不同材料压印接头的拉剪性能和疲劳性能

采用分体式下模压印连接设备分别对SPCC钢和5052铝合金进行压印连接,然后对两种材料的压印接头进行拉剪试验,并在不同载荷水平下进行疲劳试验,研究了它们的拉剪性能和疲劳性能。结果表明:在拉剪载荷下,铝合金压印接头从上、下板接触挤压的颈部发生断裂,钢压印接头在上、下板接触挤压的颈部发生断裂的同时发生剥离失效,压印接头的拉剪强度主要与上板的颈部强度有关;不同材料压印接头的疲劳性能均良好,钢压印接头的宏观裂纹出现在接头的盲孔边缘,垂直于载荷方向延伸,断裂发生在板材的接头处,其在0.75倍最大破坏载荷下的疲劳寿命超过500万次;铝合金压印接头在每种载荷水平下的疲劳寿命均可达200万次。     

DP780/AA6061薄板自冲铆接头微动损伤特性

对高强钢DP780与铝合金AA6061薄板的异质自冲铆接连接工艺进行研究,并分别制备了不同搭接顺序的DP780/AA6061(SA)和AA6061/DP780(AS)接头。对两组接头进行了高周疲劳试验,对比分析了两组接头的疲劳性能与失效行为,并进一步利用微观检测技术较系统地分析了两组接头的微动损伤机理。结果表明:AS接头的疲劳性能明显优于SA接头,且两组接头疲劳失效模式依次为铆钉断裂和下板断裂。SA接头和AS接头的上板近端与下板末端接触区域、上板近端与下板远端接触区域和铆钉与下板近端接触区域均发生微动磨损。微动磨损会导致SA及AS接头的铆钉和下板近端均出现疲劳裂纹,由于板材性能的差异,裂纹在铆钉和下板上的传播路径和扩展速率不同,最终导致接头失效模式存在差异。     

汽车发动机正时链系统失效分析

通过对发动机正时链条试验后的滚子、套筒及销轴的显微硬度试验及表面磨损形貌SEM的失效分析,并对破碎的滚子断口及滚子表面的微裂纹进行了形貌诊断。结果表明:正时链条在工作中滚子的断裂及疲劳剥落、套筒内的疲劳点蚀和氧化磨损、销轴的氧化及微动磨损是正时链系统失效的主要原因;系统中的链条出现的氧化点蚀、犁沟磨损及疲劳磨损等特征是系统中磨损的主要机制;链条在加工过程中存在的纵向划痕及滚子边缘部位台阶处的应力集中是影响链条使用寿命的主要因素。     

局部热处理对TA1钛合金-SPCC钢压印接头失效行为的影响

在自行搭建的局部热处理试验平台上将TA1钛合金-SPCC钢压印接头连接部位加热至900℃水淬,研究了局部热处理对此压印接头失效载荷和失效模式的影响。结果表明:局部热处理后该压印接头的失效载荷为5 371.9N,比未经热处理的(4 252.4N)提高了26.34%;未经热处理压印接头的失效模式为上下板拉脱失效,断裂方式为韧性断裂,局部热处理后该压印接头的失效模式为拉脱+颈部断裂混合失效,断裂方式为准解理断裂。     

铜铝异种金属板压印连接与接头拉剪载荷研究

采用一种新的塑性成形连接方法--压印连接方法来实现铜、铝合金板的连接,通过拉剪实验研究了连接接头的力学性能,并分析了铜、铝合金板的排列顺序对接头拉剪载荷的影响。实验结果表明,对于铜、铝复合接头,铜板在上时接头具有较高的拉剪载荷(3kN),是铝板在上时拉剪载荷的4.6倍。根据接头失效形式对复合接头进行优化后发现：下层铝板的厚度增大时,接头的拉剪强度略有增大,拉剪过程中的能量吸收明显增大;提高下板材料强度时,接头的拉剪载荷明显增大;铜板作为上板进行压印连接时,失效形式为颈部断裂失效,且接头的拉剪强度较大。     

