板厚、温度和速度对单搭接胶接接头强度的影响

为了探讨单搭接胶接接头结构的破坏机理,采用Hopkinson拉杆实验技术,研究了板厚、温度和速度(试样端部的最大速度)对单搭接胶接接头强度的影响。实验结果表明,板越厚、温度越低、速度越大,接头的强度越大。运用有限元方法分析了胶层的应力分布,通过引入剥离应力对试样强度的影响因子,研究发现板越厚、温度越低、速度越大,剥离应力对接头强度的影响越小。     

多焊点情况下胶焊单搭接头的静力分析

以胶接分析为基础,将焊点视为大剪切弹性模量胶粘荆,假设被粘体切应力沿厚度线性分布,胶层和焊点切应力沿厚度方向不变,建立了多焊点情况下胶焊单搭拉剪接头的线弹性应力解析模型.计算结果表明:被粘体正应力和胶层切应力解析解与有限元模型吻合得较好.对焊距的参数研究表明:胶焊单搭拉剪接头连接区纵向正应力和切应力随焊距减少而分布更均匀,峰值切应力下降,与前人的试验结果一致.     

单搭接胶接接头拉伸剪切性能的数值模拟与实验研究

采用数值模拟和光测技术对单向拉伸载荷作用下单搭接胶接接头中的剪切性能进行分析,研究了不同厚度胶层中切应力的变化规律。用有限元方法(FEM)对不同胶层厚度的试件进行建模,得到了拉伸载荷下胶粘剂中的切应力分布及其统计参数。利用数字图像相关(digitalimage correlation,DIC)方法对试件的变形场进行测量。结果表明,当胶粘剂的厚度较小时,胶粘剂中的切应力的分布统计参数随着其厚度的增加会有显著的变化,但是当厚度超过一定的数值时,统计参数对厚度的变化不再敏感。     

胶接体系的胶接强度、粘结能及损伤破坏研究

胶接是指一种用粘合剂实现连接和固持的方法,胶接形式的金属薄板在汽车工业,建筑业以及航空航天领域有着广泛的应用.论文采用有限元模拟方法,研究了该胶接体系在受载状态下的滑剪破坏行为,重点关注了胶层粘结能,搭接长度,胶层厚度对胶接接头承载能力的影响,同时初步探讨了胶层的界面损伤情况.胶层粘结能的提高能够显著提高接头的承载能力.此承载能力受搭接长度和胶层粘结能的共同影响,较大的粘结能情况下,提高搭接长度能够显著提高接头的承载能力.胶层厚度对接头的承载能力也存在影响,在论文考虑的厚度范围内,提高厚度能够增强接头的承载能力.最后初步考虑了接头在达到载荷峰值时刻的胶层损伤情况.     

单搭接胶接接头弹性应力的二维分析方法

提出一种能得到单搭接胶接接头二维弹性应力解析解的的一般分析方法.该方法从纵向正应力沿厚度线性分布的理论假设出发,用完整的几何方程与本构方程,在考虑了被粘物与胶层的剪应力和剥离正应力沿厚度的变化,而且严格满足包括搭接区端头胶层剪应力为零的所有边界条件下,能够准确地预测接头任意点的应力状态,并适用于被粘物/胶层几何和材料属性的任何组合.通过与以往的解析解和有限元分析结果对比表明:不仅胶层平均剪应力最大值发生在距胶层端头很近的位置处,而且平均剥离正应力最大值位置也距离接头端头很近.这与以往绝大多数理论解预测"胶层剪应力和剥离正应力最大值都发生在端头处"的结论不同;该解析解有很好的精度和较广的适用范围.     

单搭拉剪胶焊接头的应力和刚度分析

胶焊复合连接技术兼具胶接和点焊的优点,它因提高结构强度和刚度而使车辆轻量化成为可能.以胶接理论为基础,考虑了被粘体剪切应变,将焊点视为大剪切弹性模量胶粘剂,胶层和焊点沿其厚度方向的剪应力不变,建立了胶焊单搭拉剪接头的线弹性应力解析模型.在应力模型基础上,将接头各组成部分看作是独立承载的拉伸和剪切弹簧单元,得到了其刚度解析模型.应力模型中的正应力和剪应力与有限元解吻合得较好,证明理论模型正确,参数研究中确定了影响胶焊单搭接头应力分布特征的关键耦合参数.     

