无限寿命螺栓疲劳失效的实验研究

文章研究了高周循环螺栓小疲劳裂纹形成和扩展的过程,讨论了结构碳钢制造螺栓时热轧和调质状态的应力情况,得出了小裂纹尺寸与应力强度因子幅值△K的关系式、疲劳裂纹扩展速度dl／dN和扩展寿命Np的计算式。     

基于ANSYS Workbench的管道疲劳强度分析及优化

疲劳破坏作为一种常见的失效形式,直接关系到机械结构的寿命,通过有限元软件ANSYSWorkbench能够准确计算出机械结构的疲劳寿命。通过SolidWorks建立三维实体模型,在ANSYSWorkbench中进行网格划分,对于液体冲击及螺栓预紧力作用分为两种环境进行静力学计算。将两种环境叠加处理,再通过ANSYSWorkbench中的FatugueTool模块进行非比例载荷疲劳寿命分析。然后根据管道的疲劳寿命结果,优化螺栓预紧力大小,选取最优螺栓预紧力实现管道疲劳寿命的最大化,优化结构的疲劳强度。结果表明,经螺栓预紧力优化后,管道疲劳寿命提高了10%。     

随机载荷下盾构螺栓疲劳寿命分析

为提高盾构螺栓设计结果的可靠性,以某新型盾构螺栓疲劳寿命为研究对象,对盾构螺栓进行静强度分析.根据Miner-Palmgren线性累积损伤理论对螺栓进行疲劳寿命分析,运用Matlab软件模拟螺栓所承受的随机载荷,尝试在设计阶段无法获得实测载荷数据的情况下通过数值仿真方式模拟随机载荷,并运用线性累积损伤理论对盾构螺栓进行...     

螺栓预紧力对发动机气缸盖疲劳特性的影响

发动机气缸盖是较易发生疲劳破坏的发动机零件之一,其机械疲劳强度与螺栓预紧力之间存在关系。利用Solidworks建立气缸的简化模型,导入Workbench中进行静力学分析：在Workbench中建立两个不同的载荷环境,利用组合求解功能对螺栓预紧力和气缸盖受到气缸内气体的最高爆发压力进行线性组合,完成非比例载荷的疲劳寿命计算,得到不同螺栓预紧力下的气缸盖疲劳寿命曲线,由此获知螺栓预紧力和气缸盖疲劳寿命之间的关系,这为合理选择螺栓预紧力提供了依据。     

复杂飞机结构裂纹萌生寿命确定的工程方法

采用静拉伸应变测量试验的方法,确定了典型飞机复杂结构在载荷作用下的应变分布,并准确判断出其疲劳危险部位。对典型飞机复杂结构模拟件进行了等幅加载疲劳试验,并在疲劳试验过程中采用着色探伤方法测得了疲劳裂纹扩展数据。在此基础上,提出并建立了一种适用于确定复杂结构疲劳裂纹萌生寿命的工程方法,包括疲劳裂纹萌生寿命反推法和含有不确定寿命样本的统计推断方法。根据该方法对试验样本疲劳数据进行处理得出了裂纹萌生中值寿命及其在95%置信水平下的单侧置信下限。     

螺栓疲劳破坏及提高联接强度的分析

螺栓联接是机械制造与安装中广泛应用的一种联接形式。由于工作环境恶劣，加之螺栓的疲劳破坏不易被发现，很难预防，螺栓疲劳断裂而造成的重大事故时有发生，给生产与生活带来巨大经济损失。因此应该充分重视和加强对螺栓疲劳破坏的研究，努力改善和提高螺栓联接的强度。螺栓的疲劳破坏分析在螺栓联接中，受拉螺栓联接的使用更为普遍。据资料统计，在破坏了的螺栓零件中，疲劳破坏的比例高达８５％左右，其危害性远远高于其它破坏形式。造成螺栓疲劳破坏的原因主要是零件本身存在的疲劳源及载荷分配不均。在螺栓的制造和使用过程中，由于锻…     

