基于Wilson-θ算法的动载荷识别及影响因素

基于结构动力学正问题Wilson-θ算法的基本理论,推导了时域逆问题动载荷识别的改进算法,给出了算法的基本步骤和递推过程,同时将动载荷识别模型引入到模态空间,利用模态叠加实现多自由度系统的动载荷识别。仿真分析表明,该方法具有较高的识别精度和一定的抗噪声干扰能力,为动载荷时域识别方法提供了一种新的思路。     

基于结构动态响应的载荷识别研究

研究了基于系统动态响应来识别结构输入力的求解方法。分析实例悬臂梁结构的结构动力学方程以及物理数学方程,通过MATLAB仿真算例进行特征值求解,模态响应以及动态响应研究,对比有限元分析获得结构的响应结果;利用系统动态响应进行傅里叶变换和傅里叶逆变换得到输入力的时域形式,对获得的载荷结果进行识别算法分析,并且对比结构的输入力载荷。识别结果表明,这种方法对于正弦波输入力具有良好的识别效果,误差达到0.09%,能为二维结构,甚至三维结构载荷识别提供参考。     

轴承-转子系统模态参数时域识别的研究

轴承－转子系统模态参数时域识别对于回转机械的状态监测与故障诊断具有重要意义。然而，一般时域识别方法通常存在对系统定阶的困难，因此本文提出一种逐步扩阶的ＳＴＤ方法，并在双跨转子实验台上进行了模态参数识别实验，结果表明，该方法较好地解决了对系统定阶的困难，可以取得良好的识别结果     

机械结构模态参数时域识别方法原理及展望

分析了传统模态分析方法在大型机械结构模态识别中的弊端,指出利用基于响应信号的时域信号进行大型机械结构的模态参数识别已日益成为一种趋势。对时域模态参数识别的主要方法进行了论述,分析了各类方法的识别原理及优缺点,在此基础上总结了目前时域识别方法存在的问题,并对今后的研究工作进行了展望。     

基于状态变量的时域参数识别方法的某SUV白车身模态试验分析

状态变量模态参数识别方法作为一种时域参数识别方法,适用范围很广。通过建立白车身模态试验系统,将此方法应用到某SUV白车身模态试验分析中,得到白车身的模态参数,并与频域的P-P法和时域的ITD方法识别的结果比较,固有频率最大偏差均在0.5%以内。试验表明,此车身在低频域内多为组合振型,局部模态并不理想,但整体振型具有较好的低频动态特性。试验结果分析对此SUV白车身后期的性能改进具有重要的指导意义。     

一种多自由度振动系统动载荷识别的时域方法

为了解决复杂机械结构输入载荷难以直接测量的问题,基于结构动力学理论,应用Duhamel积分,推导了一种单自由度振动系统动载荷时域识别方法;在此基础上,通过模态坐标变换法,将多自由度振动系统运动方程解耦,以系统加速度响应作为输入,建立了一种多自由度振动系统动载荷识别的时域方法与模型。以一个多自由度的弹簧阻尼系统为对象,研究了载荷识别模型同时在正余弦组合激励、随机激励、三角脉冲激励等三种载荷形式下的稳定性和精确性。研究结果表明:在测量响应无噪声的情况下,载荷识别模型对三种激励的识别均具有很高的精度,识别结果与原始载荷相关系数达到0.99;在测量响应含有30%随机噪声的情况下,三种载荷的识别结果依然有很高的识别精度,相关系数均在0.97以上。     

时序分析在机床上的应用技术讲座 第五讲模态参数识别及其应用

采用模态分析技术识别机床结构模态参数是研究机床动态特性的一个很重要的手段。这种技术分时域识别法和频域识别法两类。采用ARMA模型进行识别属于前者(这是本讲伪内容);采用ARMA谱进行识别(常称为谱分析)属于后者(将在第六讲中介绍)。时域识别法中,可根据系统的随机响应信号进行识别,也可根据系统的自由响应信号进行识别,本讲将介绍这两种方法,并给出应用实例。 我们知道,一个p自由度的振动系统对应于一个2p阶的微分方程,系统的模态参数有:模态固有频率。。;、模态阻尼率5;、相角6;和振幅人,下标6表示第《阶模态的相应参数,《一互,2,…     

基于环境激励的结构模态参数识别方法

利用时域分析最小二乘复指数法(kast-Squares Complex Exponential,LSCE)推导出在脉冲响应下结构的模态参数,并利用ITD(Ibrahim Time Domain)法对随机振动响应的参数进行识别,为分析工作模态下结构的优化设计、损伤诊断和故障诊断打下基础.在充分研究了环境载荷对工程结构影响的基础上,重点分析了风载荷对大跨度工程结构的影响.利用有限元软件对空间桁架结构进行有限元工作模态分析,得出在环境载荷激励下的结构响应,进而利用参数识别方法得出模态参数,其结果与工程实际相符,证明了环境载荷处理的可行性和该理论体系的正确性.     

时域内动态载荷识别的径向基形函数法

为了减小载荷识别过程中的不适定性,稳定地实现动态载荷的时域重构,提出了基于径向基形函数的时域动态载荷识别方法。在离散化系统动力响应卷积关系式的基础上,将载荷在时间域内划分单元,采用径向基函数构造载荷形函数,并在整个时间域内进行组装,得到整体形函数响应矩阵,建立载荷识别的正向模型;在此基础上,利用正则化方法实现动态载荷识别。算例表明,该方法能够有效减小核矩阵的规模,改善核矩阵的病态性,在采样时间步长较大且响应存在测量噪声的情况下,可保证动态载荷反演的稳定性和精确性。     

载荷识别的逆系统方法

给出一个支载荷识别的时域方法，该法将控制中的逆系统理论用于载荷识别，将载荷识别这种逆问题转变成正问题来处理，得到离散系统和连续系统荷识别的计算模式，文中方法可以识别载荷的时间历程、载荷的作用位置，载荷的分布规律，通过仿真和实验，验证了方法的有效性。     

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.     

Limits of topographic measurement by the scanning tunnelling and atomic force microscopes

Parameters describing the topographic character of a surface (height, surface wavelength, slope and curvature) can be derived from equivalent sinusoidal profiles. The response of a surface-measuring instrument may be modelled in terms of instrument parameters such as stylus radius, and scanning range and resolution. The performance of the instrument may then be mapped as a zone in amplitude-wavelength (AW) space to show the sinusoidal profiles it is capable of measuring. In a first-order analysis the STM and AFM are considered as equivalent to contact-stylus instruments with a notional stylus radius equal to the tip radius plus the gap. Comparisons between different instruments and types of instrument are readily made by mapping in AW space. The error arising from convolution of the sinusoidal profile with that of the finite tip may be quantified and plotted as contours in AW space.