MODELLING AND VIBRATION CONTROL OF BEAMS WITH PARTIALLY DEBONDED ACTIVE CONSTRAINED LAYER DAMPING PATCH

A detailed model for the beams with partially debonded active constraining damping (ACLD) treatment is presented. In this model, the transverse displacement of the constraining layer is considered to be non-identical to that of the host structure. In the perfect bonding region, the viscoelastic core is modelled to carry both peel and shear stresses, while in the debonding area, it is assumed that no peel and shear stresses be transferred between the host beam and the constraining layer. The adhesive layer between the piezoelectric sensor and the host beam is also considered in this model. In active control, the positive position feedback control is employed to control the first mode of the beam. Based on this model, the incompatibility of the transverse displacements of the active constraining layer and the host beam is investigated. The passive and active damping behaviors of the ACLD patch with different thicknesses, locations and lengths are examined. Moreover, the effects of debonding of the damping layer on both passive and active control are examined via a simulation example. The results show that the incompatibility of the transverse displacements is remarkable in the regions near the ends of the ACLD patch especially for the high order vibration modes. It is found that a thinner damping layer may lead to larger shear strain and consequently results in a larger passive and active damping. In addition to the thickness of the damping layer, its length and location are also key factors to the hybrid control. The numerical results unveil that edge debonding can lead to a reduction of both passive and active damping, and the hybrid damping may be more sensitive to the debonding of the damping layer than the passive damping.     

VIBRATION ATTENUATION VIA CONSTRAINED LAYER DAMPING AND DASHPOT ON A SPRING-MASS-PLATE SYSTEM

The vibrations and damping characteristics of an annular plate with constrained layer damping (CLD) treatment subject to a traveling spring-mass-damper (SMD) are investigated. The equations of the CLD-treated plate are first derived from the energy principle. These equations are simplified via the Donnell-Mushtari-Vlasov assumptions. The response equations are eventually uncoupled for each mode and are in terms of a single-degree-of-freedom (s.d.o.f.) linear oscillator with hysteretic damping. The receptance method follows to joint the plate and the SMD, and the resulting change of natural frequencies and damping ratios are investigated. Individual effects due to the inertia and the stiffness are illustrated as well. The results shows that the damping ratios resulted from the viscoelastic core are more significant than that from the viscous damper. In addition, there exists a best design on the thickness of the viscoelastic material core to have the maximum damping ratios. The results also show that the attachment of SMD bifurcated the plate's natural frequencies for every mode but n = 0. The bifurcation becomes more obvious with the rotational speed. These results provide useful information for vibration suppression in engineering design.     

A FINITE ELEMENT FORMULATION FOR COUPLING RIGID AND FLEXIBLE BODY DYNAMICS OF ROTATING BEAMS

The work presented in this paper is based on an existing comprehensive formulation for rotating flexible systems. In the existing formulation the flexible degrees of freedom (d.o.f.) are represented by an analytically computed modal basis and the coupling matrices between the rigid- and the flexible-body d.o.f. are developed based on the analytical modal representation of the flexible d.o.f. In this paper, the existing formulation is generalized for rotating beams by representing the flexible d.o.f. either as physical d.o.f. of a finite element formulation or as a set of retained and internal d.o.f. of a Craig-Bampton formulation. The coupling matrices between the rigid-body rotation and the flexible d.o.f. are developed accordingly. The non-linear effects from the work done by the centrifugal forces are included in the formulation. Finite element shape functions of a beam element in a three-dimensional space and finite element shape functions for solid elements are employed for deriving the coupling terms between the rigid-body d.o.f. and the physical d.o.f. An additional transformation is required and performed when the right-body d.o.f. are coupled with the internal and the retained d.o.f. of a Craig-Bampton formulation. The coupled system of equations is solved in the time domain by combining the Newmark method for time integration and the Newton-Raphson method for solving the non-linear system of equations within each time step. Analyses are performed for a flexible rotating beam in order to validate the development. An analytical solution is compared with the new formulations that represent the rotating beam flexibility with the physical d.o.f. of beam or solid elements. The analytical solution is also compared to the formulation that represents the flexible d.o.f. in terms of retained and internal d.o.f. of a Craig-Bampton formulation. Very good correlation between the analytical and numerical results is observed.     

