Calibration and assessment of moment actuator

A moment actuator with direct detection of forces is described. Moment frequency response and moment excitation purity as performance criteria are proposed. Methods for the performance calibration of the actuator are presented. Assessment is carried out by means of the reciprocity principle. Supported by the Natural Science Foundation of Guangdong Pronvince of China under Grant 960736.     

Measurement of rotational components of structures and machines

In this paper, the measuring methods of the rotational components, i. e. the free angular velocity and the moment mobility are presented. The performance of a moment actuator composed of two magnetostrictive rods (Tb_0.3 Dy_0.7 Fe_1.95) is discussed. Both theory and experiment show that the performance of the moment actuator does not influence the measurement results of the moment mobilities basically but affects the efficiency for exciting rotation. The efficiency for exciting rotation has also been calculated.     

含间隙铰接的柔性航天器刚柔耦合动力学与控制研究

大型柔性航天器展开锁定后,运动副中仍存在大量无法消除的间隙. 铰链间隙直接影响柔性航天器的姿态 运动和有效载荷的指向精度及稳定度,会对航天器的动力学特性造成较大的影响. 针对这一问题, 提出一种含间隙铰 接的航天器刚柔耦合动力学建模与控制方法. 首先建立含间隙的铰链精确动力学模型,从而构建含间隙铰接的柔性结构 动力学模型. 然后利用哈密顿原理和模态离散方法,建立含间隙铰接柔性航天器离散形式的刚柔耦合非线性动力学 模型,采用 Newmark 算法对非线性动力学方程进行求解. 基于压电纤维复合材料 (macro fiber composite, MFC) 驱动器 构建航天器的刚-柔-电耦合动力学方程,采用最优控制设计控制律. 分析了铰链参数、中心刚体转动惯量、间隙尺寸和间隙数目对航天器动力学特性的影响,着重研究了铰链间隙对航天器姿态运动和结构振动的影响作用. 最后采用 MFC 驱动器对航天器施加主动控制. 结果表明,铰链参数和中心刚体转动惯量影响航天器的固有频率;随着铰链间隙尺寸的增大及间隙数目的增多,航天器的整体刚度逐渐减小,而航天器的姿态角和振动位移响应不断增大;通过基于 MFC 的主动控制,能够实现含间隙铰接航天器姿态运动与结构振动的协同控制,并缓解间隙对系统动态特性造成的影响.      

稀土超磁致伸缩材料应力与电磁耦合特性的实验研究

讨论了稀土超磁致伸缩棒特性实验的若干应力与电磁耦合问题，利用自己设计制作的实验装置建立了应力电磁耦合系统的物理模型，应用阻抗分析方法得到了相应的等效电路。测定了在电磁场与应力场共同作用下ＴｂｘＤｙ１－ｘＦｅ２－ｚ三元稀土合金超磁致伸缩棒的磁致伸缩系数，机电耦合系数等。针对磁通泄漏问题，专门设计制作了圆柱型硅钢密闭磁路，本的实验结果为稀土眼磁致伸缩材料应用器提供了重要而准确的数据。     

磁头精定位控制中压电致动特征的解析解

利用压电弹性介质的二维本构关系,对于分割电极片状压电致动器在恒定的反平行电场作用下的电-力致动特性,在对自由端边界作圣维南意义下的放松处理后,采用弹性力学的半逆求解方法,导出了其力-电耦合的静态位移和应力分布的解析解.通过将所得解析解与没有简化假设的有限元数值解进行比较,结果表明:所得解析解的致动特性（即自由端位移随外加电压的变化特征）与数值解的结果几乎完全重合,表明其二维解析解是有效和可靠的.     

