液体黏性调速起动瞬态过程数值模拟研究

为揭示油膜挤压效应对液体黏性调速起动过程的影响,本文采用有限元素法联立求解修正瞬态雷诺方程、能量方程、润滑油黏温方程等对调速起动过程进行数值模拟研究.结果表明由于油膜在调速起动过程中逐渐减薄,挤压效应对油膜承载力产生较大的影响,但在起动过程的不同阶段其影响不同.在起动过程开始阶段,油膜挤压效应的影响较小,随着油膜的减薄,挤压效应对油膜承载力的影响越来越显著.调速起动试验验证了这一结果的正确性.     

微纳米结构壁面对流场及动压润滑的影响研究

固体边界具有的微纳米结构将影响流体在近壁面处的流动行为,进而由于尺度效应改变流体在整个微间隙的流动或润滑规律.将壁面可渗透微纳米结构等效为多孔介质薄膜,采用Brinkman方程来描述流体在近壁面边界渗透层内的流动,并将其与自由流动区域的不可压缩流体Navier-Stokes控制方程耦合,在界面处的连续边界条件下求解和分析了速度分布规律和压力变化规律.针对恒定法向承载力的油膜润滑条件,进一步讨论了静止表面或运动表面的微纳米结构对近壁面流动行为的影响;并揭示了考虑壁面微纳米结构的流体动压润滑的油膜厚度和摩擦系数的变化规律.论文结果为具有可渗透微结构表面的微间隙流动与润滑提供了理论参考.     

可控挤压油膜轴承主动控制转子系统振动

本文提出了“可控挤压油膜轴承”,以主动控制转子系统的振动,设计了不同的可控挤压油膜油承方案,借稳态不平衡响应构成的二次目标函数,分析比较了它们的振动控制效果,根据这一研究,可初步得到如下结论:对于航空发动机,可控挤压油膜轴承极有希望成为一种更有效的振动控制方法。     

挤压油膜阻尼器-滑动轴承转子系统动力学分析与优化设计

为了对挤压油膜阻尼器-转子系统中挤压油膜阻尼器(SFD)的各项参数进行优化设计,使转子系统的动力学性能达到最佳状态,本文综合运用转子动力学和油膜润滑基本理论以及数值分析方法,对SFD-滑动轴承转子系统的灵敏度及动力学优化进行了系统研究。灵敏度分析结果表明:轴承间隙c1、SFD间隙c2、油粘度η对转子系统的一阶临界转速的影响较大;SFD间隙c2、轴承间隙c1、转轴刚度K2对二阶临界转速的影响较大。据此得到优化的设计变量为c1、c2、η、K2,并采用遗传算法对临界转速进行了优化分析;经过优化后,系统的一阶、二阶临界转速差值由原来的510rad/s变为860rad/s,系统动力学性能得到较大改善。本文的优化设计结果可为此类转子系统的设计提供参考。     

孔隙渗流对环面复层含油轴承润滑性能的影响

含油轴承基体中油液的渗流特性对轴承油膜润滑性能影响显著. 以不同孔隙率分布的环面复层含油轴承为研究对象，利用达西定律建立复层含油轴承基体中流体渗流的控制方程，在极坐标下建立环面复层含油轴承系统渗流润滑模型，研究复层环面副系统中油膜压力分布规律，分析轴承结构参数及孔隙渗流行为对油膜润滑性能的影响. 结果表明:复层含油轴承的流体动压力主要发生在环形摩擦面间，从摩擦界面到轴承底面，流体压力逐渐由外缘向圆心部位传导，流体动压力作用面积逐渐增大，压力峰值逐渐降低；随着倾角增大，摩擦界面间的油膜动压效应增强，油膜润滑性能变好；随着表层渗透率或厚度减小，摩擦界面间的油膜的渗流效应减弱，油膜润滑性能提高；与普通单层含油轴承相比，含致密表层的复层含油轴承能降低整体孔隙率，防止过多轴承间隙油液渗入多孔介质，提高轴承润滑性能. 研究工作为明晰环面复层含油轴承渗流行为及润滑机理提供一定理论依据.      

转子系统振动的CSFDB主动控制实验研究

采用可控挤压油膜阻尼器作为主控元件,进行转子系统振动主动控制研究,设计开发了锥形可控挤压油膜阻尼器（Controllable Squeeze Film Damping Bearing,CSFDB).CSFDB的外环轴向位置通过专门设计的电液伺服系统来调节其平淡同的轴向位置对应不同的油膜间隙,使转子系统、CSFDB、电液伺 服系统形成一个闭环控制系统,即主动控制转子系统的振动,本文的实验研究工作内容有,CSFDB-转子系统振动特性实验研究;CSFDB-转子系统加、减速振动特性试验研究;转子系统振动的CSFDB主动控制实验研究。转子模型为一单盘悬臂转子,研究结果表明,CSFDB控制效果明显,所研制的控制仪工作可靠,能满足实时必研究;CSFDB外环位置调节系统设计思路可行,性能可靠避孕药推广应用前景。     