复合材料层合板单搭胶接力学性能检测技术与分析

胶接工艺缺陷对单搭胶接接头的拉伸剪切性能有着重要的影响。为了研究不同单搭接胶接层厚度对不同材质复合材料层合板胶接性能的影响规律,通过喷水穿透法超声C扫描对试样的剪切区域进行无损检测,并分别采用1mm、2mm、4mm的胶层厚度,以碳纤维/玻璃纤维复合材料层合板为被粘物,进行单搭胶接拉伸剪切性能试验。检测及试验结果表明:当胶层厚度h1mm时,对于相同材料的被粘物,胶层厚度越大,试件胶接接头剪切强度越小;相同的粘接剂厚度,以碳纤维增强复合材料板为被粘物的试件胶接接头剪切强度大于以玻纤增强复合材料板为被粘物的试件胶接接头强度;胶粘剂与碳纤维被粘物表面的润湿效果要优于胶粘剂与玻纤被粘物表面的润湿效果。     

层合板预紧螺栓搭接孔边应力分析

针对复合材料层合板预紧螺栓单板搭接和双板搭接结构,分别建立了全尺寸三维有限元模型,应用非线性接触算法模拟螺栓连接,采用Prets179预紧力单元施加螺栓预紧力.通过分析两种搭接形式在不同预紧力下的孔边应力分布,得到了预紧力与孔边拉应力以及预紧力与孔边层间应力的关系曲线.分析表明:随着螺栓预紧力增加,层合板孔边拉应力水平不断降低;双板搭接的孔边应力明显低于单板搭接的孔边应力.     

周期激励下单搭接接头强度与振动特性研究

主要研究汽车轻量化粘接结构在周期性振动载荷激励下强度与振动属性的改变。首先,利用实验手段,研究了振动载荷对单搭接接头疲劳特性的影响,分析了疲劳后接头的强度及模态频率的变化;其次,通过仿真分析方法,建立了基于经典双线性内聚力模型(Cohesive Zone Model)的单搭接接头静态及动态仿真模型,对胶接接头的模态频率、振型及加载开裂过程中胶层单元失效扩展进行模拟,与此同时,探讨了疲劳载荷对胶层内聚力模型的弱化效应。最后,利用SEM电镜分析手段,从微观上分析了粘接接头疲劳损伤及断裂机理。     

金属多级类蜂窝的压溃行为研究

通过实验和数值模拟方法系统研究了单胞壁开孔金属多级类蜂窝与双胞壁开孔金属多级类蜂窝的压溃行为.重点分析了试件尺寸、开孔位置、孔偏距和孔梯度等因素对多级类蜂窝力学性能的影响.结果表明,多级类蜂窝的压溃过程可分为3个阶段:弹性变形、屈曲变形以及密实;单胞壁开孔多级类蜂窝的压溃过程趋向于渐近内凹压溃,而双胞壁开孔多级类蜂窝趋向于轴向压溃;试件尺寸对多级类蜂窝的力学行为有明显的影响,当胞元数达到一定数目时,其力学性能几乎与蜂窝胞元数无关.单胞壁开孔多级类蜂窝的峰值应力大于双胞壁开孔多级类蜂窝的峰值应力,但其平均压溃应力小于双胞壁开孔多级类蜂窝的平均压溃应力;与传统蜂窝相比,蜂窝胞壁开孔设计降低了蜂窝材料的比吸能;孔偏距的存在导致单胞壁开孔多级类蜂窝的峰值应力降低,但随着孔偏距的增加其平均压溃应力呈先减低后增加趋势;多梯度孔设计对多级类蜂窝材料的力学性能有重要影响,与均匀孔多级类蜂窝相比,正梯度孔分布设计降低了多级类蜂窝峰值应力,但提高了其平均压溃应力;多梯度孔分布设计对多级类蜂窝的峰值应力和平均压溃应力影响不大.     