DYNAMICS AND CONTROL OF RIGID-FLEXIBLE COUPLING FLEXIBLE SPACECRAFT WITH JOINT CLEARANCE1)

大型柔性航天器展开锁定后,运动副中仍存在大量无法消除的间隙. 铰链间隙直接影响柔性航天器的姿态 运动和有效载荷的指向精度及稳定度,会对航天器的动力学特性造成较大的影响. 针对这一问题, 提出一种含间隙铰 接的航天器刚柔耦合动力学建模与控制方法. 首先建立含间隙的铰链精确动力学模型,从而构建含间隙铰接的柔性结构 动力学模型. 然后利用哈密顿原理和模态离散方法,建立含间隙铰接柔性航天器离散形式的刚柔耦合非线性动力学 模型,采用 Newmark 算法对非线性动力学方程进行求解. 基于压电纤维复合材料 (macro fiber composite, MFC) 驱动器 构建航天器的刚-柔-电耦合动力学方程,采用最优控制设计控制律. 分析了铰链参数、中心刚体转动惯量、间隙尺寸和间隙数目对航天器动力学特性的影响,着重研究了铰链间隙对航天器姿态运动和结构振动的影响作用. 最后采用 MFC 驱动器对航天器施加主动控制. 结果表明,铰链参数和中心刚体转动惯量影响航天器的固有频率;随着铰链间隙尺寸的增大及间隙数目的增多,航天器的整体刚度逐渐减小,而航天器的姿态角和振动位移响应不断增大;通过基于 MFC 的主动控制,能够实现含间隙铰接航天器姿态运动与结构振动的协同控制,并缓解间隙对系统动态特性造成的影响.     

Stabilization of the Parametric Resonance of a Cantilever Beam by Bifurcation Control with a Piezoelectric Actuator

In this work, bifurcation control using a piezoelectric actuator isimplemented to stabilize the parametric resonance induced in acantilever beam. The piezoelectric actuator is attached to the surfaceof the beam to produce a bending moment in the beam. The dimensionlessequation of motion for the beam with the piezoelectric actuator on itssurface is derived and the modulation equations for the complexamplitude of an approximate solution are obtained using the method ofmultiple scales. We then acquire the bifurcation set that expresses theboundary of the stable and unstable regions. The bifurcation set ischaracterized by the modulation equations. Next, we determine the orderof feedback gains to modify these modulation equations. By actuating thepiezoelectric actuator under the appropriate feedback, bifurcationcontrol is carried out resulting in the shift of the bifurcation set andthe expansion of the stable region. The main characteristic of thestabilization method introduced above is that the work done by thepiezoelectric actuator is zero in the state where the parametricresonance is stabilized. Thus zero power control is realized in such astate. Experimental results show the validity of the proposedstabilization method for the parametric resonance induced in thecantilever beam.     

人工肌肉作动器的参数优化设计

由于电活性聚合物材料在电场作用下所表现出的许多优异的力学性能,如大应变、响应快、能量转换率高等特点,使得这种高分子智能材料引起了广泛关注,有望被加工成作动器、传感器及俘能器等能量转换器,在工程应用中发挥巨大作用。 但是,由于描述电活性聚合物材料变形的状态方程的非线性性,及其在力电载荷作用下多种失效模式的存在,使得设计电活性聚合物能量转换器面临诸多的困难。本文针对美国人工肌肉公司(Artificial Muscle Inc.)开发的一款电活性聚合物薄膜作动器的优化设计开展研究,主要研究了不同初始预拉伸对薄膜厚度、拉伸变形、应力及电场强度等的影响效应,结果表明,在某一预拉伸下,薄膜中的电场分布将趋于均匀。本文所提供的研究方法,可为此类作动器的优化设计提供基本的分析模式。     

典型连接结构螺栓的附加弯矩形成机理与承载能力研究及结构优化设计

针对典型连接结构中, 高强螺栓在受拉工况下因产生附加弯矩而极大削弱其承载能力的问题, 开展了螺栓附加弯矩产生的机理研究, 并提出了一种有效降低螺栓附加弯矩的结构优化设计方法. 首先, 建立典型连接结构的等效力学模型, 推导出螺栓附加弯矩的解析解, 进一步开展数值仿真分析, 验证了解析方法的正确性. 考虑螺栓同时承受拉弯耦合载荷工况, 引入梁塑性弯曲理论, 研究了不同拉弯组合下的螺栓截面各类应力分布的交互关系, 并给出了考虑轴力影响的弯矩塑性折减系数. 基于最大应力破坏准则, 开展了考虑附加弯矩和弯曲塑性影响的螺栓载荷失效判据研究, 该判据更加具有工程应用价值. 从机理出发, 开展典型连接结构优化设计以降低螺栓的附加弯矩进而提高其承载能力, 进一步采用解析方法, 阐述了铰支球头的工作机理. 采用数值仿真方法, 开展了螺栓附加弯矩灵敏度分析, 验证了优化设计方法的有效性. 进一步开展试验研究, 获得不同连接状态下螺栓的附加弯矩, 验证了优化设计方法的正确性和可行性. 该方法能够极大降低高强螺栓的附加弯矩, 最大程度发挥螺栓的承载能力, 提高连接结构的可靠性.      

