A rigid-flexible coupling finite element model of coupler for analyzing train instability behavior during collision

Rail vehicles generate huge longitudinal impact loads in collisions.If unreasonable matching exists between the compressive strength of the intermediate coupler and the structural strength of the car body,the risk of car body structure damage and train derailment will increase.Herein,a four-stage rigid-flexible coupling finite element model of the coupler is established considering the coupler buckling load.The influence of the coupler buckling load on the train longitudinal-vertical-hori-zontal buckling behavior was studied,and the mechanism of the train horizontal buckling instability in train collisions was revealed.Analysis results show that an intermediate coupler should be designed to ensure that the actual buckling load is less than the compressive load when the car body structure begins to deform plastically.The actual buckling load of the coupler and the asymmetry of the structural strength of the car body in the lateral direction are two important influencing factors for the lateral buckling of a train collision.If the strength of the two sides of the car body structure in the lateral direction is asymmetrical,the deformation on the weaker side will be larger,and the end of the car body will begin to deflect under the action of the coupler force,which in turn causes the train to undergo sawtooth buckling.

Complete geometric nonlinear formulation for rigid-flexible coupling dynamics

A complete geometric nonlinear formulation for rigid-flexible coupling dynamics of a flexible beam undergoing large overall motion was proposed based on virtual work principle, in which all the high-order terms related to coupling deformation were included in dynamic equations. Simulation examples of the flexible beam with prescribed rotation and free rotation were investigated. Numerical results show that the use of the first-order approximation coupling (FOAC) model may lead to a significant error when the flexible beam experiences large deformation or large deformation velocity. However, the correct solutions can always be obtained by using the present complete model. The difference in essence between this model and the FOAC model is revealed. These coupling high-order terms, which are ignored in FOAC model, have a remarkable effect on the dynamic behavior of the flexible body. Therefore, these terms should be included for the rigid-flexible dynamic modeling and analysis of flexible body undergoing motions with high speed.

Numerical simulation of aircraft arresting process with an efficient full-scale rigid-flexible coupling dynamic model

The arresting process of carrier-based aircraft is widely recognized as a challenging task,characterized by the highest accident rate among all carrier-based aircraft operations.Dynamic simulation plays a crucial role in assessing the intricate responses of the arresting process,favoring the design of carrier-based aircraft.An efficient and accurate rigid-flexible coupling model for analyzing the dynamic response of the arresting process is proposed.By combining the dynamic characteristics of airframe,landing gear,arresting hook and arresting gear system,the rigid-flexible coupling dynamic model is established to reflect the relative motion of the coupling parts and arresting load.The dynamic model is verified through simulations of landing gear landing drops and by comparing the arresting simulation results with corresponding data in the US military standard.Additionally,simulations of the arresting process under different off-center distance and aircraft yaw angle are conducted to obtain the dynamic response of the aircraft during the arresting process.The result indicates that the rigid-flexible coupling dynamic model proposed is effective for analyzing the arresting dynamics response of carrier-based aircraft.The axial force of the arresting cable on both sides of the hook engagement point,pitch and yaw angle of aircraft are inconsistent under yaw and off-center arresting.The analysis method and obtained results provide valuable references for assessing the dynamic responses of carrier-based aircraft during arresting process and offer valuable in-sights in the design of carrier-based aircraft.

Thermo-mechanical coupled analysis of hot ring rolling process

A 3D rigid-plastic and coupled thermo-mechanical FE model for hot ring rolling(HRR) was developed based on DEFORM 3D software,then coupled heat transferring,material flow and temperature distribution of the ring in HRR were simulated and the effects of process parameters on them were analyzed.The results show that the deformation nonuniformity of ring blank increases with the increase of the rotational speed of driver roll and friction factor or the decrease of the feed rate of idle roll and initial temperature of ring blank.The temperature nonuniformity of ring blank decreases with the increase of the feed rate of idle roll or the decrease of initial temperature of ring blank and friction factor.There is an optimum rotational speed of driver roll under which the temperature distribution of ring blank is the most uniform.The results obtained can provide a guide for forming parameters optimization and quality control.

A DYNAMIC MODEL FOR ROCKET LAUNCHER WITHCOUPLED RIGID AND FLEXIBLE MOTION

The dynamics of a coupled rigid-flexible rocket launcher is reported. The coupled rigid-flexible rocket launcher is divided into two subsystems, one is a system of rigid bodies, the other a flexible launch tube which can undergo large overall motions spatially. First, the mathematical models for these two subsystems were established respectively. Then the dynamic model for the whole system was obtained by considering the coupling effect between these two subsystems. The approach, which divides a complex system into several simple subsystems first and then obtains the dynamic model for the whole system via combining the existing dynamic models for simple subsystems, can make the modeling procedure efficient and convenient.