机构运动副间隙被动控制研究

将阶跃函数与牛顿二状态相结合 ,考虑曲柄非匀速运转 ,对含间隙平面连杆机构的副间分离与碰撞过程建立了动力学统一模型 ,利用该模型 ,引入粘弹性阻尼被动控制技术 ,通过算例分析了被动控制的效果。分析结果表明 ,在不改变机构基本参数的情况下将粘弹性材料引入到机构的间隙铰接处大大降低碰撞时引起的冲击效应 ,提高了机构运转的的稳定性 ,同时为含间隙机构控制领域的研究提供了新思路     

航空发动机整机耦合动力学模型及振动分析

面向航空发动机整机振动, 建立了航空发动机转子-滚动轴承-机匣耦合动力学模型. 该模型具有如下特点: (1)考虑转子、滚动轴承及机匣之间的耦合作用; (2)考虑了实际航空发动机的弹性支承及挤压油膜阻尼效应; (3)将转子考虑为等截面自由欧拉梁模型, 运用模态截断法进行分析; (4)考虑了滚动轴承间隙、非线性赫兹接触力以及变柔性VC(Varyingcompliance)振动; (5)考虑了转子与机匣之间的碰摩故障. 运用数值积分方法研究了航空发动机的整机振动规律, 包括: 滚动轴承VC振动分析、弹性支承刚度对耦合系统临界转速的影响、转轴模态截断阶数NM对系统响应的影响分析、挤压油膜阻尼器参数对系统响应的影响分析、突加不平衡的瞬态响应分析以及转静碰摩故障特性分析等.      

柔性转子──挤压油膜阻尼器系统的突加不平衡响应

本文选择了一种可以无限逼近阶跃函数,具有无穷阶连续导数的表示转子突加不平衡的数学模型.用此模型分析了支承在同心型及非同心型挤压油膜阻尼器上的柔性转子的突加不平衡响应.研究了系统参数对突加不平衡响应的影响及不同转速下突加不平衡对系统双稳态响应的影响.证明了设计合理的挤压油膜阻尼器对突加不平衡具有抑制作用.此外,非同心型挤压油膜阻尼器抗突加不平衡的能力要比同心型挤压油膜阻尼器强,但非同心型挤压油膜阻尼器在突加不平衡时容易产生非协调响应.     

考虑油膜力作用的船舶主推进系统冲击研究

舰船推进轴系是舰船动力装置的重要组成部分,它的稳定性是舰船生命力的基本保证.本文以舰船主推进轴系为研究对象,考虑了非线性油膜力的作用,在推进轴的非线性油膜力模型中,考虑了油膜涡动效应和挤压效应以及多个轴承油膜力的耦合影响,并考虑了轴承结构本身的刚度.文中采用弹性体动力学方法对推进轴建模,考虑了在外冲击作用下转速和轴承油膜力对于转轴冲击响应的影响,考虑横向运动与转动耦合作用,导出以非线性偏微分方程描述的舰船主推进轴的动力学方程,并用经典理论对其进行离散,最后采用龙格-库塔法进行数值仿真.实例分析指出转速对于转轴冲击响应的影响不可忽略.     

Effect of magnetic field and velocity slip on porous-walled rectangular squeeze films

This is a study of an electrically conducting flow in a squeeze film between two infinite strips where one of the strips has a porous bounding surface backed by a solid wall. The analysis is directed to study the interaction of a transverse magnetic field with the coupled flows in the squeeze film and the porous medium including the slip velocity at the porous bounding surface. Expressions for load capacity and thickness-time are obtained. It is observed that the magnetic field increases the load capacity and response times of squeeze films. This effect is more marked for small values of the permeability K.     

The flow of a power-law liquid in a continuous-flow squeeze film

Consideration is given to the flow of an inelastic ‘power-law’ liquid in a continuous flow squeeze film. This simulates the flow in a conventional squeeze film by continuously injecting fluid into the narrow gap between two plates through the lower plate (Oliver et al. [6]). To zero order in the usual lubrication approximation the results are identical with those for the conventional squeeze film. To first order, useful corrections to the normal force due to the effects of inertia are obtained.     

Combined effects of non-Newtonian couple stresses and fluid inertia on the squeeze film characteristics between a long cylinder and an infinite plate

On the basis of the Stokes micro-continuum theory together with the averaged inertia principle, the combined effects of non-Newtonian couple stresses and convective fluid inertia forces on the squeeze film motion between a long cylinder and an infinite plate are presented. A closed-form solution has been derived for squeeze film characteristics including the film pressure, the load capacity and the response time. Comparing with the Newtonian-lubricant non-inertia case, the combined effects of couple stresses and convective inertia forces provide an increase in the film pressure, the load capacity and the response time. In addition, the quantitative effects of couple stresses and convective inertia forces are more pronounced for cylinder–plate system operating at a larger couple stress parameter and film Reynolds number, as well as a smaller squeeze film height. To guide the use of the present study, a numerical example is also illustrated for engineers when considering both the effects of non-Newtonian couple stresses and fluid convective inertia forces.     