机翼尺度效应对等离子体分离流动控制特性的影响

等离子体流动控制技术是一种以等离子体气动激励为控制手段的主动流动控制技术. 为了进一步提高等离子体激励器可控机翼尺度, 以超临界机翼SC(2)-0714大迎角分离流为研究对象, 以对称布局介质阻挡放电等离子体为控制方式, 以测力、粒子图像测速仪为研究手段, 从等离子体激励器特性研究出发, 深入开展了机翼尺度效应对等离子体控制的影响研究, 提出了适用于分离流控制的能效比系数, 探索了分离流等离子体控制机理, 掌握了机翼尺度对分离流控制的影响规律. 结果表明: (1)随着机翼尺度的增大, 布置到机翼上的激励器电极长度会相应增加; 在本文的参数研究范围内, 激励器的平均消耗功率不会随电极长度的增加而线性增大; 当电极长度达到一定阈值时, 激励器的平均消耗功率趋于定值; (2)在固定雷诺数的情况下, 随着机翼尺度的增大, 等离子体的控制效果并未降低, 激励器能效比系数提高; (3)等离子体在主流区诱导的大尺度展向涡与在壁面附近产生的一系列拟序结构成为分离流控制的关键. 研究结果为实现真实飞机的等离子体分离流控制, 推动等离子体流动控制技术工程化应用提供了技术支撑.      

???????????????????????????о?

提出该结构体系在水平载荷作用下,可视为夹层复合构件,并提出了计算模型. 根据 变形协调原理对其进行受力分析,建立了多层多跨密肋复合墙体结构横向位移及各组成构件承 受剪力和弯矩表达式. 通过计算分析指出,各组件剪力分配只与各组件刚度及宽度比有关, 内墙板上部分配剪力大于下部,边框反之;各组件局部弯矩系数随$\lambda $的增加而减小,其整体工作性能增强,当$\lambda $增加到一定数值时,其工作性能与悬壁构件类似.     

相似电路耦合模型及其在压电—梁结构分析中的应用

根据线性系统微分方程的相拟性确定机械系统的相似电路,由压电材料的本构和动力方法确定压电材料作为电耦合的变压器,从而用一具耦合的电路系统模拟智能结构的电学和力学行为,通过一个压电－梁智能结构的分析,证明了模型的可用性。     

Electro-elastic analysis of fiber-reinforced multilayered cylindrical composites with integrated piezoelectric actuators

Based on the electro-mechanical coupling theory and the laminate elasticity theory, an electro-elastic solution is obtained for the fiber-reinforced cylindrical composites with integrated piezoelectric actuators when subjected to mechanical and electrical loadings. The hybrid composite is composed of three parts: internal piezoelectric actuator, fiber-reinforced laminated interlayer, and external piezoelectric actuator. The general solution in each piezoelectric smart layer is obtained by introducing three undetermined constants, and the general solutions in the fiber-reinforced laminated interlayer are obtained by means of the state-space method. The mechanical behaviors of the hybrid fiber-reinforced cylindrical composites are investigated. The illustrative examples show that the fiber’s angle, the stacking sequence as well as the applied electric loading strongly affect the physical fields in the fiber-reinforced multilayered cylindrical composites.     

电磁力控制的主动减振实验

用传递函数法对受随机激励的结构作主动减振设计时所获得的反馈,本文以电磁激振器作为控制器进行主动减振实验,试验在受低频正弦和宽带随机两种激励的四自由度汽车模型上进行。结果表明,电磁激振器作为控制器具有很小的机械滞后特性,适用于作低频、宽带的随机振动主动减振,减振效果达到80%以上。     

????????????????????????????????