A new numerical model of ring shear tester for shear band soil considering friction-induced thermal pressurization

In this study,a new numerical model of ring shear tester for shear band soil of landslide was established.The special feature of this model is that it considers the mechanism of friction-induced thermal pressurization,which is potentially an important cause of high-speed catastrophic landslides.The key to the construction of this numerical ring shear model is to realize the THM(thermo-hydro-mechanical)dynamic coupling of soil particles,which includes the processes of frictional heating,thermal pressurization,and strength softening during shearing of solid particles.All of these are completed by using discrete element method.Based on this new model,the characteristics of shear stress change with shear displacement,as well as the variation of temperature and pore pressure in the specimen,are studied at shear rates of 0.055 m/s,0.06 m/s,0.109 m/s and 1.09 m/s,respectively.The results show that the peak strength and residual strength of specimen are significantly reduced when the mechanism of frictioninduced thermal pressurization is considered.The greater the shear rate is,the higher the temperature as well as the pore pressure is.The effect of shear rate on the shear strength is bidirectional.The simulation results demonstrate that this model can effectively simulate the mechanism of friction-induced thermal pressurization of shear band soil during ring shear process,and the shear strength softening in the process.The new numerical ring shear model established in this study is of great significance for studying the dynamic mechanism of high-speed catastrophic landslides.

Rigid-flexible coupling dynamic modeling and vibration control for flexible spacecraft based on its global analytical modes

In this study, we used global analytical modeswfny(GAMs) to develop a rigid-flexible dynamic modeling approach for spacecraft with large flexible appendages(SwLFA). This approach enables the convenient and precise calculation of the natural characteristics for designing an attitude control law for the spacecraft while simultaneously suppressing the active vibration of its flexible appendages. We simplify the flexible spacecraft as a rigid-flexible coupling hub-beam system with tip mass and derive the system's governing equations of motion based on Hamilton's principle. By solving the linearized form of those equations with their associated boundary conditions, we obtain the frequencies as well as the corresponding GAMs of flexible spacecraft,which we use to discretize the equations of motion. Using this approach, we performed numerical simulations to investigate the system's global modes and assess the performance of the controller based on the GAM model. The results reveal that the GAM model can be used to directly calculate the exact global modes of SwLFAs and that the controller based on the discrete GAM model can achieve a control-index for a SwLFA in a shorter time with less input energy than other methods.

柔性齿轮运动特性及其振动抑制性能的实验研究

在三缸发动机平衡轴齿轮传动系统的传动过程中,存在着较大的振动和噪声问题,为此,提出了一种附加阻尼环的齿轮传动系统刚柔耦合模型,对柔性齿轮结构的运动特性及其振动抑制性能进行了实验研究。首先,采用集中质量法,建立了考虑齿轮间隙和时变啮合刚度的附加阻尼环6自由度齿轮传动系统的弯曲-扭转模型,利用石川公式计算出了柔性齿轮的时变啮合刚度,对比了有无阻尼环的齿轮系统的振动响应;然后,搭建了专门的齿轮传动系统测试设备,测试了不同转速下钢齿轮和柔性齿轮的加速度和噪声峰值;最后,设计了激光位移试验台,对比分析了不同转速下齿轮的微抖动,对柔性齿轮的减振效果进行了测试,并验证了理论模型的正确性。研究结果表明:当转速为1000 r/min时,钢齿轮和柔性齿轮的最大加速度信号分别为35.58 m/s^(2)和20.37 m/s^(2);当齿轮转速为4000 r/min时,柔性齿轮的阻尼效果最佳,加速度峰值降低了45.23%,噪声峰值降低了39.06%;钢齿轮的微抖动幅值明显高于柔性齿轮,两者的变化趋势相似。柔性齿轮能有效抑制轮齿微抖动振幅曲线的不平滑、毛刺现象,从而增强了三缸发动机平衡轴系的稳定性。