RANDOM VIBRATION OF A ROTATING BLADE WITH EXTERNAL AND INTERNAL DAMPING BY THE FINITE ELEMENT METHOD

The finite element model is employed to investigate the mean-square response of a rotating blade with external and internal damping under stationary or non-stationary random excitation. The blade is considered to be subjected to white-noise and earthquake excitations. The effects of rotational speed, external and internal damping on the mean-square response are studied. It is found that the mean-square response decreases quickly when the external and internal damping increases within some scope. Moreover, the increment of rotational speed will reduce the mean-square response of a rotating blade. It is also found that the mean-square response decreases when the low natural frequency of base decreases. Inversely, the mean-square response increases when the high natural frequency of base (natural frequencies of base are over the first natural frequency of blade) decreases. The reliability of a rotating blade subjected to stationary or non-stationary excitations is also obtained.     

ANALYTICAL AND NUMERICAL STUDY ON SPATIAL FREE VIBRATION OF NON-SYMMETRIC THIN-WALLED CURVED BEAMS

For spatial free vibration of non-symmetric thin-walled circular curved beams, an accurate displacement field is introduced by defining all displacement parameters at the centroidal axis and three total potential energy functionals are consistently derived by degenerating the potential energy for the elastic continuum to that for thin-walled curved beams. The closed-form solutions are newly obtained for in-plane and out-of-plane free vibration analysis of monosymmetric curved beams respectively. Also, two thin-walled curved beam elements are developed using the third and fifth order Hermitian polynomials. In order to illustrate the accuracy and the practical usefulness of the present method, analytical and numerical solutions by this study are presented and compared with previously published results or solutions by ABAQUS' the shell element. Particularly, effects of the thickness curvature as well as the inextensional condition are investigated on free vibration of curved beams with monosymmetric and non-symmetric cross-sections.     

ANALYSIS OF THE FLEXURAL VIBRATION OF A THIN-PLATE BOX USING A COMBINATION OF FINITE ELEMENT ANALYSIS AND ANALYTICAL IMPEDANCES

Many practical built-up thin-plate structures, e.g., a modern car body, are essentially assemblies of numerous thin plates joined at their edges. The plates are so thin that they invariably support the weight of the structure and machinery using their substantial in-plane stiffness. Consequently, vibrational power injected into the structure from sources mounted at these stiff points is controlled by high impedance long-wavelength in-plane waves in the plates. As the long in-plane waves propagate around the structure, they impinge upon the numerous structural joints at which short-wavelength flexural waves are generated in adjoining plates. These flexural waves have much lower impedance than the in-plane waves. Hence, the vibration of thin-plate structures excited at their stiff points develops into a mixture of long in-plane waves and short flexural waves. In a previous paper by the same authors, a numerically efficient finite element analysis which accommodated only the long in-plane waves was used to predict the forced response of a six-sided thin-plate box at the stiff points. This paper takes that finite element analysis and, drawing on theory developed in two additional papers by the same authors, couples analytical impedances to it in order to represent the short flexural waves generated at the structural joints. The parameters needed to define these analytical impedances are identified. The vibration of the impedances are used to calculate estimates of the mean-square flexural vibration of the box sides which compare modestly with laboratory measurements. The method should have merit in predicting the vibration of built-up thin-plate structures in the so-called “mid-frequency” region where the modal density of the long waves is too low to allow confident application of statistical energy analysis, yet the modal density of the short flexural waves is too high to allow efficient finite element analysis.     

透射式GaAs光电阴极AlGaAs窗层和GaAs光电发射层界面应变状况的X射线衍射研究

本文介绍了应变和弛豫的概念以及倒易点在倒易空间的分布,阐明了GaAs光电阴极AlGaAs窗层和GaAs光电发射层界面应变状况的X射线衍射的分析方法,最后给出了实例.     