165t铸造吊主梁产生裂纹原因简析及处理办法初探

冶金铸造起重机主梁结构件是典型的焊接结构,其主要失效形式是由于疲劳而产生裂纹直至断裂,而裂纹的萌生和形成寿命很短,疲劳寿命主要取决于疲劳裂纹的稳定扩展阶段。本文以图表及文字表述,简述了湖南涟钢一炼轧厂165/40tX22m行车主梁腹板母板产生裂纹的原因,并针对生产现场的实际情况简要讲述了此次裂纹处理的主要方法和需要采取的防范措施。对于预防主梁钢结构疲劳断裂事故的发生,指导该类型起重机的设计、制造和管理具有重要意义。     

飞机机轮轮毂螺栓断裂失效风险预防与分析研究

飞机机轮轮毂安装螺栓是重要的结构承力件,强度高,对裂纹敏感,一旦使用中出现裂纹将快速扩展直至断裂,对飞行安全构成较大威胁。在对近年来发生的十余起机轮螺栓断裂失效事件从失效模式、失效原因进行深入分析的基础上发现,无论疲劳、氢脆还是应力腐蚀,除与设计、选材、加工工艺有关外,还与应力水平的高低密切相关,以此结合机轮维修装配工艺过程,提出了一系列降低螺栓工作应力水平的措施并运用于机轮维修实践,显著降低了螺栓断裂的风险。     

单点与双点拉剪点焊试样的疲劳特性比较

对单点与两点焊拉剪点焊疲劳试样分别进行了疲劳试验,观测了疲劳裂纹的形状和萌生位置,分析了两种试样的疲劳性能。通过有限元模型分析了同等载荷作用下两种试样的变形,对比两种试样的载荷幅寿命关系,认为两点试样的承载能力约为单点试样的两倍。基于此,使用单点试样的载荷幅寿命曲线,预测了两点试样的疲劳寿命,寿命预测结果与实验寿命结果一致。     

ZL109铸造铝合金高温疲劳分析

对ZL109材料在AMSLER100HFP500高频疲劳试验机上进行高温高频疲劳试验。利用升降法和配对法得出中值疲劳强度(疲劳极限)σ50=144.75 MPa。用扫描电子显微镜(SEM)对断口形貌进行分析,研究裂纹源的形成原因。通过研究ZL109合金的高温疲劳性能和断口形貌,澄清了裂纹源形成的原因。结果表明铸造缺陷是裂纹源形成的主要原因,高温疲劳断裂是蠕变-疲劳交互作用的过程,合理的成分和工艺有利于提高材料的高温性能和疲劳寿命。本工作为新活塞材料的开发提供了依据。     

Effects of surface finish and treatment on the fatigue behaviour of vibrating cylinder block using frequency response approach

INTRODUCTION Due to market pressures for improvements in productivity, reliability, ductility, wear resistance and profitability of mechanical systems, manufacturers are placing increasing demands on available materials.Economic constraints require that these materials are inexpensive and easily available. In order to enhance the surface properties of today’s materials, producers of components are turning to different surface finish and treatments. There are several techniques available …     

Influence of surface treatments on fatigue life of a two-stroke free piston linear engine component using random loading

INTRODUCTION Fatigue durability has long been important issues in the design of a two-stroke free piston linear engine structure (Torres and Voorwald, 2002; Rahman et al., 2005a; 2005b). Durability assessment is traditionally done in the later part of the product development stage when prototypes are available, and heavily re- lied on in confirming ground durability tests. This process is very time consuming and often results in over-design with weight penalties, which is the major obsta…     

Fatigue test of carbon epoxy composite high pressure hydrogen storage vessel under hydrogen environment

A significant temperature raise within hydrogen vehicle cylinder during the fast filling process will be observed, while the strength and fatigue life of the cylinder will dramatically decrease at high temperature. In order to evaluate the strength and fatigue of composite hydrogen storage vessel, a 70-MPa fatigue test system using hydrogen medium was set up. Experimental study on the fatigue of composite hydrogen storage vessels under real hydrogen environment was performed. The experimental results show that the ultimate strength and fatigue life both decreased obviously compared with the values under hydraulic fatigue test. Furthermore, fatigue property, failure behavior, and safe hydrogen charging/discharging working mode of onboard hydrogen storage vessels were obtained through the fatigue tests.     