光伏电站环网柜温湿度非线性耦合预测模型研究

大型太阳能光伏电站中的环网柜工作环境复杂多变,面对温差大、潮湿等恶劣环境,极易发生环网柜运行故障,影响太阳能光伏的安全稳定接入并网。环网柜温湿度具有明显的线性和非线性变化特征,基于环网柜内部温湿度实测数据,利用自回归移动平均(ARIMA)模型和径向基函数(RBF)模型对线性和非线性数据处理能力的优势,构建ARIMA-RBF权重组合温湿度预测模型,对某光伏电站实际环网柜内温湿度进行动态预测。预测结果表明:相较于单一模型,ARIMA-RBF权重组合模型的预测精度更高、稳定性更好;该组合模型通过适当的加权策略充分发挥了单一模型对数据不同特征的处理能力,能较好地评估环网柜内部温湿度状态,可为建立更具普适性的预测模型提供参考,并有助于减少环网柜因长期超温和潮湿环境下运行引起的故障。

高温动压涨圈密封结构参数多目标优化分析

针对航空发动机涨圈密封在高温工况下磨损严重的特性,提出一种动环端面开设螺旋槽的动压涨圈密封。综合考虑切口对主密封端面流动的相互影响,建立流固热耦合数值分析模型,分析动压涨圈密封的密封性能,采用响应面法对静环结构参数进行多目标优化分析,试验验证模型的准确性。研究结果表明:动压涨圈的密封性能主要受切口间隙影响,而减磨性能主要受轴向厚度和径向宽度影响;切口间隙的增大将导致密封性能和减磨性能的下降,但轴向厚度和径向宽度的增加可有效减弱切口间隙的不利影响。优化参数组合为切口间隙0.2 mm、轴向厚度13 mm、径向宽度6.5 mm,优化后泄漏率降低26.73%,密封性能、减磨性能得到明显提升。

柔性齿圈行星轮系耦合模型创建及振动特性研究

针对柔性齿圈结构振动特性分析缺失以及现有传动系统特性分析方法不足,本文结合模态叠加法、承载接触分析技术与集中质量法,构建了考虑轮齿间接触特性、结构振动与系统振动的行星轮系模型。分析了柔性齿圈行星传动系统的结构振动特性及柔性齿圈对系统动态性能的影响,并避免了集中质量模型无法计入构件结构振动,全有限元模型计算量过大、收敛困难,现有刚柔耦合模型的刚性接触、齿轮参数标准化以及难以引入构件误差等问题。本文为柔性齿圈的设计以及传动系统动态特性的深入探究提供了模型基础和理论指导。

埋地管道的横向静力分析耦合模型及其解耦条件

现有埋地管道横向静力分析中的刚性管假设可以实现横向分析与纵向分析的解耦,但往往与实际情况不符。为此,本文根据埋地管道的受力特点,建立了考虑纵向内力影响的横向静力分析耦合模型。基于此耦合模型,结合挠曲线方程与纵向内力的关系,推导出横向分析和纵向分析的解耦条件,为建立解耦模型提供了理论基础。与此同时,一方面为便于实用,另一方面为检验解耦模型的误差,文中针对圆环形管道导出了其横截面剪应力分布规律,给出了埋地管道横向静力分析的实用耦合模型,并结合弹性中心法,建议和提出了耦合模型的实现算法。最后,采用耦合模型对两端固定的埋地给水管道进行了横向内力分析及解耦模型的误差探讨。结果表明,管道两端处纵向剪力对横向内力影响显著,解耦模型误差很大;但随着与管端距离的增加纵向剪力的影响急剧减小,近跨中区域解耦误差几乎可忽略不计。

硅基微环光学调制器动态特性模拟与分析

建立了硅基微环光学调制器特性模型,利用一种动态分析方法对器件的调制特性进行了模拟与分析。该动态分析方法将动态过程(时域)离散化,具有易于计算机编程的特点。利用该方法研究了环内相位调制与耦合调制方式下器件的光谱特性及调制带宽,对其调制机理进行了解释与分析,并重点对两种调制方式的啁啾特性、调制效率、调制深度,以及调制带宽等性能进行了详尽的分析对比。研究对于高性能硅基微环光学调制器的实现及应用具有一定的理论指导意义。

基于刚柔耦合环模型轮胎均匀性建模与分析

轮胎在生产制造过程中会不可避免地产生结构、材料、质量分布等不均匀问题。汽车即使在平稳路面上行驶,轮胎的不均匀性也会引起轴力的波动,并且轴力的高阶谐波还可能引发车辆内部的噪声问题。本研究基于刚柔耦合环模型,提出了一个用于分析轮胎几何不均匀导致的动态响应的理论模型。该模型考虑了径向尺寸偏差的影响,得到了不同垂向负荷下轮胎与路面接触压力分布和接地印痕长度,进而分析了轴头纵向力和径向力的波动,并利用试验数据进行了验证。结果表明,建立的模型可以很好地描述轮胎几何不均匀性对其受力的影响,并预测低速时径向尺寸偏差对径向力波动的影响。