铝合金板材自冲铆接头的疲劳性能分析

介绍了自冲铆是一种无需预钻孔的薄板新型连接技术及自冲铆的工艺特点。参照国家标准疲劳试验方法,针对5052H32铝合金板材单搭自冲铆接头进行了疲劳试验,测得其疲劳强度为45．9MPa。分析了自冲铆接头的疲劳失效机理,发现微动磨损是导致其失效的主要原因。     

架空导线微动磨损表面的微观分析

在轴向静载荷为 30MPa ,振动频率为 10Hz,弯曲振幅为 0 8mm的试验条件下 ,在弯曲疲劳试验装置上对JL/G1A 12 5 2 6 / 7架空导线进行微动试验。利用扫描电子显微镜分析了经 5 4× 10 6周次循环振动后的线夹处导线的微动磨损表面形貌特征。结果表明 :架空导线的各同层铝线间的接触处、外层铝线与内层铝线的接触处、内层铝线与钢线的接触处、外层铝线与线夹的接触处均发生了微动磨损 ,其中与线夹接触的外层铝线磨损最为严重。磨损机制为粘着磨损、氧化磨损和磨粒磨损 ,磨屑主要为铝的氧化物 ;微动疲劳裂纹发生在磨损区域内 ;在磨损区与非磨损区的界面没有发现疲劳裂纹。     

SPFC440钢/5052铝自冲铆接头与胶铆复合接头腐蚀性能对比

为研究SPFC440钢与5052铝合金自冲铆接头的腐蚀性能,分别制备了自冲铆接和胶铆复合两种接头。通过对不同腐蚀时长下的两种接头试样进行疲劳性能测试,分析了粘胶剂对铆接接头腐蚀疲劳性能的影响,并对疲劳断口、裂纹扩展进行SEM和EDS检测。结果表明：粘胶剂的存在不仅提高了接头强度,还保护了金属界面,减小了电偶腐蚀的影响;随着腐蚀时间的增长,复合接头的最大静载荷值不断减小,自冲铆接接头最大静载荷先增大后减小;复合接头的拉伸失效模式与自冲铆接接头的失效形式相似;自冲铆接接头的疲劳裂纹主要集中在下板料的铆钉周围,复合接头主要为下基板的断裂;铆钉与下板相互接触区域以及两板间接触面出现了严重微动磨损。     

冷轧钢压印接头拉伸-剪切和疲劳性能研究

对冷轧钢圆形连接点和矩形连接点的压印接头进行拉伸-剪切试验,研究连接点形状对接头拉伸-剪切性能的影响.并对圆形连接点压印接头进行疲劳试验.试验结果表明,两种接头拉伸-剪切强度和刚度相当.圆形连接点拉伸-剪切过程中的能量吸收值大于矩形连接点,矩形连接点的失效形式为上板拉脱失效.应力比R=0.5,当最大疲劳载荷为接头强度的95％时,接头循环寿命可以达到137万次,为80％时,可以达到疲劳极限500万次.疲劳失效形式为上板接头处产生裂纹,裂纹方向与加载方向大致呈90°.提出了圆形点压印接头的拉伸-剪切强度预测公式和疲劳寿命计算公式,拉伸-剪切强度公式的误差为6.9％.     

中性腐蚀环境下钢丝的微动疲劳行为

在自制的微动疲劳试验机上开展中性腐蚀环境下单根钢丝的微动疲劳实验,考察在相同接触载荷下,不同振幅对钢丝的微动疲劳行为的影响,并用扫描电子显微镜观察疲劳钢丝的磨痕和断口形貌,研究钢丝微动疲劳断裂机制.结果表明:在较大的振幅下,钢丝的微动区均处于滑移状态,而在较小振幅下,钢丝的微动区从滑移状态逐渐转变为黏着状态;磨损机制主要为磨粒磨损、疲劳磨损、腐蚀磨损和塑性变形;钢丝疲劳寿命随着微动振幅的增大而减小;钢丝的疲劳断口可分为3个区域,即疲劳源区、裂纹扩展区及瞬间断裂区.     

