阻尼层对自由阻尼处理结构的影响

在表面阻尼处理结构中,介绍了描述普通的阻尼层材料的贮能模量以及损耗因子随温度变化的规律,建立了自由阻尼处理梁的结构损耗因子的计算公式.通过数值计算揭示了自由阻尼处理梁的耗散特性.通过改变温度、阻尼层厚度、敷设纤维材料等不同的方法达到改变损耗因子的目的,给出了在不同条件下通过数值计算得出的结论,并比较这几种不同的方法对损耗因子的改变有何不同.     

形状记忆合金在结构阻尼性能优化中的应用

文中研究了通过嵌入NiTi-SMA丝提高自由阻尼层结构损耗性能的方法。首先描述了普通阻尼层材料的贮能模量及损耗因子随温度变化规律。基于一维SMA的Brinson模型给出了NiTi-SMA丝受限回复应力的计算公式,建立了含NiTi-SMA丝的自由阻尼处理梁结构损耗因子的计算公式。通过数值计算揭示了含NiTi-SMA丝的聚氨脂自由阻尼处理梁的耗散特性,分析了NiTi-SMA丝含量及阻尼层厚度对自由阻尼处理梁耗散特性的影响。结果表明,埋入NiTi-SMA丝之后,阻尼结构的损耗因子得到了显著提高。     

自由阻尼结构损耗参数的换算方法

在自由阻尼结构理论的基础上,建立了不同自由阻尼结构之间的结构损耗因子换算关系。针对自由阻尼板、壳结构开展了阻尼测试,换算结果与测试结果一致性良好,验证了换算方法的有效性。同时开展了换算系数和误差放大因子的仿真分析。仿真结果表明:对于弹性模量较高的阻尼层,换算系数随厚度比变化较小,换算精度较高;对于弹性模量较低的阻尼层,换算系数随厚度比变化较大,换算精度较低。建议阻尼层比目标基材层厚,且换算基材厚度小于目标基材厚度的2倍。该换算方法可用于预估一些难以测量的自由阻尼结构损耗参数,为大型简单圆柱壳结构敷阻尼层后损耗参数的获得以及多种阻尼层在大型圆柱壳结构上抑振性能的评比提供参考方案。     

敷设阻尼薄板隔声性能的测试与计算分析

首先,采用脉冲响应衰减法测试了敷设阻尼薄板的阻尼损耗因子,分析了阻尼敷设比例及薄板的悬挂状态对薄板阻尼损耗因子的影响;其次,在混响-全消室中测试了敷设阻尼薄板的隔声量,比较了不同阻尼敷设比例薄板的测试结果;最后,建立了敷设阻尼薄板隔声量计算分析模型,隔声量计算值与试验值吻合较好,验证了计算模型的有效性。研究了敷设阻尼材料厚度与敷设比例对薄板结构隔声性能的影响,综合考虑轻量化和隔声性能,分析了阻尼材料厚度与敷设比例对薄板降噪效率的影响,并以降噪效率最大为目标进行了薄板隔声特性的优化。     

阻尼合金减振元件厚度与减振效果研究

通过对减振件厚度与结构耗因子及减振效果的理论分析与试验研究，找到了它们之间的相互关系。阻尼合金减振元件的厚度与结构损耗因子有密切关系。因此，减振元件厚度增减将直接影响振效果。     

夹层阻尼结构抑振特性研究

利用等效复合刚度法,对多夹层阻尼结构的抑振特性进行了理论推导,并对不同夹层阻尼结构的等效复合刚度和损耗因子进行了仿真计算,分析了不同的夹层材料和几何参数对结构抑振量的影响。研究表明,增加多夹层组合结构的夹层层数对组合结构损耗因子的提高量有限;适当增加夹层的厚度可改善组合结构抑振性能;变化夹层的材料,采用较硬的约束层和较软的阻尼层可显著提高组合结构的抑振量。     

运用有限元分析的阻尼板优化设计

根据阻尼板各阶损耗因子与各材料应变能之间的关系,利用有限元软件AN SY S对5层阻尼圆板的前4阶损耗因子进行了有限元分析计算,并选取它们的倒数和为目标函数,再次应用AN SY S软件中的优化模块对阻尼圆板的各层厚度进行了优化设计。通过对一块5层阻尼板的优化仿真,使得阻尼板前4阶的阻尼损耗因子较优化前有较大幅度的提高,使其在工作环境中具有更好的减振性能。     

热氧老化对阻尼橡胶材料阻尼性能的影响

通过对ZN-1阻尼橡胶材料进行加速热氧老化试验,考察了其在老化前后阻尼性能的变化;利用Arrhenius方程推导出了该材料的阻尼性能与老化时间、老化温度的关系。结果表明:随着老化温度的升高及老化时间的延长,ZN-1阻尼橡胶材料的最大损耗因子逐渐减小,并得到了25℃时热氧老化后最大损耗因子与老化时间的关系式,可用于阻尼橡胶材料老化后阻尼性能及使用寿命的预测。     

颗粒阻尼器损耗因子外因特性研究

对稳态能量流法测量阻尼损耗因子的原理进行了推导,采用稳态能量流法对某型颗粒阻尼器的阻尼损耗因子进行了实验研究。对粘贴有该颗粒阻尼器的钢板进行了振动仿真分析与实验相结合的研究,验证了稳态能量流法测量损耗因子方法的正确性。实验结果表明,该颗粒阻尼器的阻尼损耗因子随加速度变化呈现明显的“分段表征”特性,随频率变化呈现明显的“山脊”特性。对颗粒阻尼器表现出该特性的原因进行了理论分析。     

基于ESO的约束阻尼板拓扑优化设计研究

基于渐进结构拓扑优化方法（Evolution Structural Optimization，ESO），以阻尼材料用量为约束条件、模态损耗因子最大化为目标函数，研究了约束阻尼板结构的拓扑优化设计问题，推导了灵敏度分析公式，给出了阻尼结构拓扑优化设计方法，得到了在一定阻尼材料用量下约束阻尼板结构的模态损耗因子最大的拓扑构形。该方法对于阻尼结构的优化设计有一定的意义，具有较强的工程实用性。     

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.     

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.