某车型发动机悬置螺栓连接失效原因分析

针对公司某车型发动机悬置支架与发动机支座连接螺栓在路试过程中发生疲劳断裂进行分析。本文从材料断口学、金相学等失效分析方法分析螺栓断裂原因;基于VDI2230螺栓连接计算系统对螺栓连接安全设计进行分析,从增大预紧力提高螺栓的疲劳性能进行分析。并对导致结构连接失效的原因提出优化设计措施,供汽车悬置支架连接设计相关人员参考。     

ZKG223钎杆连接套管断裂原因分析

某ZKG223钎杆连接套管在使用过程中发生断裂失效。通过宏观检查、化学成分分析、金相检验、断口分析对套管断裂失效原因进行了分析。结果表明:该连接套管断裂类型为疲劳断裂。断裂起源于套管内壁螺纹损伤处,套管与钎杆装配时存在连接松动造成使用过程中螺纹发生磕碰挤压损伤,引起疲劳裂纹的萌生及扩展,最终导致套管断裂失效。     

断裂失效分析(续)

3.3疲劳断裂失效分析　疲劳断裂失效分析的内容包括：分析判断零件的断裂失效是否属于疲劳断裂与疲劳断裂的类别;引起疲劳断裂的载荷类型与大小以及疲劳断裂的起源等.疲劳断裂失效分析的目的则是找出引起疲劳断裂的确切原因,从而为防止同类疲劳断裂失效再次出现所要采取的措施提供依据.     

高强度螺柱断裂原因

某高强度螺柱在服役10个月后发生断裂，采用宏观观察、化学成分分析、扫描电镜分析、金相检验以及力学性能测试等方法对螺柱断裂原因进行了研究。结果表明：在较大交变载荷的作用下，断裂螺柱螺纹牙底的折叠位置萌生裂纹并扩展，最终发生疲劳断裂。     

汽车发动机风扇叶片断裂分析

汽车发动机风扇叶片在汽车运行中断裂,对断裂叶片的断口进行了宏、微观分析,并追踪了风扇的生产工艺,探明了叶片失效的主要原因是冲压工艺不当产生了微裂纹,在随后的工作应力作用下,产生疲劳断裂,改进工艺后避免了该类失效事故的发生。     

QT700-2球墨铸铁发动机曲轴失效分析

目的某厂生产的QT700-2球墨铸铁曲轴在路试过程中出现断裂,需寻找失效原因并提出解决措施。方法通过应用金相组织分析、化学成分分析、表面残余应力测试和力学性能测试等方法,对该曲轴的失效原因进行了分析。结果测试后分析结果表明,曲轴是在较大扭转循环载荷下,在第四连杆颈滚压圆角边缘多点萌生裂纹而导致疲劳断裂是其失效的主要原因。结论建议改进热处理工艺,保证组织的均匀性;改进加工工艺,减少应力集中;并强化表面残余应力以提高曲轴的疲劳寿命。     

某电厂给水泵汽轮机次末级叶片的失效分析

借助于扫描电子显微镜、硬度测试和疲劳试验等手段,分析了OCr17Ni4Cu4Nb马氏体沉淀硬化不锈钢制叶片的断裂机理和失效原因.分析表明.动叶片的断裂机理为高周疲劳,动叶片的失效原因与电火花强化直接相关.提出了改进方法.     

某直升机连接螺栓断裂原因

某型直升机固定尾减速机钛合金内侧压板的3件35Ni4Cr2MoA钢连接螺栓在试车时发生了断裂。通过宏观观察、断口分析、金相检验、力学性能试验和氢含量测试等方法,分析了连接螺栓的断裂原因。结果表明:连接螺栓的失效模式为疲劳断裂,压板孔壁与螺栓杆部的局部挤压损伤形成了疲劳裂纹源,试车过程中裂纹不断扩展,最终导致了连接螺栓的断裂。     

某型教练机减摆器断轴失效分析及改进研究

某型教练机减摆器是防止前轮摆振和传力的关键构件,减摆器轴断裂失效将严重危机飞行安全,使用中曾多次发生断裂.本文应用飞机疲劳断裂理论对该构件进行了疲劳强度计算和断裂原因分析,其结论与该构件的实际断口分析是相符的,属于疲劳断裂.并在此基础上提出预防断轴的措施和在减摆活塞上加装双向安全活门的改进研究建议.     

