铝合金车轮弯曲试验疲劳寿命预测研究

弯曲疲劳试验是汽车车轮三项性能试验中失效频率较高的一项.文中建立弯曲试验的有限元模型,使用I-DEAS有限元分析软件进行静力分析,分别采用名义应力法和局部应力应变法, 结合Manson-Coffin、Simth-Waston-Topper损伤公式预测铝合金车轮弯曲试验的疲劳寿命.通过与某型16×6.5J车轮试验对比,证明Simth-Waston-Topper方法预测铝合金车轮弯曲疲劳寿命更接近试验寿命.     

基于变幅小载荷下的曲轴疲劳寿命预测分析

通过ABAQUS对曲轴模型进行有限元分析,得到局部最大时间应力载荷谱.运用雨流计数法对载荷谱进行处理,得到各应力幅值下的循环数.采用修正Corten-Dolan累积损伤理论,结合变幅载荷的应力幅值对曲轴进行疲劳寿命预测.通过分析,低于疲劳极限的应力会对曲轴产生强化作用,影响曲轴的疲劳寿命.     

基于多因素修正的超越离合器保持架疲劳寿命分析

以超越离合器保持架为研究对象,针对其交变载荷作用下易发生疲劳断裂的现状,首先利用有限元分析手段获得其模拟载荷谱,然后建立残余应力修正载荷谱的数学模型并在此基础上完成模拟载荷谱的修正,最后将修正后的分析载荷谱及材料的疲劳性能参数导入多因素修正后的名义应力法疲劳寿命计算软件中,对保持架的疲劳寿命进行求解,并通过台架试验加以验证。通过对比数值分析与试验可以发现结果基本吻合,基于多因素复合修正的疲劳寿命分析方法不仅增加了分析数据的可靠性,而且为零件疲劳寿命预估提供了新的技术路径。     

用当量S—N曲线估算疲劳裂纹形成寿命

介绍了一种利用相对Ｍｉｎｅｒ法则估算构件在变幅载荷谱下裂纹形成寿命的当量Ｓ－Ｎ曲线方法。与常规的名义应力法相比，此方法不用常幅试验下得到的Ｓ－Ｎ曲线，而是根据该构件在两种载荷谱下的疲劳试验寿命，推导出能反映在变幅载荷谱条件下构件疲劳特性的当量Ｓ－Ｎ曲线为依据寿命估算。运用此方法，本文对文献（１）所给六种载荷谱下的试片寿命进行了计算，并以试验寿命为依据对按常规Ｓ－Ｎ曲线法修正的Ｓ－Ｎ曲线法，局部应力     

随机载荷循环作用下的机械结构疲劳寿命预测模型

基于名义应力法建立了随机载荷循环作用下的结构疲劳寿命预测模型。分析了结构所受循环载荷作用的不确定性特征,在以循环载荷作用次数为寿命度量指标框架下,运用概率加权法和线性Miner累积损伤法则,分别建立了疲劳寿命与应力之间关系分别服从指数函数和幂函数两种形式时,随机载荷循环作用下的结构疲劳寿命预测模型,并运用所建立的模型对某转动轴的疲劳寿命进行了预测研究。     

CRH3型动车组车轮的疲劳寿命分析

为了真实计算动车组车轮疲劳寿命,在分析国内外车轮相关标准的基础上,提出了利用车轮静强度分析和有限元名义应力方法的高速动车组车轮强度的分析方法.基于UIC510-5标准,确定了车轮强度分析的计算载荷工况,利用有限元静强度分析方法对CRH3型动车组车轮进行疲劳强度评价,结果表明机械载荷工况下车轮强度满足要求;最后基于线性损伤累积法则,利用有限元名义应力方法和ANSYS/WORKBENCH得出车轮的疲劳寿命预测图及安全系数图,计算结果满足疲劳寿命要求,为动车组的安全性维护提供了理论依据,对动车组的安全运行有极强的实际应用价值.     

