一种轿车车轮应力状态测量与分析方法

基于台架应变测试试验方法,研究轿车车轮在疲劳试验中的应力状态。结果表明:车轮的径向疲劳试验时,轮胎会对车轮的载荷产生较大的影响,轮胎与转鼓的挤压变形以及正反转动都会对车轮的应力状态产生影响;车轮径向疲劳试验时,最大应变出现在轮辋与轮胎接触位置沿车轮圆周方向,而在靠近轮心位置的应变较小;车轮弯曲疲劳试验时,最大应变出现在轮辐靠近轮心的位置,最大应变出现在轮辐的长度方向;不同的载荷对车轮应变的变化规律并没有影响,但是会对最大和最小峰值产生影响。     

冲角工况下列车车轮损伤机理研究

曲线通过和蛇行运动时将会在轮轨间产生一定的冲角,为探究列车车轮在冲角工况下的损伤机理,利用JD-1轮轨模拟试验机对列车车轮进行滚动接触疲劳试验.结果表明:在冲角工况下车轮试件磨痕的不同区域存在不同的损伤机理,按损伤机理的不同可以将其分为塑性堆积区、疲劳损伤区和磨损区三个区域.在应力发生剧烈变化且应力方向由高应力区指向低应力区的区域将会出现材料的塑性堆积,并且在堆积处产生疲劳裂纹.滚动接触下的疲劳裂纹可以萌生于表面和亚表面,在较强应力作用下,车轮材料的晶粒发生了明显的细化,在横截面上呈现出纤维状组织.     

轮对结构柔性对车轮辐板疲劳寿命的影响

针对高速动车非轴对称车轮辐板区域随机疲劳寿命问题,分别将轮对视为刚性体和柔性体建立了车辆-轨道系统动力学模型,仿真得到载荷时间历程和轮轨接触点在踏面上的位置时间历程。在三维有限元模型中使用约束方程模拟轮轴过盈配合,使非线性问题线性化,采用准静态叠加法得到应力时间历程。基于临界距离法中的点法,以疲劳破坏临界平面上的正应力为主循环计数参数,剪应力为辅助计数参数进行多轴循环计数,结合Spagnoli法和Miner理论研究了轮对结构柔性和车轴刚度对车轮辐板随机疲劳寿命的影响。研究结果表明,轮对结构柔性对车轮辐板疲劳寿命有较大影响。随着车轴刚度的降低,轮轨接触横向力的幅值显著增大,轮对模态的特征频率和车轮辐板区域的寿命降低。因此,在轮对轻量化设计时,需综合考虑车轴的结构刚度。     

油管的疲劳强度分析

疲劳断裂是油管失效的一种形式 ,本文针对抽油机井常用油管 (J5 5 ,2 1/ 2″)在循环载荷作用下的疲劳断裂问题进行了理论与实验研究。在实测油管载荷谱与应变谱的基础上应用弹塑性有限元法计算油管螺纹内的应力应变场 ,并进行了有关的疲劳实验 ,以得到油管的疲劳强度。油管内第一啮合齿齿根处应力应变最大 ,应力已经达到屈服阶段 ,油管是在高应力应变水平和低应力应变幅状态下工作。当油管内的应力应变进入强化段εeq >1 0 - 2 ε,塑性应变幅超过 4× 1 0 - 5ε时 ,油管就会发生疲劳断裂     

高应力比循环下微动疲劳裂纹萌生位置的预测分析

对于微动疲劳问题,循环应力比的大小会影响试件应力状态及分布,从而影响疲劳裂纹的萌生位置.本文通过对一类微动疲劳问题进行有限元法分析,模拟疲劳实验过程,并采用最大应力变化幅△σθmax作为指标预测了不同应力比下疲劳裂纹的萌生位置.数值分析显示,在应力比不是很大时,试件与微动接触头的边缘存在接触,并在此处产生较大的应力集中,容易萌生裂纹;而在应力比足够高时,微动接触头端部与试件呈恒张开状态,△σθmax及裂纹萌生发生在距初始接触区边缘一定距离处.疲劳裂纹萌生位置的理论预测结果与相关试验的疲劳裂纹发生位置比较一致.     

