弹塑性随机振动系统中恢复力数学模型的若干形式

本文基于弹塑性随机振动系统恢复力数学模型的统一形式，提出了能考虑刚度下降段和系统在滞变过程中强度退化的四种恢复力数学模型，为适应系统在多次强随机干扰下的反应分析需要，根据试验结果，提出了经受过强随机干扰的有损伤系统的恢复力模型，并建立了相应的数学表达式，最后针对钢筋砼框架结构在主余震作用下的弹塑性地震反应分析给出了具体算例。     

反扰力振动控制理论及其在井塔消振中的应用

应用反扰力振动控制方法，通过施加一个与原扰力在相位上相反的控制力，来抵消原扰力对结构的影响。此法用于实际的矿井井塔建筑结构消振工程，取得了消振９０％以上的显著效果，从而证实了此法的正确性和有效性。此法在动力荷载扰力作用下的建筑结构振动控制工程中，具有重要的应用价值     

基于Liapunov理论的结构非线性振动的混合控制

研究了地震激励下高层建筑进入塑性阶段后，结构非线性振动的混合控制问题。高层建筑简化为剪力墙形式，具有非线性滞变恢复力。采用被动基础隔振和主动控制力相结合的策略，对结构的非线性振动进行混合控制。基于Liapunov第二法，从系统的能量角度出发进行稳定性分析，找到控制系统的Liapunov函数，本着工程抗震设计中安全与经济的原则，应用允许结构反应进入非线性或塑性阶段的理论，判定所提出的混合控制方法具有Liapunov意义下的稳定。     

振动挤出过程中毛细管内聚合物熔体的剪切速率分析

借助自行研制的恒速型毛细管动态流变实验研究装置,对平行叠加振动条件下聚合物熔体经毛细管的挤出过程进行了分析;不依赖现有的任何本构关系,在考虑惯性项影响的前提下,建立了振动力场下毛细管壁处聚合物熔体剪切速率的计算公式;实验测量一定振动频率和振幅下毛细管瞬时入口压力、瞬时体积流量以及体积流量与入口压力波形的相位差,通过上述公式即可求得聚合物熔体在毛细管壁处的剪切速率。     

偏心激励作用柔性主被动隔振系统功率流特性

针对柔性基础上偏心激励作用复杂机械系统，建立了机器-柔性板基础主被动隔振系统数学模型，推导了系统动态特性传递方程。以传递到基础的功率流为评价指标，探讨不同激励及主动控制策略对主被动混合隔振效果的影响。     

模糊—神经网络控制算法及其在离心力—振动复合环境试验系统中的应用

针对离心－振动复合环境试验系统所存在的耦合性、非线性和不确定性提出了一种模糊－神经网络控制算法,利用被控对象输入输出信息离线、在线相结合学习系统的动态特性,对时变、非线性系统进行跟踪控制,并研究了该算法在系统中的实现方法。实现表明了控制系统具有良好的跟踪能力。该算法也适用于快速变化这类系统的实时控制。     

惯容器对隔振系统动态性能影响研究

本文设计了一种滚珠丝杠惯容器及ISD隔振系统,通过实验研究了惯性轮的转动惯量对惯容值的影响;同时,分析了滚珠丝杠惯容器的机械动力学特性,推导了ISD隔振系统的振动传递率计算公式,探讨了惯容器对ISD隔振系统动态特性的影响。在电机被动、主动和混合隔振工况下,开展了弹簧阻尼系统和ISD隔振系统的振动性能对比实验,验证了惯容器对振动系统固有频率和减振效果的影响规律。研究结果表明,惯容器可降低振动系统的固有频率,使共振频率向低频移动,共振振幅降低;在共振频率附近,惯容器可抑制共振振幅,惯容值越高,抑制效果越明显;ISD隔振系统在低频的减振效果优于传统的弹簧阻尼系统;随着频率比的增加,ISD隔振系统的传递率趋于稳定值,惯容器会引起高频隔振性能降低。     