圆平板挤压膜实验及其参数识别

完成了简谐激励下水中平行圆板的挤压膜振动实验．用最小二乘法识别出非线性粘性挤压膜力模型中的４个系数．不同挤压膜厚、不同频率和不同振幅情况的数值模拟结果与实验值吻合较好．研究结果表明，所用模型可较好地描述粘性挤压膜运动，识别出的系数在一定范围内给出良好精度的数值模拟．     

NONLINEAR FLUID FORCES IN CYLINDRICAL SQUEEZE FILMS. PART I: SHORT AND LONG LENGTHS

Using three approximation methods, nonlinear models have been derived for short and long cylindrical squeeze films with arbitrary inner cylinder motions. Elliptical and parabolic velocity profiles are employed in the derivation in order to determine the effects of the choice of velocity profile. The only differences in the final squeeze film equations, due to the three approximation methods and the two velocity profiles, are in the four constant coefficients. Each term in the squeeze film equations is a nonlinear function of cylinder position. Comparing the present nonlinear expressions with existing models for short cylindrical squeeze films shows that the force terms are either exactly the same or have the same trends with instantaneous eccentricity values. For long cylindrical squeeze films, the present expressions have some force terms which are essentially the same as in other studies, while other force terms show variations with position which are very different from a previously published study.     

Combined effect of viscosity variation and non-Newtonian Rabinowitsch fluid in wide parallel rectangular-porous plate with squeeze-film characteristics

The present article carries out the study of viscosity variation of non-Newtonian fluid with the homogeneous porous wall on wide parallel rectangular-plate based on the Rabinowitsch fluid model. The non-linear modified Reynolds equation is derived for the lubrication of rectangular squeeze film bearing with viscosity variation and porous parameter. Using the Morgan–Cameron approximation, the nonlinear Reynolds-type equation for squeeze-film which governs the film pressure is solved within the fundamentals of small perturbation technique. The characteristic of the wide parallel rectangular-porous plate is numerically computed for different physical quantities such as film pressure, load carrying capacity and response time. Moreover, as limiting cases some of the results from the available literature are recovered also. Further, the findings reveal that the viscosity variation of non-Newtonian fluid and the presence of porous wall lead to reduction in the load capacity and the response time respectively. Here, the porous matrix consists of a system of capillaries of very small radii with the homogeneous porous wall. The impact of porosity is incorporated as a result it acts as self-lubrication on bearing surface. Also, the effect of viscosity variation is one of the most important characteristics of fluid which helps in the design of bearings for lubrication in engineering and industrial applications.

     

An experimental test of equations predicting the load bearing capacity of squeeze films of elastico-viscous liquid

A form of squeeze film apparatus was recently described in which the movement of one plate towards the other was simulated by the continuous volume generation of liquid over the plate area. The liquid exuded from a large number of holes in the lower plate surface and formed a “continous flow” version of squeeze film apparatus with no moving parts [1]. A later paper gave derivations of equations from which squeeze film load bearing capacity could be evaluated, taking into account viscous, inertial and normal stress effects in the liquid film [2].In order to find the total load in a squeeze film system, it was necessary to obtain the relationship between the first normal stress difference and shear rate for the liquid in use, using an experimental method. At high shear rates, the jet thrust method provided these data [3,4] and from them the load bearing capacity of squeeze films of hot, polymer-thickened oil were predicted [2].A more complete test of the method is possible with a highly elastic liquid because considerable load enhancement due to extra stress is present at moderate deformation rates in squeeze film systems [1,5,6,7]. Thus a 0.1 per cent aqueous polyacrylamide solution gives well-defined load enhancement and (quite independently) the jet thrust method gives the relationship between normal stress and shear rate from which predictions of load enhancement may be made. Furthermore, convergent nozzles may be used in the jet thrust apparatus [3] to measure the stress development in an elastic liquid which is being simulateneously sheared and stretched, a situation which more closely resembles the squeeze film case than that of steady shear.     

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。     

Surface roughness effects on squeeze film behavior in porous circular disks with couple stress fluid

The effect of surface roughness on squeeze film behavior between two circular disks with couple stress lubricant is analyzed when the upper disk has porous facing which approaches the lower disk with uniform velocity. The modified Stochastic Reynolds equation is derived on the basis of Stokes micro-continuum theory for couple stress fluid and Christensen Stochastic theory for the rough surface. Closed form solution of the Stochastic Reynolds equation is obtained in terms of Fourier–Bessel series. The importance of roughness and couple stress on bearing characteristics are presented in terms of load carrying capacity, squeeze time, and relative percentage of the load. It is observed that, effect of couple stress fluid, and surface roughness is more pronounced compared to classical case. These predictions enable design engineers to choose suitable parameters.     

Inertia effects in hydromagnetic lubrication

Summary A theoretical investigation of inertia effects in a squeeze film bearing with an electrically conducting lubricant in the presence of a uniform transverse magnetic field is presented. The two cases of infinitely long rectangular plates and circular plates as bearing surfaces are considered. It is shown that the load supporting capacity of the bearing increases and the squeeze decreases if the lubricant inertia effects are taken into account. However, the inertia effect becomes smaller when the strength of the magnetic field increases.