油管的疲劳强度分析

疲劳断裂是油管失效的形式之一,本文针对抽油机井常用油管(J55,2 ")在循环载荷作用下的断裂问题进行了理论与实验研究。实测了井口处油管载荷谱与应变谱,得到了油管载荷的变化规律,同时通过在室内建立模拟油管工况的试验台,得到了油管从上扣到加载的全过程中油管螺纹段内壁的环向、轴向、剪应变等的变化规律。并且采用油管螺纹段轴对称接触模型进行了弹塑性有限元分析,计算了油管螺纹内的应力应变场,发现油管内第一啮合齿齿根处应力应变最大,应力已经进入屈服阶段,油管是在高应力应变水平和低应力应变幅状态下工作。并利用局部应力应变法进行了相应的疲劳实验,得到油管的疲劳断裂条件,当油管内的应力应变进入强化段εeq>10-2ε,塑性应变幅超过4×10-5ε时,油管就会发生疲劳断裂。     

磨损加疲劳载荷下的协同疲劳行为

自行研制的摩擦磨损装置与轴向疲劳试验机相互配合,实现GDL-1钢试样在疲劳应力(240~280 MPa)及接触载荷(30 N)作用下摩擦磨损疲劳试验.通过对磨损层厚度的分析,研究试样承受摩擦磨损载荷及拉压疲劳载荷双重作用下的疲劳寿命变化,用SEM扫描电镜观察分析次表层内疲劳裂纹扩展的演变过程,并采用Hertz线弹性理论和Smith接触理论计算分析摩擦表面以下切应力值.结果表明:在磨损疲劳载荷作用下,形变层的流变作用将显著影响疲劳小裂纹扩展方向,渐趋于切应力方向,从而提高试样疲劳寿命.在此基础上,建立了在摩擦磨损疲劳载荷下疲劳裂纹扩展模型.此外,计算可知在距表层深度0.03 mm处切应力最大,0.18 mm以内材料产生塑性变形,导致形变层的形成.     

近场动力学框架下钢轨疲劳裂纹萌生预测的数值方法研究

经典连续介质力学在求解由裂纹引起的不连续问题时，会出现数学构架失效的情况. 为克服这一难题，基于近场动力学理论，构建铁路钢轨疲劳裂纹萌生的数值预测方法，可实现钢轨疲劳裂纹萌生寿命与位置的预测. 当未出现疲劳裂纹时，通过与经典连续介质力学模型的结果对比，验证近场动力学模型的正确性和适用性. 分析了车轮全滑动、黏着-滑动和无摩擦三种状态对钢轨疲劳裂纹萌生的影响规律，结果表明:车轮由全滑动向无摩擦转变的过程中，裂纹萌生位置由钢轨表层转移到内部，裂纹萌生所需的荷载循环次数由0.45×107次增至2.05×107次，可见车轮滚滑状态会影响裂纹的萌生位置，并且较大的切向接触应力会显著降低钢轨的疲劳裂纹萌生寿命.      

采用显微网格法研究韧性材料平面应力状态下裂尖附近的应变场

用显微网格数字图象处理方法，测量了韧性材料平面应力条件下Ｉ型单边裂纹尖端附近的应变场。实验结果表明：在裂尖两侧存在与裂纹方向夹角约为５０°的大变形带。最大应变位于离裂尖一定距离的大变形带上，随着载荷增加，最大应变的位置逐渐靠近裂纹尖端。应变峰值轨迹线在裂纹顶端呈放射状，载荷增加时，应变峰值的轨迹线位置并不改变。     

ANALYSIS OF GROUNDING CHARACTERISTICS AND STRAIN ENERGY OF RADIAL TIRES WITH RADIAL STIFFNESS1)

