电磁悬浮式微驱动器的有限元分析研究

设计了一种新型的多点峰值磁场相互作用的电磁悬浮式微驱动器,解决了悬浮驱动力与横向力相互耦合的问题,有利于调节悬浮体的运动姿态.通过对悬浮力关于输入电流、气隙高度做单一因素参数化有限元分析和联合参数化有限元分析,得到了微驱动器有限元特征参数关系曲线.通过实验测试,得到的实验特征参数关系曲线与理论特征参数关系曲线和有限元特征参数关系曲线吻合一致,表明了所设计的微驱动器的可行性.     

非接触式电磁驱动器的驱动力解析及动力学仿真分析

电磁驱动是通过改变输入电流及各电磁铁与导磁体的气隙大小控制磁力,进而实现非接触式电磁驱动的技术.采用永磁支撑电磁驱动方式构建一种电磁驱动器,以电磁驱动力的数学模型为基础,建立非接触式电磁驱动器的动力学模型,并对电磁驱动器的响应特性进行数字仿真研究.结果表明,该电磁驱动器具有很好的动态特性.     

U形箝位机构对微驱动器运动精度的影响研究

讨论利用尺蠖运动机理实现大行程线性运动的微型驱动器,特别就其U形箝位机构对驱动器运动精度的影响进行探讨.分析结果表明,电磁箝位脚与行走台面间磁路气隙的大小将影响箝位力和箝位剩磁力的大小;箝位脚因箝位剩磁力和重力引起的摩擦力而发生挠变形,此箝位脚的刚度将影响微驱动器行走步长或导致回窜;箝位力不足或箝位剩磁力过大时可致二维驱动器的直线运动发生偏转.文中研究的驱动器,电磁箝位脚与行走台面间的磁路气隙应不小于5 μm,以20 μm ～40 μm为最佳;驱动器伸缩部分的最小伸缩量ΔL应大于0.52 μm,驱动器才能有累加位移;二维驱动器的空载直线运动的最小箝位电磁力应大于27.8 N.     

磁悬浮球形主动关节机理与控制策略研究

提出一种新型多自由度磁悬浮球形主动关节,对关节产生磁悬浮力和电磁转矩的机理进行了研究,从关节定子和转子之间的气隙磁能着手,即根据气隙磁能建立主动关节的机电能量转换关系,推导出了驱动关节旋转的电磁转矩和支撑关节的悬浮电磁力;分析了磁悬浮球形主动关节旋转与悬浮的控制关系,通过位移传感器检测转子的偏移信号,经过滤波、放大及悬浮控制器等环节的处理变换成电流信号,反馈到绕组控制输入端与输入的转矩电流进行叠加以改变定子绕组中电流的大小,从而实现了对球形主动关节旋转与悬浮的精确控制,并提出了对其的综合控制策略及控制原理。     

EMS磁悬浮列车悬浮特性研究

通过搭建单电磁铁悬浮模型对磁悬浮列车的悬浮特性进行了研究。从电流刚度、气隙刚度以及垂直方向合力(悬浮力)三个方面分析电流、悬浮间隙对悬浮特性的影响,为磁悬浮动力学建模提供理论基础。     

异极永磁偏置径向混合磁轴承及其性能分析

介绍了异极永磁偏置径向混合磁轴承的结构和工作原理,利用等效磁路法建立悬浮力计算模型,理论分析说明异极磁轴承比三极磁轴承最大承载能力提高了33.3％,通过有限元分析得出异极磁轴承能得到比三极磁轴承更好的悬浮力与电流线性关系.搭建试验台对理论分析和仿真结果进行验证,异极磁轴承悬浮力与电流线性关系更好,最大承载力提高了29....     

基于电流反馈的MSCMG轴向磁轴承低功耗控制

为了进一步降低MSCMG永磁偏置轴向磁轴承的悬浮功耗,在建立其数学模型的基础上,针对传统定气隙控制在承受负载时线圈电流增大的问题,提出了基于电流积分正反馈的轴向磁轴承变气隙控制方法。该方法利用永磁偏置混合磁轴承的位移负刚度提供悬浮力,通过电流反馈改变转子悬浮参考位置来减小磁轴承线圈电流。仿真分析和试验结果表明,该方法具有良好的稳定性,与定气隙控制方法相比,磁轴承静浮时的铜耗降低了90%以上。     

基于TR磁浮列车的混合悬浮反馈控制策略

为研究电磁永磁混合悬浮的反馈控制策略,基于TR08磁浮列车参数,建立了电磁永磁混合悬浮气隙控制系统数学模型,引入了状态反馈控制策略,分析比较了混合悬浮控制系统在斜坡及阶跃启动条件时的启动性能.研究了在悬浮气隙阶跃干扰及悬浮力正弦干扰条件下,混合悬浮控制系统的调节过程.研究结果表明:混合悬浮较之常规电磁悬浮方式,具有降低电磁极功耗,增加悬浮气隙调节范围的特点;电磁永磁混合悬浮气隙控制系统具有控制精度高、响应速度快及鲁棒性能较强等优点.     

