoter which is a liquid polyurethane-based primer containing solvents and which is corresponding to Terostat 8596 polyurethane adhesive. Terostat 8519P adhesion promoter was applied in two different ways: a) to one substrate and b) to both substrates. The produced adhesive joints were subjected to strength tests using the Zwick/Roell Z150 testing machine. The examination of fracture in the tested adhesive joints was performed in accordance with the EN ISO 10365 standard. The shear strength results have demonstrated that both the method of application of the adhesion promoter (Terostat 8519 P) and the presence of cataphoretic coating had an influence on adhesive joints strength. The use of the adhesion promoter significantly affects the strength of both uncoated EN AW-5754 aluminium alloy adhesive joints and the adhesive joints subjected to powder coating. The use of the adhesion promoter has a less significant effect on the cataphoretic-coated samples.     

Glass/epoxy composites and aluminium alloy joint using Kevlar® intermediate layer and nanoclay-reinforced epoxy adhesive

Adhesive lap joint between glass fibre/epoxy composites and aluminium alloy (2014 T4) was prepared by an in situ moulding process using a matched die mould. The surface of aluminium alloy was treated with chromic acid before adhesive bonding. Lap shear strength and fatigue life were evaluated in tensile mode and tension–compression mode (at 40% of lap shear load of adhesive joint), respectively. Knurling on the surface of aluminium alloy improved the lap shear strength of the adhesive joint but did not influence the fatigue life of the same. Lap shear strength and fatigue life of adhesive joint made with neat epoxy adhesive and reinforcement of an intermediate layer of Kevlar^® between glass/epoxy composite and aluminium alloy were observed to be 0.44?kg/mm² and 3.6?×?10⁵ cycles, respectively. In another case, lap shear strength and fatigue life of similar type of adhesive joint made from nanoclay (Cloisite 30B)-reinforced epoxy adhesive and without reinforcement of an intermediate layer of Kevlar^® were observed to be 0.38?kg/mm² and 2.3?×?10⁵ cycles, respectively. Whereas, lap shear strength and fatigue life of adhesive joint made from nanoclay-reinforced epoxy adhesive along with the reinforcement of an intermediate layer of Kevlar^® were 0.48?kg/mm² and 3.9?×?10⁵ cycles, respectively. Therefore, adhesive joint made from nanoclay-reinforced epoxy adhesive along with the reinforcement of an intermediate layer of Kevlar^® was the best.     

CRH3高速动车组空调通风口胶接结构设计

通过理论分析和计算确定了动车组空调通风口部件与铝合金车体胶接用胶粘剂的强度指标。介绍了胶粘剂的选择及胶接结构的设计原则,考查了搭接长度、搭接宽度、胶层厚度和被粘接材料厚度等对胶接件粘接强度的影响。结果表明:车体与空调通风口部件的胶接接头选择受剪切应力作用的搭接接头较适宜,并且搭接接头的承载能力随搭接长度或宽度增加呈先快速上升后趋于稳定态势;当搭接长度为10 mm、胶层厚度为6 mm、铝合金板厚度为5 mm且常温湿固化型单组分PU(聚氨酯)胶粘剂的剪切强度超过0.23 MPa时,搭接接头的承载能力相对最大。     

低压缩永久变形氟橡胶与铝合金粘合的研究

研究ＫＨ５５０、ＫＨ５６０、Ａ－１５１三种硅烷偶联剂以及ＴＡＩＣ和２，５－二甲基－２，５－二叔丁基过氧己烷硫化助剂对低压缩永久变形氟橡胶胶料硫化的影响，分析了上述五种材料有机官能团参与交联反应的活性。采用以ＫＨ５６０为主配制的胶粘剂可良好地将铝合金与低压缩永久变形氟橡胶粘接，同时对铝合金表面的处理作了一定的研究，解决了目前快速硫化的低压缩永久变形氟橡胶与铝合金粘接的难点。     

The effect of water on the adhesion of organic coatings on aluminium

Water normally decreases the strength of adhesive joints. In the case of epoxy coatings on aluminium, however, after an initial decrease the adhesive strength increased with the time of exposure to water. It is suggested that this increase is caused by the hydration of aluminium oxide adjacent to the adhesive joint, thus enabling additional hydrogen bonding between the organic coating and its support.