利用轮胎综合试验机对径向刚度下子午线轮胎进行性能试验,采用正交试验法针对不同胎压、垂向载荷下轮胎的接地特性进行分析,结合仿真软件ABAQUS与试验进行对比。结果表明,橡胶材料Mooney-Rivli模型也具有一定的适用性,胎压增大时径向刚度发生线性变化,胎面印痕由椭圆形转变成近似矩形,印痕面积略微增大;随着胎压的不断增大,胎面印痕的面积显著减小,接触面的压力主要集中在胎肩,胎冠处也有所增加;胎压一定时,垂向载荷逐渐增大时,整个印痕面的应力呈对称分布,印痕面应力由内高外低逐渐向外高内低变化。建立数学模型与有限元软件同时对轮胎进行应变能分析,发现在低胎压150 kPa下受载荷时轮胎容易发生微小侧向位移同时发生变形,此时极易引起迟滞损失并造成应变能急剧增加。     

Experimental analysis of vertical soil reaction and soil stress distribution under off-road tires

In this study, the vertical soil reaction acting on a driven wheel was measured by strain gages bonded to the left rear axle of a 2WD tractor driven under steady-state condition on different soil surfaces, tractor operations, and combinations of static wheel load and tire inflation pressure. In addition, the measurements of radial and tangential stresses on the soil–tire interface were made simultaneously at lug’s face and leading side near the centerline of the left rear tire using spot pressure sensors. The experimental results indicate that the proposed method of vertical soil reaction measurement is capable of monitoring the real-time vertical wheel load of a moving vehicle and provides a tool for further studies on vehicle dynamics and dynamic wheel–soil interaction. Furthermore, the measured distributions of soil stresses under tractor tire could provide more real insight into the soil–wheel interactions.     

不同材料参数和内压的轮胎对单腹板轮毂变形的影响

将轮胎材料简化为各向同性超弹性材料特性，考虑轮胎与轮毂和地面之间的三维接触以及轮胎中钢丝圈的影响，建立飞机单腹板机轮整体结构有限元模型。主要分析不同轮胎材料参数和内压下，单腹板轮毂轮缘处的径向变形，结果表明；轮毂剖面上测点的应变值与实验结果基本一致。轮胎下沉量与轮毂测点的径向变形和轮毂所受的载荷基本呈线性关系；凸出一侧的轮缘变形最大；轮胎下沉量较大时。轮胎材料参数对轮毂的径向变形影响明显；轮毂测点径向变形在1-2.5mm时，相同的径向变形，轮毂受到的总载荷受轮胎材料参数变化而变化，而在变形较大或较小时，影响不明显。对于同一种轮胎材料，不同的内压，轮毂的变形减轻比较大，气压越高，对于相同的轮胎下沉量，轮毂受到总体荷载也越高。     

子午线轮胎接触变形的结构有限元分析

针对195／60R14子午线轮胎建立了三维非线性有限元模型，着重研究了额定充气压力及静载荷作用下帘线承受拉应力和剪应力的基本特征。计算结果表明，接地区域摩擦力呈斜对称分布，反映了轮胎中帘线-橡胶复合材料存在变形耦合效应；冠带层、带束层、胎体帘线应力分布较为复杂，载荷变化对其应力水平和分布影响较大；在胎肩部位应力较高，且随载荷变化局部帘线应力变化剧烈，在承受交变载荷时，易形成层间剥落。分析结果有助于预测轮胎的使用性能，可以针对性地应用于因轮胎结构设计引起的质量损坏，某些对轮胎使用性能不利的受力状态可通过结构的优化设计来克服。     

一种用于金属薄板轴向拉压疲劳试验的防弯夹具

在金属薄板的轴向疲劳S-N曲线测试中,研究将一种侧向防弯曲夹具应用于存在压向载荷的试验。通过粘贴应变片方法测量试样的表面应力,对试样的受力情况做了定量的分析。测量结果表明试样安装防弯曲夹具后,基本消除了由压缩失稳产生的弯曲应力。且通过对不同拧紧方式的测量,表明一定的夹紧力下不对试验力产生影响。试验夹具设计成对试样中心轴线的支撑而让边缘疲劳敏感部位处在非接触状态,试样断口表明疲劳起源在这些并没有与试样接解的部位。用钛和铝两种材料的薄板在不同试验机上进行了不同寿命和频率的试验,试验结果与正应力比试验同时给出以对比,各种研究表明本试验有效解决了薄板疲劳受压时的失稳问题。     