地铁道岔滑床板断裂失效分析

采用断口宏微观分析、化学成分分析、金相检验、硬度测试等方法对某地铁道岔滑床板断裂的原因进行了分析。结果表明:滑床板失效模式属于疲劳断裂,焊接工艺不当导致焊缝位置晶粒粗大、硬度偏低以及存在应力集中等是其发生疲劳断裂的主要原因,并由此提出了改进措施。     

Characterization and Failure Analysis of an Automotive Ball Joint

This case study describes the failure analysis of an automotive lower ball joint that fractured under normal driving conditions. Through spectroscopy, the material was determined to be SAE-AISI 5135H steel. The metallographic examination revealed a tempered martensitic structure, and hardness measurements radially across the surface of the cut ball stud suggested that the stud was through hardened. Scanning electron microscopy of the fracture surfaces indicated fatigue as the main failure mechanism. Finite element analysis was used to analyze the performance of the part under a normal loading condition. A detailed fatigue analysis to determine the effect of various loads on the life of the ball joint was completed using three methods: S-N curve approximation using hardness values, S-N approach using Basquin’s equation, and a linear elastic crack-growth model. The cause of failure was determined to be from surface cracks forming in the high stress concentration neck region where the ball and stud are joined. The presence of a small surface flaw in this region was shown to significantly reduce the fatigue life of the ball joint.     

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。     

Failure of a Fusion Welded Ball Joint as a Result of Modification in MnS Direction

A failure investigation was performed on a ball joint from an ATV front suspension system. The location of the fracture was the bearing ball/stud interface, which is a fusion-welded joint, and occurred after approximately 20 h of field-testing. The two parts are made out of carbon steel and were previously heat-treated. Many elongated MnS inclusions were found in the stud material, and these inclusions were parallel to the symmetry axis. Even though these inclusions were not significantly sized, their number was important. Macroscopic evidence showed that the joint failed in a ductile mode under centered tensile overload. Microscopic examination showed that MnS orientation changed in the fusion joint area. The inclusions had been redirected during the welding process and laid parallel to the fracture surface. This reorientation caused a significant decrease in the effective cross section of the joint and overload fracture occurred.     

某电传操纵系统弹簧拉杆可调叉形接头断裂原因

某飞机电传操纵系统弹簧拉杆可调叉形接头在运行过程中发生断裂,通过宏微观分析和金相检验等方法对拉杆接头的断裂原因进行了分析。结果表明:拉杆接头断裂为疲劳断裂,断裂的根本原因是其显微组织不均匀的同时出现了魏氏组织,使接头的抗疲劳性能严重降低,导致疲劳裂纹的萌生与扩展;而拉杆的受力不均匀则加速了其疲劳裂纹的扩展。     

某型液压泵壳体螺纹拉脱原因分析

通过断口分析、化学成分分析、硬度测试等方法,对某液压泵壳体螺纹的拉脱原因进行了分析。结果表明：液压泵壳体螺纹拉脱的失效性质为剪切疲劳断裂;循环散热导管接头装配过紧．造成了液压泵壳体螺纹损伤,是导致剪切疲劳断裂的原因;为有效避免螺纹拉脱故障．应增加管接头与液压泵壳体螺纹的有效配合长度。     

Composite-to-metal tubular lap joints: strength and fatigue resistance

The axial strength and fatigue resistance of thick-walled, adhesively bonded E-glass composite-to-aluminum tubular lap joints have been measured for tensile and compressive loadings. The joint specimen bonds a 63 mm OD aluminium tube within each end of a 300 mm long, 6 mm thick E-glass/epoxy tube. Untapered, 12.5 mm thick aluminium adherends were used in all but four of the joint specimens. The aluminum adherends in the remaining four specimens were tapered to a thickness of 1 mm at the inner bond end (the bond end where the aluminum adherend terminates). For all loadings, joint failure initiates at the inner bond end as a crack grows in the adhesive adjacent to the interface. Test results for a tension-tension fatigue loading indicate that fatigue can severely degrade joint performance. Interestingly, measured tensile strength and fatigue resistance for joints with untapered adherends is substantially greater than compressive strength and fatigue resistance.The joint specimen has been analyzed in two different ways: one approach models the adhesive as an uncracked, elastic-perfectly plastic material, while the other approach uses a linear elastic fracture mechanics methodology. Results for the uncracked, elastic-plastic adhesive model indicate that observed bond failure occurs in the region of highest calculated stresses, extensive bond yielding occurs at load levels well below that required to fail the joint, and a tensile peel stress is generated by a compressive joint loading when the aluminum adherends are untapered. This latter result is consistent with the observed joint tensile-compressive strength differential. Results of the linear elastic fracture mechanics analysis of a joint with untapered aluminum adherends are also consistent with the observed differential strength effect since a mode I crack loading is predicted for a compressive joint loading. Calculations and a limited number of tests suggest that it may be possible to selectively control the differential strength effect by tapering the aluminum adherends. The effect of adherend material and thickness on fracture mechanics parameters is also investigated. The paper concludes by examining the applicability of linear elastic fracture mechanics to the joints tested.     