Linear and higher order displacement theories for adhesively bonded lap joints

This work presents an adhesive model for stress analysis of bonded lap joints, which can be applied to model thin and thick adhesive layers. In this theory, linear variations of displacement components along the adhesive thickness are firstly assumed, and the longitudinal strain and the Poisson's effect of the adhesive are modeled. A differential form of the equilibrium equations for the adherends is analytically solved by means of compatible relations of the adhesive deformation. The derived shear and peel stresses are compared with the classical adhesive model of continuous springs with constant shear and peel stresses, and validated with two-dimensional finite element results of the geometrically nonlinear analysis using a commercial package. The numerical results show that the present linear displacement theory can be applied to both thin and moderately thick adhesive layers. The present formulation of the linear displacement theory is then extended to the higher order displacement theory for stress analysis of a thick adhesive, whose numerical results are also compared with those of the finite element computation.     

Design and analysis of a smart composite pipe joint system integrated with piezoelectric layers under bending

Incorporating with the high electro-mechanical coupling performance of piezoelectric materials, design and analysis of an adhesively bonded smart composite pipe joint system were conducted. In this joint system, piezoelectric layers were integrated into the joint coupler in order to reduce stress concentration in the joint adhesive layer. To theoretically verify the composite action and efficiency of the integrated piezoelectric layers, an electro-mechanical model based on the first-order shear deformation theory was established. This model was able to clarify the energetic characteristics of the proposed joint system on the improvement in the joint strength, which was under the action of a bending moment at the joint ends. The state-space method was utilized to obtain the final analytical solutions, including the peel and shear stress distributions in the adhesive layer. Finally, some numerical examples were calculated to evaluate the effect of the detailed stacking sequence and size of the integrated piezoelectric layers on reducing the stress concentration in the adhesive layer as well as the applied electric fields. These numerical results validated the integrity of the developed adhesively bonded smart composite pipe joint system.     

Two kinds of contact problems in three-dimensional icosahedral quasicrystals

Two kinds of contact problems, i.e., the frictional contact problem and the adhesive contact problem, in three-dimensional(3D) icosahedral quasicrystals are discussed by a complex variable function method. For the frictional contact problem, the contact stress exhibits power singularities at the edge of the contact zone. For the adhesive contact problem, the contact stress exhibits oscillatory singularities at the edge of the contact zone. The numerical examples show that for the two kinds of contact problems, the contact stress exhibits singularities, and reaches the maximum value at the edge of the contact zone. The phonon-phason coupling constant has a significant effect on the contact stress intensity, while has little impact on the contact stress distribution regulation. The results are consistent with those of the classical elastic materials when the phonon-phason coupling constant is 0. For the adhesive contact problem, the indentation force has positive correlation with the contact displacement, but the phonon-phason coupling constant impact is barely perceptible. The validity of the conclusions is verified.     

In situ determination of adhesive shear moduli using strain gages

A new, convenient and cost-effective method of determining in situ adhesive shear moduli using strain gages is proposed and evaluated. Thick-adherend lap shear specimens with stacked gage rosettes at the center of the bond line are loaded in tension for adhesive shear strain measurement. Experimental and numerical results indicate that the test specimen has a nonuniform adhesive shear stress (or strain) distribution in the test section and that this distribution (except at the center point of the bond line) is greatly affected by load eccentricity. In addition to the nonuniformity in the shear stress distribution, the issue of material nonhomogeneity in the gage-covered region affects the strain gage measurement. By taking into account these two issues and assuming linear-elastic behavior, two approaches for converting the gage-measured shear strain into the adhesive shear strain are developed and verified by experiment. It is shown that the strain gage measurement associated with either of two conversion techniques can determine the in situ adhesive shear moduli, which are comparable with moiré experiment and KRG-1 extensometer measurements.     

