粘接剂对1420铝锂合金压印接头疲劳性能的影响

压印连接以高效率、低能耗的优点在薄板材料连接中被广泛应用,但其连接强度相对较低,鉴于此,压印-粘接复合连接应运而生。本文以1420铝锂合金为原材料,制备了1420同种材料组合的压印接头及压印-粘接复合接头并进行对比。通过拉-剪静态力学试验测定两种接头的静力学强度及承载能力,通过拉-拉动态疲劳试验测定两种接头的动态疲劳性能,采用三参数法拟合疲劳寿命曲线,并对疲劳失效断口进行分析。结果表明:压-粘接头的静强度比压印接头提高了108.17%,接头承载能力提高169.63%。在短寿命区,两种接头均为颈部断裂失效;在中长疲劳寿命区,压-粘接头的疲劳寿命优于压印接头,压-粘接头疲劳断裂位置为压印点,压印接头疲劳断裂位置为下板。对疲劳断口进行SEM分析,发现两组疲劳断口均呈现韧性断裂与脆性断裂同时出现的特征。     

泡沫金属三明治结构压印-粘接复合接头剥离性能分析

为研究三明治结构压印-粘接复合接头的抗剥离性能,选取AA5052铝合金板以及泡沫镍、泡沫铜以及泡沫铁镍进行压印-粘接复合连接,对接头进行拉伸剪切试验,采用扫描电镜对失效断口进行了观察,分析了接头的失效形式、失效载荷、能量吸收值以及失效机理。结果表明:夹层的存在会使接头中胶层的失效过程更加稳定,夹层对于压印-粘接复合接头的承载能力并无显著影响,但是会降低其失效过程中的能量吸收值。     

粘接剂对自冲铆-粘接复合接头强度的影响及数理统计分析

以自冲铆接和自冲铆-粘接复合接头为对象,采用数理统计分析检验实验数据合理性,进而对比不同材料组合及连接方式来分析粘接剂对自冲铆接接头强度的影响。实验表明,自冲铆接的剪切强度比剥离强度高;粘接剂对异种材料组合(硬质材料置于上板)自冲铆接的影响较同种材料组合自冲铆接更显著;异种材料组合(硬质材料置于上板)自冲铆-粘接复合技术,采用胶层厚度为0.1mm时,可获得有效的连接结构且具有良好的承载能力;T型异种材料组合压印连接吸震、缓冲效果更好。     

钛铝合金板材压印成形及接头力学性能实验研究

对钛合金(TA1)和铝合金(Al5052)板材组合进行压印连接的可行性进行了研究,发现压印连接可以有效地实现TA1-TA1组合和Al5052-TA1组合的连接。对所获得的接头进行准静态力学性能测试,并运用扫描电子显微镜对接头拉伸断口进行微观分析。结果表明,压印连接时,钛合金和铝合金的组合能够获得成形性较好的压印接头,TA1-TA1接头的最大载荷和失效位移较Al5052-TA1接头提高了303.8%和49.4%,这两种接头静态失效形式相似,为上板颈部材料首先被破坏,产生裂纹,之后裂纹沿周向逐渐扩展,最终导致整个压印接头断裂。由微观断口可以判断TAl-TA1接头断口处呈现准解理和韧窝形貌,即同时具有韧性断裂和脆性断裂的特征;Al5052-TA1接头断口处呈现直径和深度较大的拉长韧窝,即为韧性断裂。     

钛合金压印接头疲劳性能与微观分析

压印连接是近年来新兴的连接方式,因其具有简单高效、低耗环保等优点,在连接应用方面越来越受到重视,而疲劳破坏是机械零件失效的主要形式。对钛合金压印接头的疲劳性能进行了实验研究,与母材的力学性能进行了对比分析,并对疲劳失效断口进行了断口分析和能谱分析。实验结果显示钛合金压印接头的平均拉伸-剪切强度约为同等尺寸材料拉伸-剪切强度的36.7%;钛合金压印接头的疲劳极限约为材料疲劳极限的46%,平均载荷约为接头最大静强度的42%。微观特征显示断口呈脆性疲劳断裂特征,由于微动磨损和氧化作用产生了成分为氧化钛的微动磨屑,且其硬度较高,因此在微动过程中起到磨粒的作用,从而加速了磨损和裂纹扩展,最终导致疲劳失效。     

