混合刷式密封泄漏特性的数值研究

为分析某型号汽轮机改进的刷式密封结构的密封性能,采用non?Darcian多孔介质模型的Reynolds?averaged Navier?Stokes方程数值求解方法,对泄漏流动特性及转子表面、刷束自由高度和保护高度的压力、速度、湍流动能分布规律进行数值研究,并与迷宫密封进行相应的比较。结果表明：相同的间隙和压比下,混合刷式密封流场分布要比迷宫密封复杂,泄漏量明显小于迷宫密封;相同的结构和参数下,泄漏量随着压比的上升而增加;转子表面的轴向压力和湍流动能从进口到出口呈现阶梯状递减趋势,保护高度的径向压力基本趋于常数值;刷束径向速度和湍流动能随着压比的上升而增加,刷束下半部分和后挡板保护高度对泄漏特性影响比较大。研究结果为汽轮机刷式密封的结构设计,改善性能,提供了理论依据。     

明渠扩散段急流运动特性及调控方法研究综述

依据文献分析了有限宽度水槽突然扩散、固定扩散角渐变扩散、无边界平板扩散和急流扩散4种典型明渠扩散段水流的共同流动特征.给出了有限宽度水槽突然扩散段水流宽度的沿程发展规律,以及在平底明渠急流扩散段设计时,为防止水流脱离的扩散角计算方法和突然扩展区急流扩散的边界方程;通过不同底坡比降的试验和原型资料分析,论述了陡坡扩散区水深沿程变化特点、沿程各断面横向分布规律,介绍了陡坡上水平扩散角的计算方法与扩散角最大值的存在.通过大扩散角水槽试验,发现在扩散段不同流态的过渡水流现象及稳定性不一样.上游来流为急流时,下游水跃进入扩散段就是水流失稳、主流偏转的开始;采用潜没式三角翼可以防止扩散段回流发生,提高过流均衡性.     

液压消音器的内部流场信号传输特性

对液压管路中给定的压力阶跃信号进行数学分析,得出信号在管路中传输特性;为设计液压消音器提供了数学基础。     

计及输入变量强相关性的概率潮流计算模型

利用统计学的方法,以风电场出力为例,对其大量历史数据进行相关性分析,将具有强相关性的随机变量用最小二乘进行线性拟合,并用其中一个变量的线性表达式表示,从而消去随机变量之间的强相关性,并认为余下的呈弱相关或不相关的随机变量之间相互独立,以便采用半不变量法计算概率潮流。     

基于OPC技术的流量仪表在线补偿系统

为了提高传统流量仪表的测量准确性和抗干扰能力,本文设计了基于OPC技术的流量仪表在线补偿系统.采用OPC技术实现在线补偿算法单元与实时监测补偿系统的实时通讯,通过计算后的补偿值在实时监测补偿系统上显示,从而使流量测量更加准确,而且便于维护.     

大坝渗流监测系统中电源智能控制子系统的设计与实现

文登市米山水库大坝自动化监测系统由于现场设备一直处于24 h供电状态,使得现场设备故障频发。为了解决这一问题,采用了电源智能控制系统,通过485总线与上位机进行通讯,由上位机对电源系统进行控制,实现了对现场设备的定时、按需、智能供电。经过半年多的使用,取得了良好的效果。     

Numerical Simulation and Analysis of Migration Law of Gas Mixture Using Carbon Dioxide as Cushion Gas in Underground Gas Storage Reservoir

One of the major technical challenges in using carbon dioxide（ CO2） as part of the cushion gas of the underground gas storage reservoir（ UGSR） is the mixture of CO2and natural gas. To decrease the mixing extent and manage the migration of the mixed zone,an understanding of the mechanism of CO2and natural gas mixing and the diffusion of the mixed gas in aquifer is necessary. In this paper,a numerical model based on the three dimensional gas-water two-phase flow theory and gas diffusion theory is developed to understand this mechanism. This model is validated by the actual operational data in Dazhangtuo UGSR in Tianjin City,China.Using the validated model,the mixed characteristic of CO2and natural gas and the migration mechanism of the mixed zone in an underground porous reservoir is further studied. Particularly,the impacts of the following factors on the migration mechanism are studied： the ratio of CO2injection,the reservoir porosity and the initial operating pressure. Based on the results,the optimal CO2injection ratio and an optimal control strategy to manage the migration of the mixed zone are obtained. These results provide technical guides for using CO2as cushion gas for UGSR in real projects.     

多孔介质通道气液两相流型及压降特性研究

通过高速摄影仪研究多孔介质通道内气液两相流体垂直向上流动的流型,在实验参数范围内依次拍摄到泡状流、弹状流、脉冲流、雾状流4种典型流型,并总结了各种流型的特征。依据实验获得的两相流动阻力数据,分别对分相模型阻力关系式和均相模型阻力关系式进行了拟合,得到了适于实验特点的两类阻力关系式。改进后的两类模型均与实验数据实现了较好的吻合,但模型关系式定义中包含了影响阻力压降各要素的均相模型具有更高的预测精度,且该模型物理意义更加清楚,可以优先用于多孔介质通道气液两相流动的阻力计算。     

Modeling electric vehicle’s following behavior and numerical tests

The micro modeling for electric vehicle and its solution were investigated. A new car-following model for electric vehicle was proposed based on the existing car-following models. The impacts of the electric vehicle＇s charging electricity were studied from the numerical perspective. The numerical results show that the electric vehicle＇s charging electricity will destroy the stability of uniform flow and produce some prominent queues and these traffic phenomena are directly related to the initial headway, the distance between two adjacent charging stations and the number of charging stations. The above results can help traffic engineer to choose the position of charging station and the electric vehicle＇s driver to adjust his/her driving behavior in the traffic system with charging station.     

A novel contour design technique of super/hypersonic nozzle diverging section with sharing throat

A straightforward technique has been developed to quickly determine the wall contour of super/hypersonic nozzles working at multiply Mach number which share a common throat section.Mach number distribution along the centerline of the nozzle is specified in advance and divided into two sections,both of which are described by the b-spline function.The first section is shared by different exit Mach number nozzles.The nozzle contour is determined by the method of characteristics plus boundary layer correction.An example of this design method is employed to illustrate the technique with a computational fluid dynamics calculation.The simulation results indicate that desired Mach numbers are obtained at the nozzle exit,and the good flow quality is attained for different nozzles within δMa/Ma±0.56% in the flow core region.This technique improves the design precision of the converging-diverging nozzle,cancels waves completely,and achieves nozzles with multiple Mach number exiting which share a common throat section.