Influence of the accumulated error in thread pitch on the stress–strain state and cyclic strength of threaded joints

Using the finite element method, the analysis of influence of errors in pitch during the thread production on the behavior of stress distribution in stud–nut joints is performed. The value of maximum local stresses in studs of a threaded joint is shown to substantially depend on errors in thread pitch of a stud and a nut. On the basis of the analyses of stresses and strains under cyclic loading, fatigue curves are plotted for the threaded joints having deviations in thread pitch. It is shown that, with a rational selection of the deviation in pitch, the cyclic strength of threaded joints can be considerably increased. The results of analysis agree satisfactorily with the data of fatigue tests of the M39 × 3 threaded joints.     

泡沫金属夹层板自冲铆接头的疲劳性能及失效机理

对铝合金自冲铆接头及泡沫金属夹层结构自冲铆接头进行疲劳实验,通过三参数经验公式采用S-N曲线拟合法绘制接头的F-N曲线,分析接头的疲劳寿命及泡沫金属夹层对自冲铆接头疲劳性能的影响;采用扫描电子显微镜对接头的疲劳失效断口进行观测,分析其微观失效机理。结果表明:泡沫金属夹层缩短了自冲铆接头的疲劳寿命,不同泡沫金属夹层对自冲铆接头疲劳性能的影响具有差异性,在高疲劳载荷下泡沫铜夹层接头疲劳性能更优。三组接头疲劳失效形式都为下板断裂,在高疲劳载荷下裂纹易在铆扣区域萌生,在中低疲劳载荷下裂纹萌生于下板一侧,沿铆扣区域下侧向板材另一侧扩展。     

Probabilistic analysis of the uncertainty in the fatigue capacity of welded joints

This paper presents the results of a study of the uncertainty in the fatigue capacity (constant amplitude fatigue life) of welded steel joints, due to uncertainties related to geometrical and material parameters.An efficient method of probabilistic fracture mechanics analysis is described and applied. A linearelastic fracture mechanics model and the Paris-Erdogan law of crack propagation were adopted. Stressintensity factors were evaluated by employing an influence function method, which is very cost-effective. The main parameters were treated as stochastic variables. Data for weld and crack geometry of the non-load carrying fillet weld cruciform joint selected as the example joint in the study, were recorded from specimens. Other data were compiled from the literature. The uncertainties associated with the basic variables were transformed into a measure of uncertainty of the fatigue capacity by employing the Monte Carlo simulation technique. The relative contributions to the uncertainty in the fatigue capacity from the various factors were also compared.The $\text{S-N}$ data established analytically compared fairly well with test data obtained with 42 specimens. The probabilistic fracture mechanics analysis provided a sufficient sample of data to allow a test of analytical probability distributions to the fatigue life. The fit of two- and three-parameter lognormal and Weibull distributions was examined. Only the three-parameter lognormal pdf passed the chi-square test on the 5% confidence level.     

2219铝合金TIG和FSW接头力学及疲劳性能

目的 研究钨极氩弧焊(TIG)和搅拌摩擦焊(FSW)对2219铝合金(母材)力学及疲劳性能的影响。方法 通过拉伸试验,得到了母材、TIG和FSW接头的抗拉强度和伸长率;通过疲劳性能试验测试了母材、TIG和FSW接头在不同应力下相应的疲劳寿命,根据疲劳试验结果绘制了其试样的S-N曲线;使用扫描电子显微镜观察并分析了疲劳断口的形貌特征。结果 未焊接的铝合金母材抗拉强度和伸长率最高,分别为506 MPa和15.92%;TIG接头抗拉强度和伸长率分别为330 MPa和7.65%,FSW接头抗拉强度和伸长率分别为310 MPa和8.74%。母材、TIG和FSW接头等3种疲劳试样在2×10⁶次循环下的疲劳强度分别为129、108、115 MPa,其疲劳断口均可分为裂纹源区、裂纹扩展区和瞬间断裂区,疲劳裂纹分别起始于试样表面的局部变形区、第二相夹杂物和“吻接”缺陷。疲劳裂纹扩展区的主要形貌为疲劳辉纹和二次裂纹,瞬间断裂区以脆性断裂为主。结论 TIG和FSW等2种焊接工艺均导致了2219铝合金的强度、塑韧性和疲劳性能降低,其接头表面的第二相夹杂物和“吻接”缺陷促进了疲劳裂纹的萌生。