Prediction of soil vertical stress under off-road tire using smoothed-particle hydrodynamics

Evaluation of vertical stress distribution in clay-loam soil using Smoothed-Particle Hydrodynamics-Finite Element Analysis (SPH-FEA) technique is presented in this research. The moist soil is modelled using the hydrodynamic elastic–plastic material and Murnaghan equation of state, while the tire is modelled using FEA in Visual Environment’s Pam-Crash software. Soil-tire interaction is performed using the node symmetric node to segment with edge treatment method. A single-wheel tester in a soil bin environment was utilized to provide experimental data. The objectives of the experimental test were to (1) calculate maximum subsoil stresses in the subsoil at 1 to 15 passes of a wheel with loads of 1, 2, 4, and 5 kN on soil with moisture levels of 0, 10, 17, and 24%.; (2) calibrate soil with different levels of moisture (3) compare predicted soil stresses with experiments. The maximum stress at 20 cm depth increased with increasing soil moisture and also with high levels of tire load. In contrast, successive traffic showed a decreasing effect on soil stress. The coefficient of determination 0.97 shows the predictions agreed very well with experiments. The moist soil-tire interaction model will be further used to analyze the soil stress in different soil depths and different forward velocity.     

The effect of inflation pressure and vehicle loading on the sidewall of a radial tire

The sidewall is one of the regions where service failures occur in a pneumatic tire. Knowledge of the stresses or strains developed in the sidewall under varying service conditions is required if such pneumatic-tire failures are to be avoided. This paper describes an experimental investigation into the effect of inflation pressure, vehicle load and camber angle on the sidewall-surface strains in a radial tire. Photoelastic coating and a specially designed strain-gaging technique were used. For pure-inflation pressure, the magnitude of the measured shear strains in the sidewall is directly related to the inflation pressure. The maximum sidewall shear strains in pure inflation are located in the lower sidewall (18 mm from bead), irrespective of the magnitude of the inflation pressure. The mendional sidewall strain is predominant in the inflated but otherwise unloaded tire. The meridional strain is proportional to the square root of the inflation pressure. The maximum mendional strain is located in the mid-sidewall region. For a constant vehicle loading, there is a transition inflation pressure below or above which the circumterential shoulder strain increases sharply. This observation highlights the importance of maintaining satistactory inflation pressure in passenger-car tires as an under-inflated tire will induce severe strain development at the shoulder. In addition to the vehicle load, the introduction of camber angle produces localized change in the meridional and circumterential strains within the contact zone. The increase of camber angle up to 10 deg causes continuous increase in the meridional strain in the lower sidewall but decrease in the upper sidewall. The mid-sidewall meridional strains remain practically unchanged. The circumferential strains along the load line are, in general, lower due to the increase in camber angle.     

Stress and fatigue life analyses of a five-piece rim and the proposed optimization with a two-piece rim

A five-piece rim and a two-piece bolt-connected rim were investigated to examine stress levels and fatigue lives on critical regions. The finite element models of the rim/tire assemblies were developed and validated through tire engineering data and previously validated modelling approaches. The rim/tire assemblies were simulated under two conditions, (1) application of a 23,100 kg static load followed by a 24.14 km/h travelling speed and an 82° wheel angle, and (2) application of a 26,900 kg static load followed by an 8.05 km/h travelling speed and an 82° wheel angle. The results revealed that travelling and steering speeds were the key factors in causing high stresses and bolt tension forces. Compared to the five-piece rim, the two-piece rim decreased the maximum stresses by over 30% for both loading conditions; consequently the fatigue lives were increased by over two orders of magnitude. The maximum bolt forces for the two-piece rim were estimated to be 195,680 N and 111,360 N separately.