Study on failure mechanism of mechanical clinching in aluminium sheet materials

Mechanical clinching is a connection technology that is widely used in different industrial fields because it has several advantages, including easy preparation, an excellent fatigue property and environmental friendliness. In this study, tensile-shear tests and fatigue tests were conducted to characterize the mechanical properties of clinched joints using aluminium alloys. The experimental results showed that the fracture regions were concentrated in the indentations of the lower sheets. The failed surfaces were examined using a scanning electron microscope and an energy-dispersive X-ray machine to study the fretting fatigue failure mechanisms of the clinched joints. Two types of fretting wear modes were observed: the neck fretting wear mode and indentation-surrounding fretting wear mode. The results also showed that the proportions of these two fretting wear modes could be impacted by the applied load levels.     

Fretting fatigue crack initiation lifetime predictor tool: Using damage mechanics approach

Fretting fatigue is a combination of two complex mechanical phenomena. Fretting appears between components that are subjected to small relative oscillatory motions. Once these connected components undergo cyclic fatigue load, fretting fatigue occurs. In general, fretting fatigue failure process can be divided into two main portions, namely crack initiation and crack propagation. Fretting fatigue crack initiation characteristics are very difficult to detect because damages such as micro-cracks are always hidden between two contact surfaces.In this paper Continuum Damage Mechanics (CDM) approach in conjunction with Finite Element Analyses (FEA) is used to find a predictor tool for fretting fatigue crack initiation lifetime. For this purpose an uncoupled damage evolution law is developed to model fretting fatigue crack initiation lifetime at various fretting condition such as contact geometry, axial stress, normal load and tangential load. The predicted results are validated with published experimental data from literature.     

Fretting fatigue considerations in holistic structural integrity based design processes (HOLSIP)—A continuing evolution

Fretting fatigue has become one of the most significantly recognized failure mechanisms in engineering applications of critical components of many joined sub-systems or systems. It is one of the major areas of concern in fixed wing aircraft connections, rotary wing gearboxes, clutches, bearings, bushing, lugs, and engines of all types in the aviation industry. For many years the power generation industry has recognized the importance of fretting fatigue and some major failures have been attributed to fretting fatigue over many years. It has been of concern in many other industries in recent years. As the knowledge on fretting corrosion, fretting wear, and fretting fatigue has expanded it has been recognized as a major source of the failure of engineering components in a myriad of applications. This has led to recent standards for testing and terminology related to fretting fatigue in Japan, the USA/Canada (ASTM), and France.     

TC4合金微动疲劳损伤研究

研究了TC4合金在柱面-平面接触务件下的微动疲劳行为，分析了其微动疲劳损伤机制。结果表明：在试验务件下，微动区边缘的损伤特征以粘着磨损为主，而微动区中部则以磨粒磨损和接触疲劳为主。疲劳裂纹易于在微动区．特别是在蚀坑处萌生和扩展。促使微动疲劳裂纹萌生的因素：一是法向应力和切向摩擦力引起的材料表层塑性变形，二是微动磨损破坏了材料的表面完整性，造成了缺口应力集中效应。     

Finite Element Analysis of Localized Plasticity in Al 2024-T3 Subjected to Fretting Fatigue

Fretting fatigue is a combination of two complex mechanical phenomena, namely, fretting and fatigue. Fretting appears between components that are subjected to small relative oscillatory motion. Once these components undergo cyclic fatigue load at the same time, fretting fatigue occurs. Fretting fatigue is an important issue in aerospace structural design. Many studies have investigated fretting fatigue behavior; however, the majority have assumed elastic deformation and very few have considered the effect of plasticity. The main goal of this study is to monitor the effect of different fretting fatigue primary variables on localized plasticity in an aluminum alloy (Al 2024-T3) test specimen. In order to extract the stress distribution at the contact interface under elasto-plastic conditions, a modified finite element contact model was used. The contact model was verified through comparison with an elastic analytical solution. Then, a bilinear elasto-plastic isotropic hardening model with a von Mises yield surface was implemented to simulate the material behavior of the aluminum alloy. The effect of different fretting fatigue primary variables, such as axial stress, contact geometry, and coefficient of friction, on localized plasticity was investigated. Finally, the relationship between the location of maximum localized plasticity and Ruiz fretting damage parameter with the crack initiation site is discussed.     

