轴向交变载荷作用下螺栓联接结构的松动试验研究

在设计、试制螺栓加载装置的基础上,对螺栓联接结构进行了轴向振动的疲劳试验,获取了螺栓夹紧力的时变曲线,并对试验后的螺栓接触表面进行损伤分析,研究螺栓联接结构的松动机理.结果表明:在轴向振动条件下,螺栓联接结构的夹紧力下降较为明显,但拧出力矩相对于预紧力矩变化不大.螺栓的松动过程可分为以下两个阶段:试验初期由于螺栓接触面的塑性变形,夹紧力迅速下降;然后由于接触面之间的微动磨损,夹紧力缓慢下降.螺纹接触面之间的损伤机制主要为黏着磨损、磨粒磨损和剥层.     

横向交变载荷下TiCN/MoS2涂层螺栓的防松性能研究

基于自主设计的螺栓连接振动试验装置，系统研究了横向交变载荷下TiCN/MoS₂涂层螺栓分别与TiCN/MoS₂涂层螺母和无涂层螺母配合时连接结构的松动行为，并利用体式显微镜(OM)、扫描电子显微镜(SEM)、电子能谱仪(EDX)和白光干涉仪等微观分析设备对试验后的螺纹表面进行损伤分析，深入讨论其磨损机理. 结果表明:在相同试验条件下，TiCN/MoS₂涂层螺栓比无涂层螺栓螺纹表面的损伤轻微，连接结构的松动程度更低；与无涂层螺栓螺纹根部相同等效应力状态下，TiCN/MoS₂涂层螺栓连接结构的预紧力可提高约10%，螺纹表面的损伤减轻，同时连接结构的松动程度进一步降低；TiCN/MoS₂涂层螺栓螺纹表面的主要磨损机制为疲劳磨损.      

ANALYTICAL SOLUTION OF THE FREE VIBRATION OF VISCOELASTIC SANDWICH ANNULAR PLATE

基于薄板小挠度理论和Kelvin-Voigt 黏弹性本构方程,建立了黏弹性夹层环形薄板振动控制方程.采用分离变量法计算了内边固支、外边自由黏弹性夹层环形薄板的固有频率和振型,并与有限元计算结果进行比较. 分别讨论了夹心层比和内外半径比对固有频率及衰减系数的影响. 研究表明:系统频率随夹心层厚度增大,先增大后减小,而衰减系数一直增大;系统频率和衰减系数随内外半径比增大而增大.     

带有两端支座松动故障的转子系统的振动分析

应用现代非线性动力学理论，分析了带有两端支座松动故障的转子-轴承系统的复杂运动现象。模拟结果表明：带有两端支座松动故障的转子-轴承系统运动在未到共振区时以周期运动为主，在过共振区后，运动形式以拟周期和混沌为主，两个松动支座的振动在一定程度上相互抑制。同时，当支座发生松动时，轴颈的轴心轨迹以及支座的Poincare截面图和相轨迹都呈现出特殊的形状，并且这些形状又随松动支座的振幅是否达到最大间隙值而有所不同。上述结论可望为转子-轴承系统的松动故障的研究及故障诊断提供理论参考。     

斜拉桥塔-索-桥面连续耦合参数振动特性分析

针对端部激励作用下斜拉索与桥塔、桥面协同振动问题,考虑拉索几何非线性、倾角、阻尼以及拉索重力弦向分力的影响,引入拉索高精度抛物线形,建立了桥塔-索-桥面连续非线性精细化振动模型,推导了拉索与桥塔和桥面共同在激励作用下的耦合振动方程组,研究了桥塔-索-桥面结构系统参数的振动特性,并用数值仿真方法分析桥面与拉索频率比、桥面激励幅值、索力及拉索阻尼对结构耦合振动特性的影响规律。结果表明:桥面与拉索的频率比分别为1∶2和2∶1时,拉索会发生不同模式的大幅振动;相比于超谐波共振模式,亚谐波共振模式的拉索振幅更大,但达到共振所需时间较长;拉索振幅随桥面激励幅值的增大呈非线性增大,桥面激励幅值越大,拉索积蓄共振能量所需的时间越短;拉索振幅随索力增大而减小;拉索自身阻尼对其振动的影响较小,增大拉索阻尼时,拉索振幅虽有减小趋势,但是减小幅度有限。     

