电磁轴承—转子系统的动态特性

本文提供了一个闭环控制电磁轴承-转子试验系统,在电磁力的控制作用下,重量为4公斤、直径为50毫米的转子完全悬浮于二个径向电磁轴承之中,转速可达3000转/分。本文还建立了此闭环控制系统的数学模型,通过数字仿真分析了其动态特性,探讨了控制器参数对转子运动的控制效果以及与电磁轴承动刚度之间的变化关系。     

弹性箔片动压径向气体轴承动特性的实验研究

建立了新型弹性箔片动压气体轴承性能测试实验台，在静载60N、转速9000r／min条件下进行轴承性能测试试验，通过中心插值法获得轴承中心的扰动速度和加速度，采用时域最小二乘法计算不同激振频率下的8个轴承动态线性刚度和阻尼系数，考察了激振频率对轴承动特性系数的影响．结果表明：轴颈中心扰动轨迹为椭圆形且振幅随动态激振频率增加而增大；刚度和阻尼系数的直接项随动态激振频率增加而减小；交叉刚度和阻尼相对激振频率的变化较小，且其值小于直接项；当激振频率与轴颈转动频率相同时，工频成分的影响较大，轴心扰动幅值明显增大，刚度和阻尼的直接项小于其它频率时的值．     

挤压油膜阻尼在储能飞轮转子支承系统中应用研究

在飞轮储能系统实验研究中,利用永磁轴承-螺旋槽流体动压锥轴承的混合支承,并采用了挤压油膜阻尼为转子支承系统提供阻尼。基于流体润滑理论的雷诺方程和长轴承近似理论,推导出一端封闭、一端开口边界的挤压油膜的压力分布近似解析解,得到等效油膜刚度和阻尼系数。最后对比分析了飞轮转子支承系统不平衡响应的计算与试验结果。     

求一般结构系统部分复模态的Ritz向量法及应用

构造了一种获取一般结构系统（刚度，阻尼矩阵可以是非对称的）Ｒｉｔｚ向量基的迭代方法，从而可以高维阻尼系统部分复模态解降价成为一个低维二次特征问题，将此降阶后的二次特征问题化成标准特征值后即可用ＱＲ方法求得系统的部分低阶持征解，作为应用，对一个实际转子－轴承系统的动力特性进行了计算分析。     

涡轮膨胀机止推轴承－转子系统的振动分析

为了确保涡轮膨胀机止推轴承在受到瞬时冲击时不致发生损坏事故，研究了止推轴承－转子系统的轴向瞬态过程，计算了止推轴承的线性油膜刚度系数和阻尼系数，并对线性和非线性两种情况下的轴向瞬态响应作了分析与比较，为止推轴承；转子系统的可靠性评估提供了科学依据。     

涡轮膨胀机止推轴承—转子系统的振动分析

为了确保涡轮膨胀机止推轴承在受到瞬时冲击时不致发生损坏事故，研究了止推轴承－转子系统的轴向瞬态过程，计算了止推轴承的线性油膜刚度系数和阻尼系数，并对线性和非线性两种情况下的轴向瞬态响应作了分析与比较，为止推轴承－转子系统的可靠性评估提供了科学依据。     

箔片-电磁混合轴承的稳态承载特性及控制

箔片-电磁混合轴承(HFMB)是一种将气体箔片轴承和电磁轴承混合使用的新型轴承,有效解决了气体箔片轴承低速磨损大和电磁轴承承载力有限的不足,并且具备载荷可分配和支撑系统动力学性能可调节等优点.文中在分析两种轴承稳态承载特性的基础上详细讨论了混合轴承的稳态控制方法,给出了一种以电磁轴承实际承载力与预分配承载力差值最小为控制目标,通过等边三角形为基本单元对混合轴承工作区域进行划分的箔片-电磁混合轴承稳态工作位置搜索算法.最后建立了系统模型并进行了数值仿真,验证了稳态控制系统的可行性和有效性.     

模糊控制理论在有源磁悬浮系统中的应用

建立了陀螺浮子磁悬浮数学模型,对该系统进行了MATLAB仿真并分析了该系统的刚度和阻尼特性。在此基础上,计算了满足刚度和阻尼特性的PID控制器参数,仿真结果表明,基于刚度和阻尼特性的PID控制器能够基本满足系统的要求,但响应时间过长。因此进行了模糊控制理论在磁悬浮系统中的研究,提出了模糊-PID控制。以经典PID控制器参数为参考,建立了模糊控制隶属度函数,设计了模糊控制表格,并对模糊-PID控制器在该系统中的应用进行了仿真研究,仿真结果表明,建立在经典PID控制器基础上的模糊-PID控制能够得到较好的稳态特性和动态性能,鲁棒性也得到增强,能够在一定程度上提高液浮陀螺仪的精度和抗干扰能力。     