考虑径向惯性力时圆柱的非线性强迫振动

研究了考虑径向惯性力时弹性圆薄板大挠度非线性强迫振动问题，提出了一个类似修正迭代法的求解方法，并以固支圆板为例作了具体的求解     

Application of a Dynamic Vibration Absorber to a Piecewise Linear Beam System

This paper deals with the application of a linear dynamic vibration absorber (DVA) to a piecewise linear beam system to suppress its first harmonic resonance. Both the undamped and the damped DVAs are considered. Results of experiments and simulations are presented and show good resemblance. It appears that the undamped DVA is able to suppress the harmonic resonance, while simultaneously many subharmonics appear. The damped DVA suppresses the first harmonic resonance as well as its super- and subharmonics.     

Dynamics of a Rigid Unbalanced Rotor with Nonlinear Elastic Restoring Forces. Part II: Experimental Analysis

In Part I, theoretical analysis of the dynamic behaviour of a rigid rotor with nonlinear elastic restoring forces was carried out. In this part (Part II), an experimental confirmation of the theoretical data from that analysis was sought. With this aim, an experimental model was set up consisting mainly of a practically rigid rotor clamped onto a small diameter piano wire symmetrical to the wire supports. These supports were rigid and equipped with roller bearings and a device that made it possible to adjust the initial tension in the wire so as to make the elastic restoring forces less or more linear. The rotor was dynamically unbalanced and was driven by an asynchronous motor regulated by means of an inverter in order to adjust the rotor speed. A series of tests was performed on this rig with different values of the initial tension in the wire, and the trajectories of two points on the rotor axis were recorded in the course of the tests. These trajectories were obtained, under the hypothesis of similarity, from the orbits covered by two given sections of the wire and detected with two pairs of capacitive transducers. The collected data was compared with the theoretical results from Part I of the present investigation. Comparison of the collected data with the corresponding theoretical results made it possible to infer that system nonlinearity in the presence of small damping can give rise to motions that are periodic, whether synchronous or not, or quasi-periodic, but never chaotic.     

Dynamics of a Rigid Unbalanced Rotor with Nonlinear Elastic Restoring Forces. Part I: Theoretical Analysis

In a previous paper, the dynamic behaviour of a Jeffcott rotor was studied in the presence of pure static unbalance and nonlinear elastic restoring forces. The present paper extends the analysis to a rigid rotor with an axial length such as to make the transverse moment of inertia greater than the axial one. As in the previous investigation, the elastic restoring forces are assumed to be nonlinear and the effects of couple unbalance are also included but, unlike the Jeffcott rotor, the system exhibits six degrees-of-freedom. The Lagrangian coordinates were fixed so as to coincide with the three coordinates of the centre of mass of the rotor and the three angular coordinates needed in order to express the rotor's rotations with respect to a reference frame having its origin in the centre of mass. The precession motions of such a rotor turn out to be cylindrical at low angular speeds and exhibit a conical aspect when operating at higher speeds. The motion equations of the rotor were written with reference to a system that was subsequently adopted for the experimental analysis. The particular feature of this system was the use of a steel wire (piano wire) for the rotor shaft, suitably constrained and with the possibility of regulating the tension of the wire itself, in order to increase or reduce the nonlinear character of the system. The numerical analysis performed with integration of the motion equations made it possible to point out that chaotic solutions were manifested only when the tension in the wire was given the lowest values – i.e. when the system was strongly nonlinear – in the presence of considerable damping and rotor unbalance values that were so high as to lose any practical significance. Under conditions commonly shared by analogous real systems characterised by poor damping, where the contribution to nonlinearity is almost entirely due to elastic restoring forces, the analysis pointed out that precession motions may be manifested with a periodic character, whether synchronous or not, or a quasi-periodic character, but in no case is the solution chaotic.     