结构有限寿命设计法——名义应力法

介绍了一种结构有限寿命设计方法——名义应力法。阐述了名义应力有限寿命设计法的一般步骤,并对设计方法中的几个关键问题如应力谱的简化处理、疲劳寿命的预测等做了详细的介绍。以线性累积损伤法则和应力-寿命曲线为依据,推导出适用于变幅载荷下的有限寿命设计公式。最后通过算例说明采用此方法的优越性。     

某型飞机机翼Ⅱ梁框疲劳寿命研究

某型飞机机翼Ⅱ梁框是重要的受力部件,必须准确估计疲劳寿命,以预防疲劳事故的发生。采用名义应力法和局部应变法两种方法及Miner累积损伤理论估计疲劳裂纹形成寿命;在随机载荷谱转化为等幅载荷谱的基础上通过Walker方程求得疲劳裂纹扩展寿命,从而估算出某型飞机机翼Ⅱ梁框的疲劳寿命。估算结果与试验结果吻合很好。     

汽车铝合金轮毂抗疲劳设计研究

以14×6JJ铝合金汽车轮毂为研究对象,在载荷谱分析的基础上,运用具有较高寿命估算精度和安全性的累积损伤理论—修正Miner法则,进行轮毂变幅载荷下的疲劳强度评价和寿命估算。运用可靠度理论,对预测得到的轮毂寿命进行可靠度计算。结果表明,修正Miner法则对于预测汽车轮毂的疲劳寿命具有较高的可靠性。     

齿轮弯曲疲劳寿命及可靠性分析研究

齿轮是传动系统中的关键部件,对其疲劳寿命及可靠性研究非常重要.采用了名义载荷法完成齿轮疲劳寿命的估算并对其可靠性进行研究.将齿轮材料属性定义为结构钢,给定齿轮工作载荷谱,并基于疲劳损伤理论Miner,完成时齿轮疲劳寿命的研究.     

Minimal Realization of Linear Graph Models for Multi-physics Systems

An engineering system may consist of several different types of components,belonging to such physical"domains"as mechanical,electrical,fluid,and thermal.It is t...     

INTEGRAL EQUATION METHOD＇S APPLICATION IN HOLE-EDGE STRESS OF COMPOSITE MATERIAL PLATE WITH DIFFERENT SHAPED HOLES

The strength of composite plate with different hole-shapes is always one of the most important but complicated issues in the application of the composite material. The holes will lead to mutations and discontinuity to the structure. So the hole-edge stress concentration is always a serious phenomenon. And the phenomenon makes the structure strength decrease very quickly to form dangerous weak points. Most partial damage begins from these weak points. According to the complex variable functions theory, the accurate boundary condition of composite plate with different hole-shapes is founded by conformal mapping method to settle the boundary condition problem of complex hole-shapes. Composite plate with commonly hole-shapes in engineering is studied by several complex variable stress fimction. The boundary integral equations are founded based on exact boundary conditions. Then the exact hole-edge stress analytic solution of composite plate with rectangle holes and wing manholes is resolved. Both of offset axis loadings and its influences on the stress concentration coefficient of the hole-edge are discussed. And comparisons of different loads along various offset axis on the hole-edge stress distribution of orthotropic plate with rectangle hole or wing manhole are made. It can be concluded that hole-edge with continuous variable curvatures might help to decrease the stress concentration coefficient; and smaller angle of outer load and fiber can decrease the stress peak value.     

Non-monotonic material contrast in scanning ion and scanning electron images

30 keV Ga⁺ focused ion beam induced secondary electron (iSE) imaging was used to determine the relative contrast between several materials. The iSE signal compared from C, Si, Al, Ti, Cr, Ni, Cu, Mo, Ag, and W metal layers does not decrease with an increase in target atomic number Z₂, and shows a non-monotonic relationship between contrast and Z₂. The non-monotonic relationship is attributed to periodic fluctuations of the stopping power and sputter yield inherent to the ion–solid interactions. In addition, material contrast from electron-induced secondary electron (eSE) and backscattered electron (BSE) images using scanning electron microscopy (SEM) also shows non-monotonic contrast as a function of Z₂, following the periodic behavior of the stopping power for electron–solid interactions. A comparison of the iSE and eSE results shows similar relative contrast between the metal layers, and not complementary contrast as conventionally understood. These similarities in the contrast behavior can be attributed to similarities in the periodic and non-monotonic function defined by incident particle–solid interaction theory.     

Application of Feature Extraction through Convolution Neural Networks and SVM Classifier for Robust Grading of Apples

This paper proposes a novel grading method of apples,in an automated grading device that uses convolutional neural networks to extract the size,color,texture,an...     