随机变刚度电磁支撑-转子-轴承系统不定动力参数实验识别

识别出随机变刚度电磁支撑-转子-轴承系统的不定动力参数是实验研究随机支撑刚度参数转子动力学问题的前提。为此,基于Riccati传递矩阵法的相关理论和计算程序,结合电磁支撑-转子-轴承系统各种工况下的一阶固有频率实测值,对转子系统的不定动力参数进行了识别,给出转轴轴套、联轴器等附件对转子刚度加强作用的具体数值,以及滑动轴承的支撑刚度和扭转刚度参数值。将这些数据代入到转子动力学理论模型中,得到相同工况下两测点振型幅值比值的理论值,并与实验值进行了比较。结果表明:各测点振型幅值比值的理论值和实验值之间的偏差小于5%,说明转子系统不定动力参数识别结果的精度和准确度完全满足实验研究的要求。     

核主泵叶轮间隙的轴向振动特性研究

具有径向流的间隙结构广泛存在于轴承结构与旋转机械中,间隙中的流固耦合作用可能影响整体结构的运动稳定性。基于理论间隙模型和核主泵的实际结构,本文对径向间隙流引起的轴向振动进行了多方面的研究。当间隙的一个壁面产生轴向振动并处于旋转状态时,壁面受到由径向流引起的时变轴向力,因此间隙为叶轮提供附加的轴向刚度和阻尼。通过研究以水为介质的理论间隙模型,发现径向间隙流会引起负的等效轴向动力系数（刚度和阻尼）,并且流道形状是影响间隙轴向动力特性的重要因素。扩张流道和平行流道会产生负的轴向动力系数,特别是负阻尼会引起结构振动发散;而收缩流道间隙具有稳定的轴向动力特性。最后,对AP1000核主泵原型叶轮间隙模型进行分析,结果表明,间隙会引起轴向负刚度,并且在一定工况下出现负阻尼,此时系统轴向稳定性及结构安全运行将受到严重的不良影响。     

A COMPLEX PARAMETER MODEL UPDATING METHOD FOR DAMPING CHARACTERISTICS OF FINITE ELEMENT MODELS

阻尼对于结构动力学响应具有重要的影响,但有限元模型一般很难对阻尼特性进行精确建模.基于实测频响函数,研究了一种有限元模型阻尼特性的复参数修正方法.以待修正区域各单元质量、刚度矩阵的比例修正系数为复修正参数,建立了单元矩阵比例修正的灵敏度方程直接算法,并对比分析了复修正参数与不同阻尼特性之间的数学关系.以六自由度集中参数模型和25杆平面桁架模型为例,验证了复参数修正方法在阻尼特性修正中的有效性.     

金属丝网橡胶压缩力学性能研究

对金属丝网橡胶进行了静态压缩试验。利用控制变量法研究了压缩量、相对密度、金属丝丝径、丝材和承压面积对金属丝网橡胶压缩力学性能的影响,并对平均刚度和能量耗散系数随压缩量和相对密度的变化关系进行了研究。试验结果表明:随着压缩量的增加,金属丝网橡胶非线性力学特性逐渐增强;相对密度越大,金属丝网橡胶承压能力越强;金属丝的丝径和丝材主要影响金属丝网橡胶非线性阶段的力学特性,丝径越大,丝材越硬,承压能力越强;承压面积越大,金属丝网橡胶的承压和耗能性能越好;随着压缩量的增加,平均刚度增大,承压能力增强,能量耗散系数减小,减震性能降低;随着相对密度的增加,平均刚度和能量耗散系数均增大,承压能力和减震性能均增强。     

Dynamic properties of automotive damper modules

This paper addresses the dynamic properties of automotive shock absorber modules. Analyzing an equivalent linear system, a set of characteristic dimensionless numbers are introduced in order to qualify the dynamic performance of the damper and the damper module. The dependency of these numbers on the main parameters of the module like the damping constant, the spring stiffness of the damper, the top mount stiffness and the piston rod mass is shown. These numbers may also serve as similarity coefficients for quite different dampers regarding their dynamic behavior. Furthermore, they can be used to adjust the stiffness of the different force elements of the damper module to achieve an optimal damping quality.     

Development of a family of explicit algorithms for structural dynamics with unconditional stability

A new family of explicit integration algorithms is developed based on discrete control theory for solving the dynamic equations of motion. The proposed algorithms are explicit for both displacement and velocity and require no factorisation of the damping matrix and the stiffness matrix. Therefore, for a system with nonlinear damping and stiffness, the proposed algorithms are more efficient than the common explicit algorithms that provide only explicit displacement. Accuracy and stability properties of the proposed algorithms are analysed theoretically and verified numerically. Certain subfamilies are found to be unconditionally stable for any system state (linear elastic, stiffness softening or stiffness hardening) that may occur in earthquake engineering of a practical structure. With dual explicit expression and excellent stability property, the proposed family of algorithms can potentially solve complicated nonlinear dynamic problems.     