高压氢气泄漏自燃形成喷射火的实验研究

为了探究高压氢气泄漏发生自燃时所需的临界初始释放压力随管道长度的变化规律，了解管内自燃火焰向管外喷射火焰转变的发展过程，本文利用压力、光电以及高速摄像等测试系统展开实验研究。实验结果表明:当管道长度相同，初始释放压力较低时，氢气泄漏不容易发生自燃；随着管道长度的增加，氢气发生自燃时的临界初始释放压力先缓慢减小后迅速增大；当管道长度一定时，初始释放压力越大，激波传播速度越快，氢气管内自燃的位置距离爆破片越近；气流通过激波马赫盘后，火焰燃烧加剧；随着时间的增加，火焰长度呈现先增大后逐渐减小的变化趋势，喷射火焰尖端的平均传播速度逐渐减小；火焰宽度呈现先增大后迅速减小至稳定值的变化规律。     

矩形管道中微米级铝粉爆炸实验

在矩形管道粉尘爆炸装置中开展系列实验,系统研究了点火延迟时间、粉尘粒度及粉尘浓度对铝粉尘爆炸过程中最大爆炸压力和最大爆炸压力上升速率的影响。研究结果表明:不同的点火延迟时间对铝粉尘爆炸压力有显著影响,随着点火延迟时间由小变大,最大爆炸压力和最大爆炸压力上升速率呈现先增大后减小的趋势,且不同粒径的铝粉尘最大爆炸压力对应有不同点火延迟时间。随铝粉粒度的减小,最大爆炸压力和最大爆炸压力上升速率会呈现出先增大后减小的变化规律。铝粉最大爆炸压力和最大爆炸压力上升速率随浓度的增加均表现为先变大后减小的趋势,即铝粉浓度在特定数值时会使其爆炸威力最强。     

单向双筋板结构件共振疲劳试验及分析

航空航天领域广泛存在着振动疲劳问题,严重危及飞行器结构的安全可靠性。本文首先设计了激振器直接作用于试件的力激励振动疲劳试验系统,并提出了跟踪结构共振频率的频带激励共振疲劳寿命测试方法;而后利用试件进行了频带激励下的定应变共振或定载荷共振结构振动疲劳试验;最后针对试验结果分析与讨论了可能影响结构振动疲劳寿命的各种因素。结论表明,试验结构件的边界条件、初始条件以及结构动力学特性等都可能是影响振动疲劳寿命的关键因素。频带激励共振疲劳试验方法为振动疲劳寿命曲线的测试积累了经验。     

东海低渗储层压裂高起裂压力规律分析

东海HY-A1井H8b气藏为异常高温、高压地层,压裂设计的预测起裂压力与压裂施工不一致,作业中出现高起裂现象;考虑裂缝内流体压力、主应力、井壁渗透率、裂缝倾角等因素,建立了东海低渗储层压裂高起裂压力数学模型;通过现场验证,起裂压力计算误差为4.9%,具有一致性。借助二分法对模型求解,结果表明,随井斜角度的增大,当方位角<45°时,起裂压力变化随井斜角的增大并不明显,当方位角≥45°时,起裂压力呈现先减小后增大的趋势;随方位角的增大起裂角呈现先增大后减小,直至为零,起裂压力总体呈现先减小后增大的趋势;随着方位角增大,起裂压力存在最低峰值,最低峰值区间的方位角在50°～80°之间;井斜角α=0°直井段时,方位角φ=71°时,最低起裂压力峰值为58.5 MPa,在东海本区块属于高起裂;在一定的方位角度上起裂角存在最大峰值,起裂角最大峰值区间的方位角在60°～80°之间;应力差值大、泊松比小、异常高压是高起裂压力的关键因素;在压裂设计中,满足施工需求同时,尽可能设计方位角及井斜角靠近起裂压力最小区域。     