基于定子磁场定向的无轴承异步电动机控制策略

集旋转与悬浮于一体的无轴承异步电动机是一个非常复杂的非线性系统,电磁转矩与径向悬浮力之间的非线性解耦是实现电动机稳定悬浮运行的基础.提出基于转矩绕组定子磁场定向控制策略,设计自适应磁通观测器观测定子磁通,径向悬浮控制所需的转矩绕组气隙磁通由观测的定子磁通和定子电流适时辨识.应用Matlab/Simulink对样机进行了仿真研究,计算机仿真表明,电磁转矩与径向悬浮力之间的完全解耦可以实现,验证了定子磁场定向控制策略的有效性.     

大支承力径向电磁轴承结构设计及试验研究

为实现电磁轴承在重载工况下更好的悬浮效果,对径向电磁轴承提出了大支承力的要求,要求在绕组中加载大电流时磁场分布保持均匀,以保证在不同气隙下电流与力的近似线性化。设计了E形径向电磁轴承结构,利用ANSYS Maxwell,以最大承载力为目标对磁场分布进行分析,并且通过变换轴承定子气隙参数,测试出电流变化而产生的不同电磁力,验证了径向电磁轴承支承性能。     

Quantum Cooperative Robotics and Autonomy

The intersection of Quantum Technologies and Robotics Autonomy is explored in the present paper.The two areas are brought together in establishing an interdisci...     

考虑进油孔有限长滑动轴承油膜力的近似解析解

针对具有进油孔的有限长滑动轴承油膜力求解问题,采用变分原理和分离变量法,求得了有限长滑动轴承油膜压力分布的近似解析表达式。将油膜压力分布的近似解析表达式在油膜存在区域上进行积分,即得到了油膜力。将提出的计算有限长滑动轴承油膜力方法与无限长轴承模型、有限元方法的计算结果进行了比较,发现了提出的方法与有限元方法的计算结果很接近。最后,研究了进油孔位置和进油压力对油膜存在区域、油膜力等的影响,研究结果表明进油孔位置和进油压力对油膜存在区域和油膜力有较大的影响。     

三绕组变压器的双绕组等效建模及在Matpower中的应用

针对实际电网存在着大量的三绕组变压器,但国际上一些著名商业软件,如BPA仿真软件、Matpower这一权威潮流计算开源软件,均只提供双绕组变压器模型,限制了其在具有三绕组变压器的电力系统中的应用的问题,潮流计算是自主开发的电力系统各种应用软件的核心模块,因此依托国际权威开源程序进行二次开发,是一种较好的选择。对Matpower要求的数据格式进行了归纳,对变压器的一般的等值电路及带理想变压器的等值电路和带标幺值的等值电路进行了分析研究,提出了三绕组变压器转换为双绕组等效模型的建模方法,使得原先只适应双绕组变压器的潮流计算软件可以适用于三绕组变压器电网的潮流计算;最后以Matpower软件为例进行了案例计算,并用PSASP仿真软件进行对比验证。研究结果证明,所提出的建模方法是有效的。     

On the Relation of Load to Average Gap in the Contact Between Surfaces with Longitudinal Roughness

A computer simulation model for the contact between longitudinally-oriented rough surfaces has been formulated. This model closely duplicates the actual surf ace contact deformation behavior by taking into account the elastic interactions between the asperities. There were no assumptions made about the shapes, or any deformation behavior of the asperities, except for their obeying the laws of elasticity. The plastic deformations on the high asperity peaks were taken into account by setting a ceiling on their contact pressures at the material hardness value. The simulations used real surface profiles which were digitized from unworn circumferentially ground steel surfaces. Each pair of these profiles was mathematically combined to form an equivalent rough profile pressing against an infinitely rigid flat and having the appropriately adjusted elastic modulus. A total of 28 different pairs of profiles were used in the simulations. Each contacting pair was subjected to 30 different load levels and the local contact pressures and deformations were calculated. The contact simulations yielded some important mathematical relationships between parameters, such as the real area of contact, average gap, and average asperity load through statistical curve fitting. Two analytical functions were generated to relate the average load to average gap and the real area of contact to load.     