Analysis of an adhesively bonded single-strap joint integrated with shape memory alloy (SMA) reinforced layers

Shape memory alloys (SMAs) are increasingly becoming a topic of research in the area of smart materials. In this study, the design and analysis of a SMA reinforced joint is presented to elucidate the contribution of the active composite layer to the reduction of stress concentrations in the adhesive layer. Basic thermo-mechanical properties of the SMA are obtained by micromechanics. The forces and moments at the joint edges are obtained by incorporating the thermo-mechanical effect of the active composite layer within the joint. Further, an analytic model based on the first-order shear deformation theory was employed to conduct stress analyses of this joint system. The state-space method was utilized to obtain the final analytic solutions, including the peel and shear stresses in the adhesive layer. Detailed numerical analyses are conducted. The results confirm that the active composite layer significantly reduces stress concentrations at the joint edges.     

细分曲面边界元法的黏附吸声材料结构拓扑优化分析

等几何分析采用样条基函数构造几何模型和实施变量近似,实现了计算机辅助设计和辅助工程的无缝连接,并已广泛应用于弹性力学、电磁场和位势问题等领域.然而直接采用等几何方法难以构造复杂模型,限制了该方法在大规模实际工程问题上的应用.细分曲面法可用于克服这一问题,该方法对传统模型的离散网格进行细分和拟合操作,构造出极限光滑曲面,连续性更高,对复杂结构的适用性更强.该方法主要有以下优点:(1)适用于任意拓扑结构;(2)数值计算稳定;(3)实施简单;(4)局部细化与连续性控制.由于该方法在复杂结构模型构造方面具有较强的灵活性和便利性,已被广泛应用于航空航天、汽车、动画、游戏制作等建模领域.将细分曲面法与边界元法相结合进行结构声学分析,几何场与物理场均采用箱样条基函数进行插值近似.以黏附吸声材料结构的声散射问题为例,建立吸声材料分布拓扑优化数学模型,并采用移动渐进线算法进行设计变量更新,最终获得最优材料分布.      

断裂过程区应力应变场的数学分析

本文将条状分离区看作是位错连续分布区域,利用复变函数理论及切比雪夫多项式级数展开提出了一种统一的数学分析的方法,用以对均匀材料裂纹前方分离过程区的非线性效应进行有效的,精确的解析分析。避免以前各种模型一般都需要借助于有限元法或其他离散方法才能得到数值解答的难点。本文利用这一新方法,对断裂过程区是内聚力模型,条状屈服区模型的裂纹问题,受约束金属薄膜的裂纹问题,进行了分析计算,并与已有的结果进行了比较,得到了满意的结果。     

The role of the adhesive layer in a double cantilever joint

The problem of a double cantilever beam adhesive joint is reconsidered under the assumption of cohesive fracture within the adhesive bond layer. After properly accounting for the adhesive layer, the problem is reduced to a Fredholm integral equation of the second kind for the bond line traction. Numerical results for the bond line stress distribution and the crack tip stress intensity factor are presented for several combinations of the governing material and geometrical parameters.     

叶片榫头接触应力的求解研究

接触应力分析是不易检测、难于计算，但对于设计又是非常重要的一个难题。文中将实验检测技术与数值计算方法相结合，求解飞机发动机叶片榫头上的接触应力分布。基本思路是：1)用实验检测技术求出叶片榫头接触面上若干点的应力或应变值；2)通过给叶片根部接触面施加一定的约束条件，用数值计算法计算发动机叶片在离心力载荷作用下的全场应力分布，并进一步求出接触面上的接触应力分布；3)解除接触面上的约束条件，代之以计算获得的接触载荷，计算叶片在离心力载荷以及接触载荷共同作用下的全场应力或应变分布，并比较计算结果与实验结果；4)修改约束条件或计算模型，重复上述操作，直至计算结果与实验结果比较一致。研究表明，本文提出的方法能够较准确地给出接触面的载荷分布，判断约束条件的合理性具有简单、易行的特点。由于接触应力的复杂性，本问题还有深入研究的必要。