杆件在横向力和轴向压力共同作用下的内力计算

针对杆件在横向力和轴向压力共同作用下的内力计算问题进行了研究．在考虑杆件变形因素的情形下,推导出了杆件在横向力和轴向压力共同作用下的内力和正应力的计算公式,并与材料力学中未考虑杆件变形因素的对应公式进行了比较,说明了二者之间不同之处．     

Application of Symmetries to Central Force Problems

We determine the Noether point symmetries associated with theusual Lagrangian of the differential equation of the orbit of the twobody problem. This gives rise to three definite natural forms (apartfrom the linear form) when the Lagrangian admits three Noether pointsymmetries which enables the solution of the orbit equation in terms ofelementary functions. The other forms for which the orbit equation hastwo point symmetries that arise in the Lie classification do not occurfor the usual Lagrangian. For central force problems we obtain inaddition to the six general central forces found by Broucke [8], newforce laws which lead to integrability in terms of known functions. Thisis achieved by the two Noether cases and further cases by use ofequivalence transformations of the orbit differential equation.Moreover, we give an extension of what is sometimes referred to asNewton's theorem of revolving orbits. We also make use of the Lieclassification to provide two new cases of integrable (in terms of knownfunctions) orbit differential equations and new force laws.     

内模控制及其在机构振动主动控制中的应用

振动主动控制通常采用最优控制,文中根据柔性机构的特点,采用内模控制策略。内模控制主要适合于具有周期性扰动信号的调节问题和具有周期性参考信号的跟踪问题,它的优点是对控对象参数具有鲁棒性,克服了最优控制需要精确掌握被控对象参数的缺点,文中首先介绍了内模控制的基本原理,然后给出了数值仿真结果,最后将算法应用柔性四连杆机构振动主动控制试验中,试验结果证明了方案的可行性。     

LT50m缩比模型悬索舱体系统的风振分析

在新一代大型射电望远镜（LT）的悬索舱体系统中增加了抑制风激振动的下拉结构控制索系，并分析了50m缩比模型的风振响应。首先，由非线性静力分析确定结构初始静态参考位形和初应力；其次，针对结构特点模拟作用在悬索和馈源舱上的随机风荷。在上述研究的基础上，在时域中模拟分析下拉索系对结构风振的抑制效果，同时通过典型节点时域响应的FFT变换，给出响应自功率谱图，进一步描述了振动控制的效果。     

蜂窝锥壳卫星适配器约束阻尼层振动抑制分析

主要研究在蜂窝锥壳卫星适配器上附加约束阻尼来抑制锥壳传递振动。尽管约束阻尼方面的研究很多，但是大多数都是针对简单的梁或者板结构，而对复杂蜂窝锥壳结构的振动抑制问题研究还很少；为此，通过对蜂窝壳的等效化处理和约束阻尼结构的有限元建模理论分析，建立起卫星一适配器结构在有无附加约束阻尼情况下的有限元模型，进一步通过模态分析和频响分析，得到不同约束阻尼层设计参数对结构振动抑制影响规律。分析结果对于经济有效的设计约束阻尼层和结构减振减重具有较好的参考价值。     

基于真空吸盘的新型振动加载技术研究及应用

传统的振动加载技术,试件通过刚性夹具与振动台台面进行连接,刚性夹具采用螺栓与振动台台面和试件进行连接。一些试验要求振动加载装置的连接不能破坏试件结构,传统的螺栓方式不能满足要求。本文研究了一种基于真空吸盘的新型振动加载技术,振动加载杆通过真空吸盘吸附在试件表面。该项技术已在垂尾结构的动态疲劳试验中得到应用。应用实践证明,这种基于真空吸盘的振动加载技术方便、可靠、安全,弥补了传统加载方式的不足。     

Stability of Gravity Driven Convection in a Cylindrical Porous Layer Subjected to Vibration

The linear stability theory is used to investigate analytically the effects of gravity modulation on convection in a homogeneous cylindrical porous layer heated from below. The linear stability results show that increasing the frequency of vibration stabilizes the convection. In addition the aspect ratio of the porous cylinder is shown to influence the stability of convection for all frequencies analysed. It was also observed that only synchronous solutions are possible in cylindrical porous layers, with no transition to subharmonic solutions as was the case in Govender (2005a) [Transport Porous Media 59(2), 227–238] for rectangular layers or cavities.