分布动态载荷识别的抗噪处理

针对正交多项式频域法在用多种响应对矩形薄板进行载荷识别中抗噪性较差的问题,综合运用平均法、矩阵预处理和奇异值截断法等方法对之进行改善,并引入空间映射的思想,将该方法的应用范围拓展为复杂的模型.利用仿真算例,证实了该方法具有较好的抗噪性.     

基于MELTAC-N平台的核电厂安全级DCS环网研究与测试

针对工程实践中环网通讯相关问题的处理缺乏理论基础及国产化安全级DCS平台的开发缺乏成熟经验借鉴问题,对基于MELTAC-N平台核电厂安全级DCS环网的软硬件实现进行了研究。提出了安全级DCS环网双环网冗余设计、光切换开关设计等硬件设计方法,以及以RPR协议为基础,采用全数据收发策略的软件设计方法。在CPR1000安全级DCS平台上对安全级DCS环网的可靠性及实时性进行了评价,并进行了容错能力、响应时间及响应时间稳定性测试验证实验。结果表明,基于MELTAC-N平台安全级DCS环网软硬件设计具有较好的容错能力及响应时间稳定性。     

Short-Term Relay Quality Prediction Algorithm Based on Long and Short-Term Memory

The fraction defective of semi-finished products is predicted to optimize the process of relay production lines, by which production quality and productivity ar...     

End-to-End Multiview Gesture Recognition for Autonomous Car Parking System

The use of hand gestures can be the most intuitive human-machine interaction medium.The early approaches for hand gesture recognition used device-based methods....     

The laboratory simulation of abrasive wear

Abrasive wear has long been recognised as one of the most potentially serious tribological problems facing the operators of many types of plant and machinery; several industrial surveys have indicated that wear by abrasion can be responsible for more than 50% of unscheduled machine and plant stoppages. Locating the operating point of a tribological contact in an appropriate operational ‚map’︁ can provide a useful guide to the likely nature and origins of the surface degradation experienced in use, though care must be exercised in choosing the most suitable parameters for the axes of the plot. Laboratory testing of materials and simulations of machine contacts are carried out for a number of purposes; at one level for the very practical aims of ranking candidate materials or surface hardening treatments in order of their wear resistance, or in an attempt to predict wear lives under field conditions. More fundamentally, tests may be aimed at elucidating the essential physical mechanisms of surface damage and loss, with the longer term aim of building an analytical and predictive model of the wear process itself. In many cases, component surface damage is brought about by the ingress of hard, particulate matter into machine bearing or sealing clearances. These may be running dry although, more usually, a lubricant or service fluid is present at the interface. A number of standardised wear test geometries and procedures have been established for both two- and three-body wear situations, and these are briefly described. Although abrasive wear is often modelled as following an ‚Archard’︁ equation (i.e. a linear increase in material loss with both load and time, and an inverse dependence on specimen hardness) both industrial experience and laboratory tests of particularly lubricated contacts show that this is not always the case: increasing the hardness differential in an abrasively contaminated lubricated pair may not always reduce the rate of damage to the harder surface.     

ANGULAR DISTORTION ALLOWABLE VALUE AND ASSESS METHOD OF WELD ON COKE TOWER

A graph as the new engineering method for estimate the safety of bulging deformation of coke tower is proposed. Through stresses analysis of circumferential weld of coke tower and comparing the stresses produced by pressure with heat stress of steady state, residual stress, bending stress produced by both itself weight and wind loads, it showed that the stresses produced by pressure on the angle distortion are the main factor of equivalent stress of the combined stress. After comparing four kinds of stress controlling conditions, the relation to stress with depth of angular distortion, grade of curvature of angular distortion and half of region of angular distortion has been inferred. Graph of deformation allowable value of coke tower for different condition by angular distortion and half of region of angular distortion has been plotted. The five steps for its engineering use have been explained. The lighter the grade of curvature is, the larger of bulge allowance, may be, and the bigger of depth of angular distortion may pose too. For the coke tower with a popular structure of Dg 5 400 mm×28 mm, the result by graph is nearly more than the result of two formulas formed by other research, the error is less than 7.0%. But, the graph can be easily applied to different size of angular distortion.