微动疲劳参数对钢丝微动疲劳磨损演化的影响*

微动疲劳易引起钢丝表面磨损和横截面积损失,进而造成钢丝断裂失效并缩短钢丝绳使用寿命。不同微动疲劳参数（接触载荷、疲劳载荷、钢丝直径和交叉角度）引起差异的钢丝微动疲劳磨损特性,故研究微动疲劳参数对钢丝微动疲劳磨损演化规律影响至关重要。基于摩擦学理论和Marc仿真软件构建钢丝微动疲劳磨损模型,探究接触载荷、疲劳载荷、交叉角度和钢丝直径对钢丝微动疲劳磨损演化的影响规律。结果表明：钢丝微动疲劳磨损体积主要与接触载荷和疲劳载荷有关;疲劳钢丝的磨损深度、磨损率及磨损体积随着接触载荷的增加而增大,且不同接触载荷下疲劳钢丝磨损体积均随着循环次数的增加而呈线性增加;随疲劳载荷幅值的增加,疲劳钢丝的磨损深度、磨损率及磨损体积均呈增加趋势;在不同疲劳载荷范围下疲劳钢丝的磨损体积均随着循环次数的增加而呈线性增加;当接触载荷、疲劳载荷及钢丝间摩擦因数相同时,不同交叉角度和不同加载钢丝直径下疲劳钢丝的磨损体积相同。     

关于微动磨损与微动疲劳的研究

微动磨损与微动疲劳是２种主要的微动模式,造成的损伤在工业中相当普遍,并可能引发灾难性的后果。主要研究了们移幅度、压力和疲劳应力３个基本微动参数,并以获得的微动区域、微动图为基础,分析了微动磨损与微动疲劳的运行机制和破坏规律。为更好地了解微动磨损与微动疲劳之间的内在联系,进一步探讨了接触磨损与局部疲劳、局部疲劳与整体疲劳之间的竞争机制。     

Characterization of fretting wear behavior of Cu–Al coating on Ti–6Al–4V substrate

Fretting wear and fretting fatigue are two commonly observed material damages when two contacting bodies with a clamping load are under the oscillatory motion. In this study, fretting wear damage of Cu–Al coating on titanium alloy, Ti–6Al–4V substrate was investigated using the dissipated energy approach. Fretting tests were conducted with either no fatigue load or the maximum fatigue load of 300 MPa and stress ratio of 0.1 on the substrate (specimen). In order to investigate the effect of contact load and contact size, different pad sizes and contact loads were used in the tests. Accumulated dissipated energy versus wear volume data showed a linear relationship regardless of fatigue loading condition on specimen with the smaller pad size. However, two separate linear relationships were observed based on the fatigue loading condition with the larger pad size, such that a relatively more dissipated energy was required for a certain amount of wear with fatigue load on the specimen. The linear relationship between the accumulated dissipated energy and wear volume for both pad sizes extended from partial to gross slip regimes and was not affected by the applied contact load. Further, fretting tests with and without fatigue load resulted in different shapes of fretting loops when the larger pad size was used.     

二次压缩机填料盘微动失效研究

对茂名石化乙烯工业公司低密度聚乙烯装置二次压缩机填料盘过度磨损和开裂的原因进行了分析和研究。结果表明。相邻两块填料盘之间存在着微动磨损,同时填料环的腐蚀和磨损加速了填料盘的微动,大大降低了填料盘的疲劳寿命,使填料盘疲劳开裂。