管翅式机油冷却器温度场模拟仿真与数值计算

利用SolidWorks对管翅式机油冷却器建模,使用ANSYSCFX仿真软件对管翅式机油冷却器的温度场进行模拟仿真,结合试验结果分析并讨论了风速和温差对管翅式机油冷却器传热的影响.试验结果与计算结果表明:空气侧温度和油侧温度差值与散热功率呈线性关系,差值越大管翅式机油冷却器的散热效果越明显;迎风面垂直方向风速与散热功率也呈线性关系,风速越大管翅式机油冷却器的散热效果越明显.利用MATLAB对已有的进风口风速、进油口温差以及对应的散热功率进行曲线拟合,得到进风口风速和进油口温差变化与散热功率的关系式.通过试验结果与计算仿真的数值模拟对比,验证了计算模型的有效性与准确性.     

超声式蒸发器强化传热性能分析

从改变进料温度、改变进料流量、改变进料温度与蒸汽温度的温差、改变超声功率的大小这4个方面分别对超声蒸发装置的传热性能进行了研究,实验采用单因子评价法进行分析。实验结果表明:进料温度越大、进料流量越大、超声功率越大,则传热系数K越大,蒸发传热性能越强;进料温度与蒸汽温度的差值越大,则传热系数K呈现减小趋势,即蒸发传热性能呈现减弱的趋势;在改变进料温度、改变进料流量以及改变进料温度与蒸汽温度的温差等情况下,增加超声均比不加超声对蒸发性能具有不同程度的强化效果;随着加入超声功率的增大,蒸发强化效果明显增强,但是当超声功率达到某一值时,强化效果略有减弱。     

翅片热板散热器的传热数值模拟研究

采用有限元法,应用ANSYS软件的热分析功能对翅片热板散热器的传热性能进行了数值模拟,并计算出该散热器表面的瞬态温度变化曲线,与实验测试结果吻合得较好.最后的研究结果表明:所研制的新型功率电子元器件翅片热板散热器散热性能良好,具有良好的启动性能和等温性能.     

热管换热器用于LED冷却系统的试验研究

研发了一种将大功率发光二极管(LED)散热和热管传热相结合的用于大功率LED冷却的热管散热器,并对设计出的热管散热器的传热性能进行了试验研究。结果表明,该热管散热器具有良好的散热能力,在输入功率为50W的情况下能控制节点温度在70℃以下,而且热管换热器的散热能力和工作倾角有密切关系,倾角越小,散热能力越好,垂直使用时散热能力最差,最后从理论上加以分析。     

收腰管散热器的耦合传热与试验

提出了一种收腰型散热管,在研究其对散热性能的影响的基础上,建立了收腰管型百叶窗散热器的三维模型,应用耦合传热原理对其传热过程进行模拟研究。得到不同风速下散热器的进出口压降、翅片传热系数和传热量,总结了收腰管对百叶窗散热器空气流道的流体结构及其分布规律的影响。通过风洞试验对比分析了多种管型散热器的性能差异,发现收腰管散热器具有更优的散热性能,能够满足多种车型发动机冷却系统的散热需求。     

电机控制器IGBT模块水冷散热设计

以电机控制器中IGBT模块水冷散热回路为研究对象,根据传热机理对其进行了传热与流阻分析;并利用有限元仿真模拟软件对水冷散回路的散热性能进行仿真模拟,研究不同翅片尺寸、翅片数量、冷却水流量参数对IGBT散热结温与冷却水压降的影响规律,获得了水冷散热的最优设计参数。结果表明:当冷却水流量为16 L/min、翅片数量为108、翅片尺寸为23 mm×6 mm时,水冷散热系统具有更好的散热效果。     

板翅式冷却器结构参数优化与仿真

为了提高机油冷却器的散热效率从而降低机油温度以保证发动机润滑系统的可靠性,以波纹板式散热器为研究对象,采用遗传算法对波纹板的结构参数进行了目标优化,采用计算流体动力学的方法模拟了散热器内部的流场和温度场的分布情况,并对优化结果的有效性进行了模拟验证。仿真结果表明:波纹板的节距、高度、倾角对流体的流动和换热具有重要的影响;当波纹节距为13.7mm、波纹高度为5.2mm、波纹倾角为49.5°时散热器的工作性能最佳,并且随着雷诺数的增加,TPF的值先增大后减小。通过试验测试验证了遗传优化算法和CFD仿真结果的准确性,研究方法对波纹板式散热器的优化设计具有实际的意义。     

翅片厚度对散热器散热性能影响分析

本文采用Fluent软件,在不同的空气工况下,对三组不同的散热器翅片厚度进行模拟仿真计算,得到不同厚度下翅片的温度及换热系数。研究发现,在相同的空气工况下,翅片厚度等于0.16mm时,翅片换热系数最大,传热最好,综合性能最优。这为散热带翅片的优化提供相应的参考。     

大功率密闭机柜热管散热器的试验研究

针对大功率密闭机柜散热困难,研制了R22为传热介质的微通道铝扁管型分离式热管散热器,并搭建试验装置对其散热性能进行试验研究。试验结果表明:加热功率为2k W、环境温度为50℃时,密闭机柜内部温度≤70℃,满足机柜散热要求;工作温度范围内,散热器散热功率与内、外循环进风温差有关;外循环进风风速提高,散热器换热系数非线性增加;内循环进风风速提高,散热器换热系数线性增加。研究结果为热管技术在机柜散热方面的设计提供依据。     

一种新型热翅板式电子散热器的模拟研究

由于现代电子设备及元器件不断向高集成度、高紧凑性发展,其散热量也不断增大,威胁到其正常工作的安全性和可靠性.为此,一种新型的热翅板式散热器结构被提出,并针对高散热量的电子元件(CPU芯片)进行了散热能力的研究.通过数值模拟分析了该新型散热器的散热性能,得到不同热功率下芯片的温度分布,分析了冷却温度、冷却风量等对散热性能的影响,最终得到了正常工况下的最佳风量.     

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.