难加工材料硬态干车削中切削参数对残余应力的影响

本文对切削参数和残余应力之间的关系的进行研究.针对某型号高强高硬钢在硬态干车削过程,研究了各切削参数对已加工表面残余应力及残余应力层深分布的影响.结果发现,不同的切削参数条件下,工件已加工表面残余应力可以为拉应力也可以为压应力,残余应力作用层深度为300μm左右.对残余应力影响较大的切削因素为切削速度和进给量,切深对残余应力影响较小,切削参数选择低速低进给时,容易得到有利于提高工件疲劳寿命的表面残余压应力.     

轴承套圈的预应力硬态切削分析

通过对轴承套圈工作状态的运动学和力学分析,明确了轴承工作时内圈先于静止外圈表面产生疲劳剥落的原因;阐述了轴承外圈外圆表面出现的残余拉应力现象和原因,并提出一种可改善轴承零件加工表面残余应力状态的预应力硬态切削方法。理论分析和实验结果证明,该方法可使轴承零件加工表面产生残余压应力,提高轴承的接触疲劳寿命。     

轴承钢硬态切削表面残余应力的研究

为了揭示轴承钢硬态切削中切削用量对工件已加工表面残余应力的影响规律,运用金属切削软件AdvantEdge在不同切削用量条件下进行了热力耦合切削仿真。结果表明:硬态切削后工件已加工表面出现残余压应力,随着深度的增加残余压应力值减小并逐渐转变为拉应力;切削速度和进给量对残余压应力影响较大,残余压应力最大值随着切削速度的增加呈先减小后增加的趋势,但作用深度变化较小,进给量增加时残余压应力最大值和作用深度均增加;背吃刀量增加时残余压应力最大值和作用深度变化幅度很小。研究结果可为残余应力控制和工艺参数优化提供理论指导。     

钻、铰工艺对铝合金紧固孔件疲劳寿命的影响

为研究钻、铰工艺对紧固孔件疲劳寿命的影响,分别对LY12CZ硬铝合金疲劳试样采用钻、铰两种工艺加工出孔并进行了疲劳试验,对钻、铰工艺下孔壁的表面形貌和粗糙度、切向残余应力以及试样的疲劳断口特征进行了测定和分析。结果表明:钻削后孔壁的表面较粗糙,其表面粗糙度为12.92μm,而铰削后孔壁表面非常光滑,其表面粗糙度为1.57μm;钻削孔壁表层的应力为残余拉应力,幅值为165MPa,而铰削孔壁表层的应力为残余压应力,幅值为78MPa;相比于钻孔试样,铰孔试样的疲劳条带间距较窄,裂纹扩展速率较低,其疲劳寿命是钻孔试样寿命的1.81倍。     

轴承圈加热切削加工表面质量研究

针对轴承圈易出现疲劳破坏的问题,提出采用预加热硬态切削加工轴承圈外表面的方法。普通硬态切削和预加热硬态切削试验结果表明,将工件内圈预先加热到160℃进行硬态切削加工,有助于减小加工表面的粗糙度,由于内圈加热减小了轴承圈内外表面的温度差,故加工后的表面残余应力显著减小,其值可达-50MPa,加工得到的表面纹理清晰,形貌光滑、规整,刀具进给运动轨迹清晰;加热切削得到的是均匀的锯齿形切屑,并且切屑形态呈螺旋状,与普通硬态切削相比,加热切削过程较为平稳,说明加热切削可获得良好的表面完整性,且不会引来额外的加工硬化。     

超声振动切削铝合金表面残余应力的有限元仿真

针对航空铝合金结构件加工的表面质量问题,利用有限元软件ABAQUS建立了基于Johnson-Cook本构的铝合金7050-T7451二维正交热力耦合模型。在相同的切削参数下,比较了传统切削、横向(即切削方向)振动切削和纵向(即轴向)振动切削加工的表面层残余应力,并研究了超声振动切削参数、振动频率、振动幅值下,对残余应力的影响规律;通过引用相关文献残余应力的实验数据,验证了仿真模型的正确性。研究结果表明:3种切削方式的表面残余应力均为压应力,沿深度方向向残余拉应力过渡,并且振动切削可以明显提高工件表面的残余压应力;表面残余压应力随切削速度和切深的提高而减小,表面残余压应力随着振幅或频率的增大而逐渐增大。     

加工残余应力对Ti-6Al-4V试样高周疲劳性能的影响

为探究加工残余应力对高周疲劳性能的影响,以Ti-6Al-4V材料为研究对象,测试获得了相同表面粗糙度、不同表面残余应力试样的高周疲劳性能.结果表明,该材料的疲劳试样在加工时会产生较高的残余压应力,不同加工工艺下的试样表面残余应力变化较大;在残余应力-寿命双对数坐标下,试样表面残余压应力和疲劳寿命近似成线性关系.随着应力...     