Results obtained by measuring adhesion with peel and tape tests on aluminium foil and an alloy with different surface pretreatments and different curing conditions have been compared. It is shown that the tape test is useful for the semi-quantitative determination of the stability towards water of an adhesive joint.     

Study on the fatigue strength of AA 6082-T6 adhesive lap joints

A research study on the fatigue behaviour of aluminium alloy adhesive lap joints was carried out to understand the effect of surface pre-treatment and adherends thickness on the fatigue strength of adhesive joints. The adherend material used for the experimental tests was an aluminium alloy 6082-T6 in the form of thin sheets, and the adhesive used was a high strength epoxy (Araldite 420 A/B). The surface preparation included an abrasive preparation (AP joints) and sodium dichromate–sulphuric acid etch (CSA joints).A maximum fatigue strength was obtained for the CSA surface treatment with a 1.0 mm adherends’ thickness. The fastest fatigue damage was related with a high surface roughness and a high stress perpendicular to adhesive surface, which helps to promote the adhesive failure. A numerical analysis was also performed to understand the effect of the adherends thickness on the stress level. Results showed an increase of the out-of-plane peak stresses with the increase of adherends thickness.     

Effect of surface pre-treatment on the adhesive strength of epoxy–aluminium joints

A detailed study of the effect of pre-treatment applied on the surface characteristics of aluminium substrates and on the adhesive strength of epoxy–aluminium joints is reported. The variation of the density, composition and aspect of the adherends were analysed as a function of the applied pre-treatment. In order to determine the influence of alloying elements, two different aluminium alloys were used, A1050 and A2024. The adhesive strength was measured by the lap shear test, using several epoxy resins to analyse the influence of the adhesive nature.A chromate-free treatment based on the sulphuric acid-ferric sulphate etch provided an improved joint strength compared to dichromate-sulphuric acid etching, alkaline etching or mechanical abrasion. This increase is associated to the porous oxide layer formed, but it depends on the adhesive nature used. The joints with Al–Cu–Mg alloy substrates generally presented higher adhesive strength values than those with pure aluminium adherends, due to the selective etching of some allowing elements and intermetallic compounds, which have different electrochemical potential.     

Effect of surface pre-treatment on surface characteristics and adhesive bond strength of aluminium alloy

In this work aluminium alloy surfaces have been subjected to three different methods of surface pre-treatments such as solvent degreasing, FPL (Forest Products Laboratory) etching and priming using an epoxy based primer. The treated surfaces were evaluated for surface energy, contact angle, surface topography, surface roughness and adhesive strength characteristics. The influence of surface pre-treatments on the variation of polar, dispersive and total surface energy of the surfaces is addressed. A wettability test was performed on the surfaces using an epoxy adhesive in order to assess the influence of the pre-treatment techniques on substrate/adhesive interaction. Theoretical work of adhesion values for the various pre-treated surfaces were calculated using the contact angle data and further tested experimentally by adhesive bond strength evaluation by tensile testing of a single lap aluminium-epoxy-aluminium assembly. The method of surface pre-treatment showed a profound effect on the surface topography and roughness by AFM. This study reveals that a combination of high surface energy and high surface roughness of the substrate along with good wettability of the adhesive contributed to the highest joint strength for the aluminium alloy through the FPL etching pre-treatment.     

J-125铝合金复合层板结构胶膜的研制

介绍了J-12 5改性环氧结构胶膜的基本组成和固化条件 ,并讨论了各组成及固化参数对胶粘剂力学性能的影响。该胶具有良好的综合性能 ,可广泛应用于铝合金层板胶接结构。