气瓶上、下封头纵向开裂原因探讨

针对气瓶上、下封头拉深件纵向破裂案例,分析制件在拉深过程中出现破裂缺陷的原因,进而找到解决和防止各类拉深件破裂的措施。     

泥浆泵缸套失效分析

本文介绍了泥浆泵设计过程中基本参数的确定、关键机构的受力分析,分析了缸套的实际工况和受力情况,得出缸套失效的主要原因是泥浆的腐蚀和磨粒磨损。进而继续详细分析冲蚀拉槽;磨料磨损拉槽;外径均匀磨损增大而丧失密封功能;疲劳磨损和气蚀磨损这几种主要磨损的失效形式。又因为现阶段各大油田普遍用复合性双金属缸套,就这种缸套的热镶装工艺过程复杂和生产效率低的问题进行了探讨,进而提出表面强化技术方面的方案,使其工作寿命进一步提高。     

Improving the Fatigue Performance of the Welded Joints of Ultra-Fine Grain Steel by Ultrasonic Peening

Contrast tests were carried out to study the fatigue performance of the butt joints treated by ultrasonic peening, aiming at the improvement of ultrasonic peening treatment(UPT) on welded joints of a new material. The material is a new generation of fine grain and high purity SS400 steel that has the same ingredients as the traditional low carbon steel. The specimens are in two different states:welded and ultrasonic peening conditions. The corresponding fatigue testing data were analyzed according to the regulation of the statistical method for fatigue life of the welded joints established by International Institute of Welding(IIW). Welding residual stress was considered in two different ways: the constant stress ratio R = 0.5 and the Ohta method. The nominalstress-number (σ-N) curves were corrected because of the different plate thickness compared to the standard and because there was no mismatch or angular deformation. The results indicated that: 1 ) Compared with the welded specimens, when the stress range was 200 MPa, the fatigue life of the SS400 steel specimens treated by ultrasonic peening is prolonged by over 58 times, and the fatigue strength FAT corresponding to 106 cycles is increased by about 66％; 2) As for the SS400 butt joint ( single side welding double sides molding) , after being treated by UPT, the nominal S-N curve (m = 10) of FAT 100 MPa(R =0.5) should be used for fatigue design. The standard S-N curves of FAT 100 MPa (R = 0.5, m = 10) could be used for fatigue design of the SS400 steel butt joints treated by ultrasonic peening.     

管磨机筒体法兰处紧联接螺栓的疲劳强度的可靠性设计

本文根据疲劳强度的可靠性设计理论,对管磨机的简体法兰与磨头处的联接螺栓进行了抗疲劳分析,建立了一套可行的设计理论和计算方法。     

NiTi形状记忆合金管双轴疲劳超弹性行为

采用国产NiTi形状记忆合金,在Af温度以上对其进行比例、非比例循环疲劳,结果表明:随着加载路径的非比例度的增加,稳定的平台应力和疲劳寿命降低而循环过程中的残余应变和马氏体的起始转变应力增加.     

Fatigue and fracture behavior of nickel-based superalloy Inconel 718 up to the very high cycle regime

The fatigue and fracture behavior of nickel-based superalloy Inconel 718 was investigated up to the very high cycle regime under rotary bending tests at room temperature. It was found that this superalloy can still fracture after exceeding 107 cycles. Fractographic analysis revealed that there was a transition from fatigue crack initiation at multi-sites to single initiation with decreasing stress levels. The fracture surface can be divided into four areas according to the appearance, associated with fracture mechanics analysis of the corresponding stress intensity factors. The fracture mechanism dominant in each area was disclosed by scanning electron microscope examination and analyzed in comparison with those obtained from the crack growth tests. Subsequently, life prediction modeling was proposed by estimating the crack initiation and propagation stage respectively. It was found that Chan （2003）＇s model for initiation life and the Paris law for growth life can provide comparable predictions against the experimental life.