钛合金Ti-6Al-4V高压冷却车削过程有限元分析

随着钛合金的广泛应用,改善其切削加工性、提高加工表面完整性的试验研究也已得到广泛重视,但对该过程的仿真分析尚不成熟。通过Deform 3D仿真软件建立有限元仿真模型,模拟钛合金Ti-6Al-4V在干切削、普通冷却及高压冷却环境下的车削过程,研究切削环境对切削力、切削温度等加工过程量的影响,获取已加工工件距离加工表面不同深度的残余应力分布,分析高压冷却对钛合金Ti-6Al-4V加工表面残余应力的影响规律。通过钛合金Ti-6Al-4V车削试验测量切削力及刀具表面切削温度,并与有限元仿真模型对比,以验证其可靠性。仿真结果表明:随着切削液压强的增加,切削力增加,刀具表面切削温度降低,高压冷却可有效增强切削液的冷却作用。干切削时,已加工表面(d2=0)为残余拉应力;随着切削液压强的增加,已加工表面残余应力状态逐渐由残余拉应力向残余压应力转变,当切削液压强为200 bar时,已加工表面残余应力为残余压应力,且此时已加工表面残余压应力为最大值。随着测量深度的增加,残余应力值增大,在所有切削试验中,最大残余压应力值均在距离已加工表面相同距离。仿真结果与试验结果的对比证明了有限元仿真模型的可靠性,为钛合金Ti-6Al-4V高压冷却加工热力耦合分析和优化设计提供了理论依据。     

轴承钢顺次磨削表面残余应力离散度试验研究

以轴承钢顺次磨削表面的残余应力离散度为研究对象,基于X射线衍射法顺次测试了轴承套圈淬硬热处理、粗磨、精磨和超精磨削后,轴承滚道表面环向和轴向残余应力.测试结果表明,淬硬热处理工件的残余应力标准差约为超精工序的3倍;淬硬热处理轴承套圈经超精磨削工序,其表面的环向和轴向残余应力离散度降至20 MPa.研究表明淬硬轴承钢热处理及同一道磨削工序工件表面残余应力存在较大离散性,"粗磨-精磨-超精"顺次磨削工艺叠加后,工件表面残余应力离散度呈现收敛性;淬硬热处理轴承套圈经过顺次磨削工序叠加加工后,表面残余压应力平均值获得大幅提高.这为进一步系统揭示磨削工艺对淬硬轴承钢套圈表面残余应力及其离散度影响规律提供了科学数据.     

硬切削表层残余应力特征预测研究

结合精密硬切削加工表层残余应力曲线的勺形分布特征,提出了以表面应力值、最大应力值、最大深度值和有效深度值4个变量作为表达残余应力曲线的特征参数,并作为BP网络的输出量,以刀具几何参数和切削参数等影响硬切削加工最为显著的变量为输入量,建立了硬切削加工表层残余应力特征BP网络预测模型。最后,通过实验验证了模型的准确性,实现了对精密硬切削加工表面残余应力较高精度的预测。     

FE-simulation of the effects of machining-induced residual stress profile on rolling contact of hard machined components

Compared with grinding, hard turning may induce a relatively deep compressive residual stress. However, the interactions between the residual stress profile and applied load and their effects on rolling contact stresses and strains are poorly understood, and are difficult to measure using the current experimental techniques due to the small-scale of the phenomena. A new 2-D finite element simulation model of bearing rolling contact has been developed, for the first time, to incorporate the machining-induced residual stress profile instead of only surface residual stresses. Three cases using the simulation model were assessed: (a) measured residual stress by hard turning, (b) measured residual stress by grinding, and (c) free of residual stress. It was found that distinct residual stress patterns hardly affect neither the magnitudes nor the locations of peak stresses and strains below the surface. However, they have a significant influence on surface deformations. The slope and depth of a compressive residual stress profile are key factors for rolling contact fatigue damage, which was substantiated by the available experimental data. Equivalent plastic strain could be a parameter to characterize the relative fatigue damage. The magnitudes of machining-induced residual stress are reduced in rolling contact. The predicted residual stress pattern and magnitude agree with the test data in general. In addition, rolling contact is more sensitive to normal load and residual stress pattern than tangential load.     