FREE VIBRATION ANALYSIS OF A SPINNING FLEXIBLE DISK-SPINDLE SYSTEM SUPPORTED BY BALL BEARING AND FLEXIBLE SHAFT USING THE FINITE ELEMENT METHOD AND SUBSTRUCTURE SYNTHESIS

Free vibration of a spinning flexible disk-spindle system supported by ball bearing and flexible shaft is analyzed by using Hamilton's principle, FEM and substructure synthesis. The spinning disk is described by using the Kirchhoff plate theory and von Karman non-linear strain. The rotating spindle and stationary shaft are modelled by Rayleigh beam and Euler beam respectively. Using Hamilton's principle and including the rigid body translation and tilting motion, partial differential equations of motion of the spinning flexible disk and spindle are derived consistently to satisfy the geometric compatibility in the internal boundary between substructures. FEM is used to discretize the derived governing equations, and substructure synthesis is introduced to assemble each component of the disk-spindle-bearing-shaft system. The developed method is applied to the spindle system of a computer hard disk drive with three disks, and modal testing is performed to verify the simulation results. The simulation result agrees very well with the experimental one. This research investigates critical design parameters in an HDD spindle system, i.e., the non-linearity of a spinning disk and the flexibility and boundary condition of a stationary shaft, to predict the free vibration characteristics accurately. The proposed method may be effectively applied to predict the vibration characteristics of a spinning flexible disk-spindle system supported by ball bearing and flexible shaft in the various forms of computer storage device, i.e., FDD, CD, HDD and DVD.     

关于热电子发射理论的评述(Ⅱ)——单原子层和偶极子理论

本文对热电子发射中应用单原子层和偶极子理论作了分析和批判。我们认为:1.单原子层的存在不是无条件的,它与基底的温度、结构、纯度和外界真空度都有关系;2.关于时而能、时而又不能观察到的电子发射峰值,是一个有待于进一步明确的现象,不能简单地用单原子层和偶极子理论来解释;3.吸附了外界原子或分子使电子发射增加的事实,并不是由于偶极矩降低了基底的逸出功,发射的电子来源于被吸附物质的价电子;4.实验证明“L”阴极是Ba-O-W系统,它既不是单原子层,也不是单分子层,也不适用偶极子理论。     

n-Hg_(0.80)Mg_(0.20)Te界面积累层中二维电子气的输运特性研究

通过变磁场霍耳测量研究了MBE生长的Hg0 .80 Mg0 .2 0 Te薄膜在 1 5— 2 5 0K温度范围内的输运特性 .采用迁移率谱 (MS)和多载流子拟合过程 (MCF)相结合的方法对实验数据进行了分析 ,由该方法获得的结果和ShubnikovdeHass(SdH)振荡测量的结果都证明材料中存在二维 (2D)电子和三维 (3D)电子 .其中 2D电子主要来自于Hg1-xMgxTe CdTe的界面积累层或Hg1-xMgxTe与真空界面附近的积累层 .3D电子迁移率随温度的变化关系表明了Hg1-xMgxTe中的电子散射机理与Hg1-xCdxTe中的非常相似 :在低温下电离杂质散射 (考虑了屏蔽效应 )起主导地位 ,而温度在 10 0K以上时 ,晶格散射占主导地位 .     

化学腐蚀和硫处理对InSb(111)表面的影响

本文应用俄歇电子能谱和X射线光电子能谱对化学腐蚀和硫处理的InSb表面进行了研究。实验中发现经过CP-4腐蚀以后在样品的表面生成了InSb的氧化层,氧化层中的组分是锑的氧化物明显多于铟的氧化物。样品经过硫处理以后能够除去InSb表面的氧化层并且形成硫化物钝化层。 关键词：     

X射线研究CeO2缓冲层

我们在有和无离子束辅助两种情形下,在双轴织构Ni基底上制备了CeO2薄膜,结果表明,无离子束辅助沉积时,薄膜表现出(111)取向,在离子能量为240eV,束流为200μA/cm2,基片温度为360℃的条件下沉积的CeO2薄膜呈现出良好的立方织构.另外,我们分析了薄膜应力随温度和离子辅助条件的变化关系,结果表明,离子束轰击可以减小薄膜应力,在360℃附近薄膜应力几乎被完全弛豫.     

Na在Si(111)表面(3×1)有序吸附结构的光电子能谱研究

分析了Si(111)7×7表面上Na(3×1)有序吸附的同步辐射光电子能谱的变化,并与Paggel等的扫描隧道显微镜和光电子能谱比较,得出Na吸附在类余留原子(rest atom)的位置,支持Mnch的模型,与室温下无序吸附Na的光电子能谱相比较,得出Na-Si界面肖特基势垒形成是由Na与Si原子之间的相互作用决定,与表面构形是否有序关系不大,势垒高度与MIGS理论预计值相符。     