电站锅炉模糊风险评价方法研究与应用

针对电站锅炉风险等级评价问题,将模糊综合评价技术应用到电站锅炉风险等级评价中。开展了电站锅炉失效影响因素及模糊评价因素的重要程度分析,建立了一套科学合理适于在线评价的电站锅炉风险评价体系,提出了模糊综合评价技术与改进的模糊层次分析法相结合的模糊风险评价方法,利用改进的模糊层次分析法计算了指标体系中各层指标权重。对某一台电站锅炉的实际运行工况影响子因素进行了模糊风险评价,采用模糊合成算子进行模糊综合运算得到电了站锅炉运行工况影响子因素的评价向量。研究结果表明:电站锅炉的运行工况影响子因素的风险评价等级为第6级,失效可能性等级为小,该电站锅炉运行工况良好。     

基于多目标非支配解提取法的电力系统无功优化

针对传统的电力系统多目标粒子群优化算法采用权重系数法将多目标转化为单目标,从而忽视了各目标函数间的竞争关系这一问题,提出将非支配解提取法运用到电力系统多目标无功优化中,并设定了一套提取规则,以电力系统中的有功网损、电压偏差和电压稳定裕度为目标,使目标在充分竞争的情况下得出Pareto最优解,利用IEEE-14节点系统对多目标非支配解提取法的电力系统无功优化进行了仿真测试。研究结果表明,该算法一次运行可以得出多组非支配解,既有偏向单个目标的解也有兼顾所有目标的解,克服了权重系数法的盲目性和单一性,可使电力决策者根据实际问题选择最优解,具有较好的灵活性与多样性。     

交通荷载作用下桥梁结构参数识别方法

应用动力节点加载法,将作用在桥梁上的交通荷载转化为等效节点荷载,再用两步构造法识别结构物理参数.第1步,用Newmark-β方法变换结构运动方程,并用结构的加速度响应求得变换空间内的位移、速度和加速度响应;第2步,基于最小二乘原理,构造出变换空间内求解结构参数的递推式,进行结构物理参数识别.数值模拟结果表明,在交通荷载作用下,该方法能够快速、准确地进行桥梁结构参数识别.     

RLS and LMS blind adaptive multi-user detection method and comparison in acoustic communication

RLS and LMS blind adaptive multi-user detection algorithm and multi-user detector was proposed to solve the problem of multi-user signal detection problem encountered in underwater acoustic communication networks.In simulation analysis,RLS and the LMS blind adaptive multi-user detector were designed and tested for synchronous and asynchronous multi-user communication process.The results of SIR comparison and MMSE comparison show that,both of the two methods can realize blind adaptive detection when any user change in multi-user communication,during this process,the training communication sequences are not needed.The RLS algorithm has about 5 dB higher in SIR compared with LMS algorithm,and the convergence velocity of RLS algorithm is also higher than LMS algorithm when the communication users change.RLS algorithm has better ability in multi-user detection than that of LMS algorithm,and it has great attraction and guiding significance for solving the problem of multiple access interference(MAI) in multi-user communication.     

Robust Impedance Control of Robots Using an Adaptive Interaction Force Observer

For robot interaction control,the interaction force between the robot and the manipulated object or environment should be monitored.Impedance control is a type ...     

Research on key techniques of expendable conductivity temperature depth measuring system

This paper analysis the developing of expendable conductivity temperature depth measuring system(XCTD)and introduce its principle of measuring about temperature,salinity and depth of ocean.Some key techniques are put forward.According to the real needs of XCTD,conductivity sensor with high sensitivity is designed by principle of electromagnetic induce,the ocean conductivity from induced electromotive force has been calculated.Adding temperature correction circuit would help to reduce error of conductivity measurement because of sharply changing temperature.Advanced temperature measuring circuit of high precision and the constant current source is used to weaken effect of self-heating of resistance and fluctuation of the source.On respect of remote data transmission,LVDS is a good choice for the purpose of guarantee the quality of data transmitted and the transmission distance is reaching to thousand meters in the seawater.Modular programming method is also brought into this research aimed at improve the stability,reliability and maintainability of the whole measuring system.In February,2015,the trials in South China Sea demonstrate that the developed XCTD realize effective measurement at a speed of 6 knots and detection depth at 800 m.The consistency coefficient of the acquired data is greater than 0.99 and the success rate of probe launching is above 90%.