旋转碰摩板热冲击振动的解析法研究

提出了热冲击和碰摩故障共同作用下的旋转悬臂板系统动力特性解析解法. 基于变分原理,推导出考虑碰摩力沿宽度方向差异性的薄板系统运动微分方程,将该方程的解分解为热冲击悬臂板准静态解和碰摩薄板热冲击动力解. 通过计算旋转悬臂板的模态特性和温度分布函数,获得了碰摩叶片旋转悬臂板模型的热冲击振动解析解,讨论分析得出热冲击和碰摩故障对薄板振动的影响规律. 研究表明:碰摩振动表现为复杂的多频率耦合振动,高频振动较为显著;热冲击振动表现为简单的低频振动形式,强烈的热冲击导致碰摩薄板趋于低频振动. 碰摩引起的振动形式较热冲击故障更加复杂,更容易引起叶片的破坏. 增大的摩擦系数加剧了碰摩引起的振动,利用减小表面粗糙程度等方法降低摩擦系数,可以达到减小碰摩破坏程度的目的.      

二元复合材料板的自由振动: 半解析法

二元复合材料板是超材料板结构中常见的单元之一. 针对由材料参数相差两个量级的基体和嵌入体组成的二元复合材料板, 提出结构自由振动的半解析模型, 并对其振动特性进行了研究. 基于区域分解法和二元材料的分布, 将二维平板分解成两个子区域. 通过在振型函数中附加区域试函数, 来描述复合材料板面内刚度突变引起局部位移和转角的非光滑性. 基于二元复合材料板的基本边界条件和两子区连接处的变形协调条件, 构造了新的振型函数. 基于经典薄板理论, 利用带特殊试函数的里兹法, 求得不同几何构型下二元复合材料板的固有频率和振型, 并研究了嵌入体的尺寸和位置对结构振动特性的影响规律. 通过收敛分析并与有限元仿真结果对比, 验证了本文方法的准确性. 研究结果表明: 传统的全局试函数在分析具有振动局部化的模态时会得到不准确的结果, 而附加区域试函数可以显著提高里兹法的收敛速度以及结果的准确性; 嵌入体位置对低阶固有频率的作用不明显, 却能显著改变低阶振型节线的分布和振动局部化发生的区域.      

Global and local behaviour based composite damping studies on thin-walled box structure

The local (plate)/global (beam) vibration and damping behavior of composite thin-walled box member subjected to vibratory environment are studied and presented in this paper. This investigation is carried out by the use of 3D beam and thin plate finite elements and the corresponding modal frequencies/damping values of composite box beam are predicted by modal strain energy method. Application examples illustrate the ability of the 3D beam and thin plate element to predict both local and global modal frequencies/damping of hollow box sections. The influence of L/h ratio, b/h ratio and ply angle on the frequency and loss factor of composite box beam is investigated. In addition, an attempt has also been made to investigate the effect of temperature on the composite damping characteristics of rectangular box type section.     

分布振子复合板的模态阻尼及多点激励下阻尼减振相关性

分布阻尼振子可拓宽结构减振频带,因此可将振子分布于板中以形成复合板（简称“分布振子复合板”）,进而实现较宽的减振频带．对于多点支撑处受到宽频非一致激励（例如在不同激励点处的激励频率、幅值与相位有差异）的分布振子复合板,目前还缺乏有效简便的优化控制指标．在作者之前的研究中,针对含分布振子的梁推导了基于模态应变能的模态阻尼计算理论,讨论了模态阻尼与单点激励下梁的减振效果的相关性,并应用于宽频减振设计优化．本文进一步将模态阻尼计算理论推广到分布振子复合板,并将研究从梁的单点激励扩展到板的多点非一致激励下的阻尼减振相关性．首先,在利用模态应变能法推导得到分布振子复合板的模态阻尼计算公式后,从理论上讨论了不同边界条件与模态阶次对计算结果的影响,以及计算理论的适用性．而后,进一步通过有限元参数分析了边界条件、频率比、模态阶次与质量比的影响．最后,通过算例分析了无振子板或分布振子复合板在四个激励点具有多种幅值与相位组合情况下的稳态响应．结果表明,推导的模态阻尼计算公式可正确预测不同边界条件下的模态阻尼,且理论预测的模态阻尼与基板的稳态平均加速度减小率、稳态峰值应变能减小率均有较高的相关性．     