三层板压印接头力学性能分析

本文的研究目的是分析三层板不同搭接方式的压印接头的力学性能,主要采用试验方法对其进行研究,具体方法如下:首先对1.5 mm AA5052+1.5 mm SPCC+1.5 mm AA5052三层板不同配置方式下的压印接头进行静态力学性能测试,分析三层板压印接头的静态失效模式及其静强度;再对静态力学性能最优组进行动态疲劳性能测试,分析疲劳失效模式及其疲劳强度,并采用最小二乘法拟合获得接头力-寿命(F-N)方程.试验结果表明:静态失效为上板颈部断裂、中板内锁拉脱和混合失效三种模式;T-A型接头静强度最低,T-C型接头静强度最高.其中,T-C型接头疲劳失效模式为上板颈部先断裂,之后下板出现裂纹导致接头失效;T-C型接头上板颈部疲劳性能较差,当应力水平为静强度40%时,疲劳循环最多只能达到15 965次,但是中板与下板连接可达到200万次.     

压印接头力学分析及预成角对接头强度的影响研究

从宏观和微观两方面对压印接头强度进行了研究,通过对压印连接拉伸过程动态模拟和在显微镜下观察到的裂纹形成的主要位置,分析了拉伸过程中裂纹的萌生、扩展直至整个压印接头颈部断裂的过程;对压印接头进行了显微组织分析,得出薄板经冲压后产生了加工硬化现象,接头强度得到提高.提出了预测压印接头最大破坏力的公式,对生产中模具的选取及样品强度的预测具有一定的指导意义.同时,对不同预成角度的压印连接试件进行了拉伸试验,得出0°压印接头能够承受的拉伸破坏力最大,且预成角越大,压印接头能承受的破坏力越小.     

压印连接接头的疲劳裂纹扩展分析及实验研究

研究了压印连接接头的强度性能,介绍了压印连接成形原理和工艺过程。分析了压印连接接头的表面裂纹的产生原因,通过有限元分析得出最大应力应变的位置并以实验加以验证。采用ANSYS/LS-DYNA有限元软件对压印连接接头疲劳裂纹扩展进行数值模拟。分析了平均应力、应力比和加载频率对压印连接接头的疲劳裂纹扩展速率的影响。     

金属-聚合物及金属-复合材料薄壁结构压印连接技术的研究进展

随着结构轻量化需求的增加，金属-聚合物及金属-复合材料薄壁结构在交通运输和航空航天等多个领域得到广泛应用。压印连接具有高效、节能环保和成本低等优势，为异种材料的连接提供了解决方案。由于聚合物及其复合材料延展性较差，为了减小接头的成形损伤、提高连接效率及接头的力学性能，一些改进的连接工艺相继被提出。为了推动压印连接的工程应用，本文综述了金属-聚合物及金属-复合材料薄壁结构的压印连接技术，对各连接工艺的适用性、成形工艺方法、成形质量影响因素和接头力学性能进行探讨。最后，针对连接工艺设计中亟待解决的问题，展望了压印连接技术的研究方向。     

局部热处理对不同模具压印接头静力性能影响分析

首先对同种基板不同压印模具的压印连接接头进行局部热处理,然后再进行拉剪试验,研究局部热处理对不同模具压印连接接头的抗拉强度、失效位移、能量吸收能力以及失效模式的影响。结果表明:局部热处理对方形与圆形模具压印连接接头的抗拉强度均有提升作用;对方形模具的失效位移有增大作用,对圆形模具失效位移有减小作用;对能量吸收能力均有提高作用。失效模式也受到局部热处理影响,方模与圆模压印接头经局部热处理后颈部被撕裂程度都增大,其中圆模压印接头经热处理后失效模式由内锁拉脱失效变为颈部断裂失效。     

Failure mode and strength of uni-directional composite single lap bonded joints with different bonding methods

Failure process, mode and strength of unidirectional composite single lap bonded joints were investigated experimentally with respect to bonding methods, that is, co-curing with or without adhesive and secondary bonding. The co-cured joint specimen without adhesive had the highest failure strength. Progressive failures along an adhesive layer occurred in the secondary bonded specimen. In the co-cured specimen with adhesive film, delamination failure occurred and the joint strength was lower than that of secondary bonded specimens. Delamination failure did not occur in the secondary bonded specimen because of early crack growth and progressive failure in the adhesive layer. Therefore, The failure strength of composite bonded joint is not always proportionate to adhesion strength of adhesive due to the weakness of delamination in composite materials. The influences of surface roughness, bondline thickness and fillets in the secondary bonded specimens were also studied.     

