油膜惯性力对双盘转子—SFD系统突加不平衡和加速响应特性的影响

本文分析了雷诺数和系统参数对于转子—挤压油膜阻尼器(SFD)系统突加不平衡响应和加速响应特性的影响。研究结果表明:油膜惯性力对系统的动态特性有影响;对于考虑油膜惯性力的系统,系统参数的变化对突加不平衡响应也有影响;对于加速通过双稳态响应区的突加不平衡响应,突加不平衡发生在不同的转速比区,响应走的路径也不相同。      

豆包阻尼器的减振特性研究

豆包阻尼器是一种以柔性约束下非连续颗粒介质为特征的阻尼器。研究了豆包阻尼器在不同振动条件下的减振特性,揭示了主系统激励力、阻尼、固有频率以及豆包和主系统之间的间隙等参数的变化对其减振效率的影响规律,得到了对工程应用有指导意义的结论。     

新型粘弹性阻尼器及其模具设计研究

本文对新型粘弹性阻尼器的设计计算及模具设计进行了全面的描述和分析,并以某型机相关参数为原始数据走了一个全过程。     

金属橡胶动态隔振性能的实验研究

通过对金属橡胶元件进行的一系列实验,考察了振动频率、成型厚度、成型密度、振幅及预压缩(或初始位移)等对金属橡胶元件滞迟特性的影响规律,得到滞迟特性受成型参数尤其是成型厚度、成型密度、振幅及预压缩(或初始位移)的影响较大,随着这些参数的增大,金属橡胶元件的阻尼性能增强,而振动频率对金属橡胶元件滞迟特性的影响很小。同时对随机激励下金属橡胶元件的隔振性能进行了实验研究,得出金属橡胶减振器的隔振效率ε可达63.47%,且其隔振效率ε随激励的增大而增大。     

失衡旋翼的直升机自激振动分析模型

直升机使用中很可能出现旋翼各片桨叶特性不一致的情况,为了研究失衡旋翼对直升机自激振动的影响,建立了适用于地面、悬停及前飞状态的旋翼/机体耦合动稳定性分析模型。采用当量铰旋翼模型,计入动力入流的影响,分别在旋转坐标系和固定坐标系中建立了桨叶及机体的动力学方程。以减摆器失效对直升机地面共振的影响为例,对桨叶及机体的时域响应进行了非线性数值仿真,用Floquet传递矩阵法计算了摆振后退型模态频率及阻尼,并用时域分析进行了检验。结果表明,其中一个减摆器失效后,各片桨叶摆振运动特性相差很大,系统的摆振后退型模态阻尼下降幅度高达60%以上。     

金属橡胶-钢丝绳索型减摆阻尼器动力学建模与参数识别

研制了一种直升机旋翼系统金属橡胶—钢丝绳索减摆阻尼器,对其建立了非对称弹性黏性阻尼双折线迟滞恢复力模型,利用Fourier级数展开法对模型作线性化处理,基于力—位移迟滞回线中恢复力各个成分关于位移的对称关系,设计了一种参数分离的物理参数识别算法,数值仿真显示算法精度和抗噪性高,采用振幅3.2mm,频率3Hz的正弦位移载荷激励减摆器时,实测结果的计算表明模型及算法可用于实际研究。     

某机载电子设备结构随机振动分析

针对某安装有减振器的机载电子设备结构进行了随机振动分析。讨论了减振器的仿真方法,利用CAD软件建立了电子设备三维模型,导入Patran中进行几何处理并划分网格,设置边界条件,并采用Nastran软件进行有限元求解,得到结构在机载振动环境下的应力与加速度功率谱密度响应。仿真结果和实测结果比较吻合,可用于进行带减震器结构形式的仿真分析。     

Type synthesis of deployable mechanisms for ring truss antenna based on constraint-synthesis method

Space deployable antenna is the key equipment in realizing the communication and data transmission between the spacecraft and the earth. In order to enrich the configurations of deployable antennas, the type synthesis of deployable mechanisms for ring truss antenna is conducted in this study. First, the principle of the constraint-synthesis method based on screw theory is briefly described, the structure of the ring truss deployable antenna and its folding principle are analyzed, and the ring truss mechanism is divided into upper edges, lower edges and linkages. Then, based on the constraint-synthesis method, the type synthesis of the basic unit edges is carried out, a series of basic unit mechanisms are obtained from combining the basic unit edge mechanisms, and five mechanism units with fewer joints and simple structures are selected. Furthermore, simulation models of the five ring truss deployable mechanisms are built in Solidworks and Matlab software, and the deploying process is verified by the movement simulation. Finally, mechanism characteristics of the five mechanisms are analyzed and discussed, and a prototype is manufactured, verifying the analysis in this paper. This research provides a new way for the type synthesis of spatial deployable mechanisms, and the ring truss deployable mechanisms obtained in this study can be well applied in the field of aerospace.     

基于加速动态拉格朗日法的摩擦片阻尼分析

提出了一种可用于增强薄壁结构阻尼的波纹形片状干摩擦阻尼器，并利用一种改进的非线性动力学计算方法对其稳态响应特性进行了分析。首先通过两重减缩使非线性系统自由度变成接触节点间相对位移的形式从而降低矩阵规模，在高阶谐波平衡法的基础上引入了速度型动态拉格朗日法，并通过提供解析形式的雅克比矩阵来提高计算效率与数值稳定性，从而构成了用于预测非线性系统强迫响应的算法。在一个集中参数模型上用切向/法向刚度法与时域推进法这两种主流非线性计算方法对本文算法的合理性进行了验证。利用该算法对带有波纹形阻尼器的薄壁板结构进行分析，结果表明，摩擦片对薄壁板有很好的振动抑制作用，在质量仅占主体结构0.6%的情况下，能够使共振峰值下降75.4%。该算法表现出较高的计算效率，减缩模型使用和解析雅克比矩阵的引入使CPU时间减小到原来的0.5%以下。     

Nonlinear characteristic investigation of magnetorheological damper-rotor system with local nonlinearity

Magnetorheological (MR) dampers show superior performance in reducing rotor vibration, but their high nonlinearity will cause nonsynchronous response, resulting in fatigue and instability of rotors. Herein, we are devoted to the investigation of the nonlinear characteristics of MR damper mounted on a flexible rotor. First, Reynolds equations with bilinear constitutive equations of MR fluid are employed to derive nonlinear oil film forces. Then, the Finite Element (FE) model of rotor system is developed, where the local nonlinear support forces produced by MR damper and its coupling effects with the rotor are considered. A hybrid numerical method is proposed to solve the nonlinear FE motion equations of the MR damper-rotor system. To validate the proposed model, a rotor test bench with two dual-coil MR dampers is constructed, upon which experimental studies on the dynamic characteristics of MR damper-rotor system are carried out. The effects of different system parameters, including rotational speed, excitation current and amount of unbalance, on nonlinear dynamic behaviors of MR damper-rotor system are evaluated. The results show that the system may appear chaos, jumping, and other complex nonlinear phenomena, and the level of the nonlinearity can be effectively alleviated by applying suitable excitation current and oil supply pressure.