动载荷下螺栓连接的优化设计

把螺栓法兰密封连接结构简化成-质量、弹簧、阻尼系统，其中阻尼包括黏性阻尼和库仑阻尼两个部分。用此模型对法兰在指数衰减脉冲激励下的响应进行了数值仿真，研究了螺栓中预应力、螺栓个数、法兰螺栓间的阻尼对法兰结构响应的影响，螺栓中预应力和螺栓个数对螺栓变形峰值有较大影响，阻尼对螺栓峰值的影响较小。     

Measurement of mechanical vibration damping in orthotropic,composite and isotropic plates based on a continuous system analysis

The problem of free and forced transverse vibration of an orthotropic, composite, and isotropic thin square plates with uniformly distributed damping and simply supported boundary conditions has been solved, using a modal expansion technique. A load of the type P₀cosΩt applied at the center of plate has been considered and the phase angle between the forcing function and the vibration response at the center, as a function of the forcing frequency and the damping parameter determined. This theoretical relationship together with the experimentally measured phase angle between the applied mechanical forcing and the resulting vibration response at various forcing frequencies was used to determine an equivalent viscous damping parameter. This technique has been found to be particularly useful for the measurement and comparison of the relative damping in composite or orthotropic materials. Also, a theoretical relation for the energy loss due to viscous damping in vibrating plates has been developed and the theoretical energy loss at various frequencies has been compared with the experimentally measured energy loss at the same frequencies. Typical damping results are presented for aluminum, steel and aluminum/graphite-fiber composite materials.     

加热压电纤维复合材料圆板的横向自由振动

基于经典薄板理论和极正交各向异性材料的本构理论,建立了加热压电纤维复合材料圆板的线性振动控制微分方程。采用打靶法分别获得了加热压电纤维复合材料圆板在周边固支和简支情况下,无量纲固有频率随温度和电场强度变化的关系曲线,并分析了压电纤维体积分数、刚度参数、电场强度和温度变化对压电纤维复合材料圆板无量纲固有频率的影响。结果表明,一定体积分数或者电场强度下,压电纤维复合材料圆板的无量纲固有频率都随温度的升高而单调下降;同一温度下,刚度参数越小,无量纲固有频率越低;电场强度越大,无量纲固有频率越高。     

Finite Difference Method for the Acoustic Radiation of an Elastic Plate Excited by a Turbulent Boundary Layer: A Spectral Domain Solution

A finite difference method is developed to study, on a two-dimensional model, the acoustic pressure radiated when a thin elastic plate, clamped at its boundaries, is excited by a turbulent boundary layer. Consider a homogeneous thin elastic plate clamped at its boundaries and extended to infinity by a plane, perfectly rigid, baffle. This plate closes a rectangular cavity. Both the cavity and the outside domain contain a perfect fluid. The fluid in the cavity is at rest. The fluid in the outside domain moves in the direction parallel to the system plate/baffle with a constant speed. A turbulent boundary layer develops at the interface baffle/plate. The wall pressure fluctuations in this boundary layer generates a vibration of the plate and an acoustic radiation in the two fluid domains. Modeling the wall pressure fluctuations spectrum in a turbulent boundary layer developed over a vibrating surface is a very complex and unresolved task. Ducan and Sirkis [1] proposed a model for the two-way interactions between a membrane and a turbulent flow of fluid. The excitation of the membrane is modeled by a potential flow randomly perturbed. This potential flow is modified by the displacement of the membrane. Howe [2] proposed a model for the turbulent wall pressure fluctuations power spectrum over an elastomeric material. The model presented in this article is based on a hypothesis of one-way interaction between the flow and the structure: the flow generates wall pressure fluctuations which are at the origin of the vibration of the plate, but the vibration of the plate does not modify the characteristics of the flow. A finite difference scheme that incorporates the vibration of the plate and the acoustic pressure inside the fluid cavity has been developed and coupled with a boundary element method that ensures the outside domain coupling. In this paper, we focus on the resolution of the coupled vibration/interior acoustic problem. We compare the results obtained with three numerical methods: (a) a finite difference representation for both the plate displacement and the acoustic pressure inside the cavity; (b) a coupled method involving a finite difference representation for the displacement of the plate and a boundary element method for the interior acoustic pressure; (c) a boundary element method for both the vibration of the plate and the interior acoustic pressure. A comparison of the numerical results obtained with two models of turbulent wall pressure fluctuations spectrums - the Corcos model [3] and the Chase model [4] - is proposed. A difference of 20 dB is found in the vibro-acoustic response of the structure. In [3], this difference is explained by calculating a wavenumber transfer function of the plate. In [6], coupled beam-cavity modes for similar geometry are calculated by the finite difference method. This revised version was published online in July 2006 with corrections to the Cover Date.     