Fatigue properties of combined friction stir and adhesively bonded AA6082‐T6 overlap joints

Even though friction stir welding (FSW) has been shown to produce high performing butt joints, stress concentration at the weld edges in overlap FSW significantly reduces the performance of these joints. By combining FSW and adhesive bonding into a friction stir (FS) weld bonding, joint mechanical performance is greatly improved. Quasistatic and fatigue strength of the proposed FS weld‐bonding joints was assessed and benchmarked against overlap FSW and adhesive bonding. The characterization of the structural adhesive is also presented, including differential scanning calorimetry (DSC) and thermogravimetric analysis (TGA), as well as mechanical characterization with curing temperature. A small process parameter study was made to select proper FSW parameters for AA6082‐T6 overlap FSW and FS weld‐bonded joints. FS weld bonding achieved a significant increase in quasistatic and fatigue strength when compared with overlap FSW, with 79.9% of the fatigue strength of adhesive‐bonded joints at 10⁶ cycles, whereas FSW had 41.6%.     

Fatigue performance of hybrid overlap friction stir welding and adhesive bonding of an Al‐Mg‐Cu alloy

The need for weight reduction and leaner manufacturing and assembly processes in aircraft construction has led to the pursuit of welding technologies. One such technology that has been considered for this application is friction stir welding (FSW). Since it is a solid‐state joining method, it creates high performing joints in a wide range of materials while avoiding overlap lengths and added weight from fasteners, crack stoppers, doublers, etc. However, the adoption of this technology to the assembly of large fuselage shell components is challenging, due to geometric tolerance management requirements. In this paper, a hybrid joining method is proposed for such application, involving FSW and adhesive bonding. Fatigue performance of single lap joints of AA2024‐T3 Al‐Mg‐Cu alloy was assessed and benchmarked against FSW overlap and adhesive bonded joints. Significant strength and ductility increase was achieved through the hybridization of the overlap FSW joints. Fatigue strength of the hybrid joints was also higher than FSW overlap joints, although not as high as adhesive bonded joints.     

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.     

Plasticity induced crack closure in adhesively bonded joints under fatigue loading

The mean load of a cyclic loading has a large effect on fatigue crack growth rates in metallic materials and bonded joints. In metallic structures, this effect has been attributed to plasticity-induced crack closure, but little is known about the mechanism responsible for this mean load effect on fatigue crack growth in adhesively bonded joints. This paper presents a computational investigation of the plasticity-induced crack closure mechanism affecting disbond growth in adhesively bonded joints under fatigue loading. The results show that the ratios of crack-opening and crack-closure are approximately independent of the level of plastic constraint, indicated by the ratio between the plastic zone size and the adhesive thickness. An effective strain-energy release rate parameter, which accounts for the crack closure behaviour, has been developed as a new correlating parameter for disbond growth. Comparisons with the experimental results pertinent to four different adhesive bonded joints reveal that this new correlating parameter is capable of unifying the fatigue growth rates by eliminating the effect of mean loads.     

Fatigue strength and fatigue fracture mechanism of three-sheet spot weld-bonded joints under tensile–shear loading

This paper deals with fatigue behavior of three-sheet spot weld-bonded (SWB) joints to investigate the influence of adhesive bonding on fatigue strength and fracture mechanism. From the results of tensile–shear fatigue tests, the fatigue strength of the SWB joint was higher than that of the spot welded (SW) joint. For fatigue behavior in the SWB joint, debonding between a steel sheet and adhesive propagated from an edge of bonded area to a nugget edge, and a fatigue crack initiated at the nugget edge. It was concluded that the delayed fatigue crack initiation at the nugget edge in the SWB joint resulted in the fatigue strength improvement of SW joint.     

基于循环载荷的单搭胶接接头残余强度分析

为研究循环载荷下单搭胶接接头的残余强度及失效机理,以5052铝合金单搭胶接接头为研究对象,先后对其进行静强度测试、疲劳强度测试和残余强度测试,引入威布尔分布对试验数据进行分析,检验其有效性,并采用超声扫描显微镜和扫描电子显微镜对失效胶层进行失效机理分析。结果表明,在疲劳循环载荷作用下,接头刚度基本稳定,而残余强度随着疲劳循环载荷周次的增加,呈现出先增大后减小的变化趋势;疲劳裂纹从接头搭接端部的界面端点处开始萌生,并快速向中间扩展,当疲劳循环达到一定次数时,胶层瞬间断裂,裂纹萌生阶段几乎占据了其全部疲劳寿命,失效后的胶层会出现"凹台"状微观结构。