Experimental study and evaluation methodology on hard surface integrity

The Taguchi method is adopted experimentally to investigate the surface integrity (surface roughness, residual stress, and thermal damage layer) of hardened bearing steel in hard dry turning, and the validation experiments are consequently performed. It was revealed that the value and effect sequence of optimal hard turning parameter varies with different objectives of surface integrity. However, it is quite difficult to select or determine the optimal combination of hard turning parameters. A hard-turned component performance, which reflects an integrated impact of surface integrity, should be fully recognized to resolve the inherent conflict in the selection process. Based on it, an evaluation methodology composed of four steps is proposed that surface integrity should be evaluated by the service/fatigue life of hard-turned components and therefore turning parameters. It bears significance for super-finish hard turning further application in respect that it provides an integrated approach for hard turning parameter optimization to achieve a superior surface integrity. Funded by the Ministry of Education of China- “985” of international cooperation project “Clean Manufacturing Technology”.     

Influence of Residual Stresses Introduced by Manufacturing Processes on Bearing Endurance Time

By enhancing surface properties and by reducing weight and size of machine elements, future trends in resource efficiency for machines can be fulfilled. Rolling element bearings are widely used machine elements. By improving their boundary zone properties, there is a potential to extend maintenance-free operating periods, postpone replacements or increase the lifespan of the complete system. The aim is to set favorable boundary zone properties by enhancing the residual stress state within the manufacturing process. For this, the processes hard turning and deep rolling were investigated. The influence of the initial residual stress state on fatigue life was calculated using a model based on the approach of Ioannides and Harris. The resulting residual stresses after the manufacturing process and their changes during operation in a bearing test rig are discussed and compared to those of standard bearings. The tests prove that pre-induced residual stresses increase is able to significantly delay rolling contact fatigue-related bearing failures.     

A Comparative Study of Residual Stress Distribution Induced by Hard Machining Versus Grinding

This study investigates the residual stress distribution induced by hard machining and grinding and compares its impact on fatigue parameters. The residual stress distribution below hard turned and ground surfaces is investigated after a thermally damaged layer is removed. Fatigue parameters are computed based on the residual stress distribution to compare the impact of the residual stress distribution on the fatigue performance. Rolling contact fatigue tests are then performed to substantiate the computations. The effect of residual stresses on crack initiation depth is shown to be significant for the ground specimen. The maximum shear stress at crack initiation depth of the hard turned specimen is smaller than that of the ground specimen. Due to a significant increase in crack initiation life, the predicted rolling contact fatigue life of the hard turned specimen is longer than that of the ground specimen. The overall average in the ratios of predicted life to experimental life for the hard turned specimen is closer to 1 than that for the ground specimen. The results demonstrate that the hard turned specimen shows better rolling contact fatigue performance and better accuracy in the fatigue life prediction.     

A Theoretical Study of Residual Stress Effects on Fatigue Life Prediction

Recently, the trend has been toward the use of the full subsurface stress field in rolling element bearing fatigue life prediction (stress field-based life models). By using the stress field-based bearing life models, more accurate assessments of such things as fitting practice and thermal treatments on the bearing performance are achieved. However, one aspect missing in most models has been the consideration of the changing residual stress during operation of the bearing. This study was conducted to investigate the time dependent residual stress on contact fatigue life predictions.

This study concluded that the changes in residual stress during operation were most likely a fatigue reaction of the material to the pre-fatigue residual stress and cyclic contact stress fields. The materials fatigue response changes the instantaneous values of the material constants in most stress field-based life equations, thus making them in-calculable. As such, the pre-fatigue residual stress field should be used in the stress field-based models.     