二类复特征值表达式的适用性研究

对于线性系统，根据其质量、刚度或阻尼等矩阵的性质了解特征值，是十分有意义的问题．对于有阻尼陀螺系统，本文首先通过模态正交性推导了有关矩阵的若干关系式．然后分析了复特征值的两类表达式的适用性，着重讨论了通过一元二次方程研究特征值性质的现行处理方法存在的困难．提出一种确定特征值的补充方法，指出可能存在虚数特征值的系统的性质．算例表明结论正确     

Bifurcation and chaos analysis of multistage planetary gear train

A nonlinear time-varying dynamic model for a multistage planetary gear train, considering time-varying meshing stiffness, nonlinear error excitation, and piece-wise backlash nonlinearities, is formulated. Varying dynamic motions are obtained by solving the dimensionless equations of motion in general coordinates by using the varying-step Gill numerical integration method. The influences of damping coefficient, excitation frequency, and backlash on bifurcation and chaos properties of the system are analyzed through dynamic bifurcation diagram, time history, phase trajectory, Poincaré map, and power spectrum. It shows that the multi-stage planetary gear train system has various inner nonlinear dynamic behaviors because of the coupling of gear backlash and time-varying meshing stiffness. As the damping coefficient increases, the dynamic behavior of the system transits to an increasingly stable periodic motion, which demonstrates that a higher damping coefficient can suppress a nonperiodic motion and thereby improve its dynamic response. The motion state of the system changes into chaos in different ways of period doubling bifurcation, and Hopf bifurcation.     

Evolutive and nonlinear vibrations of rotor on aerodynamic bearings

The use of air as a lubricant in aerodynamic bearings is advantageous, particularly in the food industry. Aerodynamic bearings with tilting pads have complicated stiffness and damping properties and need a very detailed theoretical and experimental research. Response curves of rigid rotor supported on aerodynamic bearings are presented for a linear but evolutive mathematical model. Due to non-monotone properties of stiffness and damping matrices at variable revolutions, a new resonance appears. The mathematical model of rotor vibrations in the whole area of bearing clearance is also developed in the consideration of strongly nonlinear properties of aerodynamic bearing.     

Damping Characterization and Viscoelastic Behavior of Laminated Polymer Matrix Composites Using a Modified Classical Lamination Theory

The damping property of materials can be defined as the ratio of dissipated energy over the total strain energy during the loading–unloading process, called the specific damping capacity (SDC). In this study, in order to characterize the damping properties of materials, a test plan in designed to extract the SDC of a single layer composite from hysteresis data. The theory of linear viscoelasticity incorporates a varying Young’s Modulus by using a complex stiffness modulus. Considering different lay-ups, the modified classical lamination plate theory is modified to represent both stiffness and SDC of laminates. The results are compared with experimental results for symmetric laminated specimen. This evaluation shows a very good agreement between theoretical and experimental results in the range of low frequency loading from 0.2 to 4 Hz. The complex compliance matrix changes the governing equation in to a complex form which contains both stiffness and damping properties.     

Transient response analysis of a steel beam with vacuum packed particles

In this paper the method of semi-active damping of vibrations is presented. Free vibrations of a cantilever steel beam encapsulated in a sleeve, filled with the granular material are investigated. Various values of the partial vacuum generated in the granular structure allow to control the global dissipative properties of the discussed system. The loose grains encapsulated in the hermetic, polyvinyl chloride (PVC) envelope transform into a rigid, viscoplastic body as the jamming mechanism occurs when the underpressure is generated. Such phenomenon enables original strategies for semi-active damping. A detailed discussion related to the experimental results concerning the amplitude of vibration, damping, stiffness, and frequency of the continuous granular beam system is provided. The simplified Finite Element Model succeeded in describing the dynamic response of the structure.     

Computational studies on high-stiffness,high-damping SiC–InSn particulate reinforced composites

With the objective of achieving composite material systems that feature high stiffness and high mechanical damping, consideration is given here to unit cell analysis of particulate composites with high volume fraction of inclusions. Effective elastic properties of the composite are computed with computational homogenization based on unit cell analysis. The correspondence principle together with the viscoelastic properties of the indium–tin eutectic matrix are then used to compute the effective viscoelastic properties of the composite. Comparison is made with parallel experiments upon composites with an indium–tin eutectic matrix and high volume fractions of silicon-carbide reinforcement. The analytical techniques indicate that combinations of relatively high stiffness and high damping can be achieved in particulate composites with high SiC volume fractions. Based on analysis, the tradeoffs between stiffness and damping characteristics are assessed by changing the volume fraction, size, packing, and gradation of the particulate reinforcement phases. Practical considerations associated with realization of such composites based on the surface energy between the SiC and the InSn are discussed.