MgB_2和Mg_(0.93)Li_(0.07)B_2的电阻率与霍尔效应研究

测量了MgB2 和Mg0 .93Li0 .0 7B2 的电阻率 ρ(T)与霍尔系数RH(T)的温度依赖关系 .电阻率的测量结果表明 ,MgB2 和Mg0 .93Li0 .0 7B2 的正常态电阻率与温度有平方的依赖关系 .MgB2 和Mg0 .93Li0 .0 7B2 的超导转变温度几乎相同 .霍尔系数的测量结果表明 ,MgB2 和Mg0 .93Li0 .0 7B2 的载流子类型为空穴型 ,二者的霍尔系数都随温度升高而减小 ,且Mg0 .93Li0 .0 7B2 的霍尔系数比MgB2 略有减小 ,这可能与Li掺杂引入空穴有关 .二者的霍尔角都与温度平方呈线性关系 .     

CO与K在Cu(111)面上共吸附的角分辨紫外光电子能谱

CO在有K沉积的Cu(111)面上吸附的角分辨紫外光电子能谱(ARUPS)测量结果表明:在室温下,有分子状态的CO吸附在该表面,CO分子的4σ态信号强度明显低于5σ/1π态的强度,这表明CO分子在该状态下是强烈倾斜的,低温下(～150K),有两种不同的CO吸附状态,一种只有在较高CO暴露量下才出现,而另一种则在任何暴露量下都存在,后者是一种类似于CO在室温时的吸附状态。 关键词：     

CO在K/Cu(111)表面吸附的功函数变化

K覆盖的Cu(111)表面在室温下可吸附CO(可能是分解吸附),在K的覆盖度θ_K明显小于θ_min(θ_min≈0.18)的范围内,室温下CO的吸附使表面功函数增大。当θ_K≥θ_min时,表面功函数先减小,达一极小值后再随CO暴露量增大。这一结果可以用凝胶一平板(Jellium-slab)模型的图象很好地解释。 关键词：     

O-(α-氰基-间-苯氧基苄基)硫代磷酸酯和磷酰胺的NMR研究

本文合成了20个题示的化合物,研究了它们的¹H和³¹P谱,找出了δ_P与取代基关系的一些规律,观察到了手性中心对δ_H的影响、及一个手性中心对另一个手性中心R、S体不等价的诱导位移,并观察了产物中R、S体的不同含量比例。     

C2H4在清洁和有Cs覆盖的Ru(0001)表面吸附的TDS研究

用热脱附谱(TDS)方法研究了乙烯(C₂H₄)在Ru(0001)表面上的吸附.在低温下(200K以下)乙烯可以在清洁及有Cs的Ru(0001)表面上以分子状态稳定吸附,在衬底温度升高至200K以上时,乙烯发生了脱氢分解反应,乙烯分解后的主要产物为乙炔(C₂H₂).在清洁的Ru(0001)表面,乙烯有两种吸附状态,脱附温度分别为275K和360K.而乙炔的脱附温度为350K.在Ru(0001)表面有Cs的存在时,乙烯分解 关键词： 乙烯 钌(0001)表面 铯钌(0001)表面乙烯 钌(0001)表面 铯钌(0001)表面     

用微波ECR等离子体溅射法在蓝宝石(0112)晶面上生长ZnO薄膜的研究

蓝宝石上外延生长ZnO薄膜在表面波和声光器件中有重要的应用．用微波电子回旋共振(ECR)等离子体溅射法在蓝宝石(0112)晶面上外延生长了ZnO薄膜,膜无色透明,并且表面光滑,基片温度为380℃,为探索沉积工艺参数对薄膜结构的影响,用XRD对不同基片温度和沉积速率生长的ZnO薄膜进行了研究．     

用总能量密度泛函集团方法研究I/Si(111)及I/Ge(111)表面吸附

本文中用自洽总能量密度泛函集团方法研究了Ⅶ族的Ⅰ在Si(111)和Ge(111)表面的吸附。分别采用了两种集团模型来模拟顶位和三度位构型,用总能量极小原理确定了吸附的最佳构型和吸附能量,得到顶位比三度位吸附更为稳定的结果,与SEXAFS实验结果一致。本文还计算了Ⅶ族元素F,Cl,Br,I在Si(111)顶位吸附的状态密度,讨论了这系列DOS的变化情况,并与实验或其他理论结果进行了比较,最后还讨论了半经验EHT方法的适用性及限制。 关键词：