Improving surface integrity in finish machining of Inconel 718 alloy using intelligent systems

In machining of hard materials, surface integrity is one of the major customer requirements which comprise the study of the changes induced to the workpiece. Surface roughness and residual stress are often considered as the most significant indications of surface integrity. Inducing tensile residual stress during the machining processes is a critical problem which should be avoided or minimized to obtain better service quality and component life. This problem becomes more evident in the presence of rough machined surface because fatigue life of manufactured components might be decreased significantly. Inconel 718 superalloy is one of the hard materials used extensively in the aerospace industries. It is prone to tensile residual stress in machined surface. Thus, controlling and optimizing residual stress and surface roughness in machining of Inconel 718 are so needed. Intelligent techniques based on the predictive and optimization models can be used efficiently for this purpose. In this study, the optimal machining parameters including cutting speed, depth of cut, and feed rate were accessed by intelligent systems to evaluate the state of residual stress and surface roughness in finish turning of Inconel 718. The results of experiments and analyses indicated that implemented techniques in this work provided a robust framework for improving surface integrity in machining of Inconel 718 alloy. It was shown that cutting speed has more effect on surface integrity than other investigated parameters. Also, depth of cut and feed rate were found in the moderate range to obtain satisfactory state of tensile residual stress and surface roughness.     

滚动轴承疲劳寿命的影响因素

对影响滚动轴承疲劳寿命的各种因素进行了综述，包括各种疲劳诱导应力(最大切应力、最大动态切应力、Von Mises应力和八面切应力)，切向力、残余应力和环向应力疲劳极限应力、表面粗糙度、弹流润滑、表面处理、润滑油中污染颗粒、温度、速度、不失效寿命和钢材纯净度(氧含量)的影响，为轴承寿命的准确预测提供参考。     

Rolling contact fatigue life model incorporating residual stress scatter

There has been a considerable body of research concerned with predicting the service life of rolling contact components. It is well known that the prevailing cause of failure in rolling contact components is fatigue crack. Although the trend has been toward the use of surface integrity in fatigue life prediction, one aspect missing in most models has been a consideration of the residual stress scatter in the subsurface. Since the fatigue life of a manufactured component depends on its weakest point, the local extreme is most relevant for the fatigue life prediction. This study thus incorporates the residual stress scatter into the rolling contact fatigue life model to predict the fatigue life closer to the experimental life. It is noted that residual stresses vary significantly at the same depth. After the residual stress scatter is incorporated into the model, the predictions agree well with the experimental lives.     

精密硬车加工轴承套圈的表面完整性试验研究

针对磨削加工中套圈精密加工存在的不足,进行精密硬车削加工轴承套圈新工艺的开发,通过加工试验分析了精密硬车加工轴承套圈的表面完整性,探究了基准面平面度、刀具磨损量等工艺参数与加工精度的对应关系。基于精密硬车削套圈试样的表面粗糙度、沟道圆度、显微硬度、热损伤、金相组织、残余应力分布、加工效率等方面的研究,得出了精密硬车削可达到磨削加工精度的结论,且金相组织稳定,不易存在热损伤,具有可控的残余应力分布和较高的加工效率,有利于产业化生产高精密轴承。利用磁性卡盘装夹套圈,分析试样基准面平面度对精密硬车削套圈沟道圆度的影响,发现提高基准面平面度可以有效提高加工套圈的沟道圆度;分析了刀具磨损对硬车削套圈加工精度的影响,得出在精密加工阶段刀具磨损量是控制套圈圆度的重要监控工艺参数的结论。     

Residual stresses and retained austenite evolution in SAE 52100 steel under non-ideal rolling contact loading

Residual stresses are introduced and modified during manufacturing as well as by normal use under rolling contact loading. Operations such as heat treatments, shot peening, grinding, etc., are known to alter the magnitude and distribution of residual stresses. Our work revolves around the changes in magnitude and distribution of residual stresses, as they relate to deformation and the strain induced transformation of retained austenite. The residual stresses and retained austenite measurements were carried out using X-ray diffraction techniques. The rolling contact fatigue lives of different variants of SAE 52100 bearing steel were evaluated in a 5-ball-rod rolling contact fatigue machine under testing conditions leading to surface nucleated failure, i.e. non-ideal rolling contact. The tests were accelerated by applying well controlled micro-indentations on the wear track. The contribution of the residual stresses and amount of retained austenite to the rolling contact fatigue life were analyzed.