Analysis of frequency-domain vibration response of thin plate attached with viscoelastic free layer damping

To predict the vibration response of viscoelastic composite structure, two key issues need to be conducted, one is introducing the constitutive model of viscoelastic material into the analysis model and the other is describing the real damping behavior of viscoelastic composite structure. The emphasis of this study is to obtain the effects of frequency dependence on the vibration response of viscoelastic composite structure and the method of introducing two kinds of damping (viscoelastic material damping and remaining equivalent viscous damping). Vibration response analysis in frequency domain was investigated for viscoelastically damped plate. A cantilever plate attached with the ZN_1 viscoelastic free layer damping (FLD) was chosen to demonstrate the developed method. Frequency-domain response of the composite plate were solved and the obtained results were compared with the experimental values for the purpose of assessing the rationality of the proposed method. In addition, in order to obtain the effects of viscoelastic material parameters on vibration response of viscoelastic composite structure, a detailed parametric analysis was performed. This study shows that the frequency dependent characteristic of viscoelastic material has significant influence on the vibration response in the resonant region and acceptable results can be achieved in the non-resonant region if frequency dependent parameters are substituted by average values of the viscoelastic parameters reasonably in the analysis process.     

FREE VIBRATION OF ANISOTROPIC RECTANGULAR PLATES BY GENERAL ANALYTICAL METHOD

According to the differential equation for transverse displacement function of anisotropic rectangular thin plates in free vibration, a general analytical solution is established. This general solution, composed of the composite solutions of trigonometric function and hyperbolic function, can satisfy the problem of arbitrary boundary conditions along four edges. The algebraic polynomial with double sine series solutions can also satisfy the problem of boundary conditions at four corners. Consequently, this general solution can be used to solve the vibration problem of anisotropic rectangular plates with arbitrary boundaries accurately. The integral constants can be determined by boundary conditions of four edges and four corners. Each natural frequency and vibration mode can be solved by the determinate of coefficient matrix from the homogeneous linear algebraic equations equal to zero. For example, a composite symmetric angle ply laminated plate with four edges clamped has been calculated and discussed.     

基于机电阻抗技术的管道法兰结构健康监测实验研究

基于机电阻抗技术,采用一种新型压电陶瓷纤维复合材料MFC(Macro-fiber composite),对管道连接处法兰的螺栓工况进行监测实验研究。首先,研究了螺栓扭矩大小对管道法兰结构的阻抗的影响程度。在对螺栓开始施加扭矩时阻抗值变化明显,当扭矩增大到一定程度后,阻抗变化减缓。同时进一步研究了松动螺栓数量与管道法兰结构的阻抗变化之间的关系。结果显示,结构的损伤值随松动螺栓个数的增加呈线性增长。采用均方根偏差统计算法,对在不同工况条件下管道法兰结构处测得的阻抗值进行了有效的分析和处理。结果表明,采用MFC作为压电敏感元件的机电阻抗法,用于管道法兰结构健康监测具有较好的稳定性和应用潜力。