活塞环-缸套动接触边界传热模型研究

由于润滑油膜内部存在多热效应耦合作用,现有内燃机流固耦合计算中常采用的活塞环-缸套间传热经验估计或热阻模型的计算结果与实际情况存在较大差异。为此本文中在线接触润滑模型的基础上,研究各热效应随工况的变化规律和相互间的耦合作用,建立了基于CFD流动传热计算结果修正的活塞环-缸套传热模型。结果表明,与热阻传热模型相比,本文中建立的修正传热模型算得的活塞温度场更符合实测的活塞温度数据;该模型经无量纲化处理后,可推广应用于其他活塞环-缸套传热计算。

中压环网结构的电缆屏蔽层传输特性的测试与分析

利用电力电缆屏蔽层进行载波信号传输,已成为国内外相关机构的研究热点。文章介绍了一个典型的由8段电力电缆通过线路开关连接成的环网结构,并对其供电电缆屏蔽层信道的传输特性(阻抗、噪声、传输特性)进行了全面的测试。测试结果和试验统计数据显示,采用高频桥接的多级电缆屏蔽层信道的传输特性基本满足载波组网通信可靠性要求,可以作为载波通信的信道,为城市小区配电自动化系统的通信系统提供了一种廉价且方便的解决方案。

构建基于信息技术的现代都市农业业务模式

本文介绍了现阶段先进的计算机信息技术,构建了"四环耦合"农业业务模式,该模式将计算机信息技术与现代都市农业深度融合,充分发挥了先进信息技术的优势,加速了现代都市农业的发展。

基于流固耦合的橡胶O形圈密封泄漏计算方法

提出一种基于流固耦合的橡胶O形圈静密封泄漏计算方法。对平行平板泄漏模型进行改进,使其适用于通道截面高度可变的泄漏率、介质压力计算;采用有限元仿真方法进行固体力学分析,求解宏观接触压力;采用Greenwood-Willamson模型进行接触力学分析,求解泄漏通道平均高度。基于数值方法研究介质压力、环境温度、表面形貌参数对橡胶O形圈密封性能的影响规律。结果表明,随着介质压力、环境温度、表面高度分布标准差的增大,体积泄漏率逐渐增大。上述数值方法以泄漏率作为表征密封性能的参数,能综合考虑橡胶材料、介质、工况等多种因素对O形圈密封性能的影响,对橡胶O形圈的寿命预测和失效分析更具指导意义。

基于半导体微环谐振器的光滤波器设计方法

提出了一种完整的基于微环谐振器的光学滤波器的系统设计方法。使用该方法可以从一定滤波特性参数出发,计算得到每个环之间的耦合系数,再根据耦合系数和器件尺寸的关系得到具体的器件尺寸,从而实现光学滤波器从性能特性到器件尺寸设计的一整套完整的解决方案。并在此基础上利用感应耦合等离子体(ICP)干法刻蚀技术和聚酰亚胺介质平坦化工艺制作了双环光滤波器,对该设计方法进行了初步的实验验证,使用扫描电子显微镜和原子力显微镜等多种测试方法证实,制作的光波导具有很好的性能,测试了其梳状滤波特性。

基于多场耦合建模与Bootstrap方法的滑环可靠性评估

导电滑环作为卫星太阳电池矩阵驱动机构的核心部件,其可靠性关系到卫星寿命的长短,由于空间用滑环寿命试验费用昂贵、试验周期长、样本数据量少等特点,无法获取大样本寿命数据,利用传统大样本数据进行统计推断,从而进行可靠性评估的方法存在困难。因此提出一种基于摩擦磨损模型的可靠性评估方法,应用赫兹理论、传热学方法分别计算摩擦副磨损过程中的接触区域变化和温度变化,量化热力电多场耦合对摩擦副磨损的影响,提出基于粘着磨损的多物理场耦合磨损模型,基于该模型得到的寿命数据,运用改进Bootstrap方法得到滑环寿命分布的参数估计,最后与传统可靠性预测方法结合,得到一系列滑环可靠性指标。方法对比结果表明,改进Bootstrap方法不仅具有较高的评估精度,还具有主观性小、适用性强的特点,由该方法所得的各可靠性指标均符合工程实际,具有很强的工程应用价值。