推导出综合考虑混凝土塑性性能及混凝土与钢筋界面裂 隙等因素的混凝土保护层锈胀开裂时钢筋锈蚀率的计算公式，验证了计算公式的可行性，探 讨了影响混凝土保护层锈胀开裂时钢筋锈蚀率的相关因素，可用于钢筋混凝土结构耐久性评 估及寿命预测.     

Single-frequency vibrations and vibrational heating of a piezoelectric circular sandwich plate under monoharmonic electromechanical loading

The forced monoharmonic bending vibrations and dissipative heating of a piezoelectric circular sandwich plate under monoharmonic mechanical and electrical loading are studied. The core layer is passive and viscoelastic. The face layers (actuators) are piezoelectric and oppositely polarized over the thickness. The plate is subjected to harmonic pressure and electrical potential. The viscoelastic behavior of the materials is described by complex moduli dependent on the temperature of heating. The coupled nonlinear problem is solved numerically. A numerical analysis demonstrates that the natural frequency, amplitude of vibrations, mechanical stresses, and temperature of dissipative heating can be controlled by changing the area and thickness of the actuator. It is shown that the temperature dependence of the complex moduli do not affect the electric potential applied to the actuator to compensate for the mechanical stress __________ Translated from Prikladnaya Mekhanika, Vol. 44, No. 1, pp. 79–89, January 2008.     

THE SURFACE EFFECT ON THE TENSILE STRENGTH OF MICROMACHINED POLYSILICON FILMS FOR MEMS

In order to accomplish reliable mechanical design of MEMS, the influences of surface roughness and octadecyltrichlorosilane (OTS) self-assembled monolayers (SAMs) on the mechanical properties of micromachined polysilicon films for MEMS are investigated. Surface effect on the fracture properties of micromachined polysilicon films is evaluated with a new microtensile testing method using a magnet-coil force actuator. Statistical analysis of the surface roughness effects on the tensile strength predicated the surface roughness characterization of polysilicon films being tested and the direct relation of the mechanical properties with the surface roughness features. The fracture strength decreases with the increase of the surface roughness. The octadecyltrichlorosilane self-assembled monolayers coating leads to an increase of the average fracture strength up to 32.46%. Surface roughness and the hydrophobic properties of specimen when coated with OTS films are the two main factors influencing the tensile strength of micromachined polysilicon films for MEMS.     

Control of mechanical deformation of a laminate by piezoelectric actuator taking into account the transverse shear

Summary The control of dynamic deformation of a laminate plate is conducted by applying electrical load to a piezoelectric actuator integrated into the laminate. The dynamic behavior of the laminate is analyzed in the paper taking into account the effect of transverse shear. The analytical model of the laminate is composed of fiber-reinforced laminae and piezoelectric layers constituting a symmetric cross-ply laminate rectangular plate with simply-supported egdes. It is subjected to mechanical and electrical loads acting on the piezoelectric actuator in order to compensate the effect of the mechanical loads. The behavior of the laminate is analyzed based on the first-order shear deformation theory. Closed-form solutions are obtained for the following quantities: (1) natural frequencies of the laminate plate, (2) weight functions for the deflections and rotations and (3) transient deflections due to loads varying arbitrarily with time. Illustrative examples are shown for the control of deflections caused by the mechanical loads by means of electrical voltage applied to the piezoelectric actuators.     

串列风力机尾流干扰的研究简

广义致动盘方法是通过引入体积力代替叶片的致动盘技术与三维Navier-Stokes 方程相结合来获得风力机周围流场信息的一种方法. 该方法避免了花费大量网格与计算资源去求解风力机叶片的附面层,从而可以把更多的网格与计算资源用于风力机尾流流场的模拟,非常适合用于风力机尾流流场的研究. 以NH1500风力机为计算模型,将常规CFD (computational fluid dynamics) 方法与广义致动盘方法计算所得的叶片载荷分布进行比较,以验证广义致动盘方法的可行性. 然后使用广义致动盘方法对风场中串列风力机进行数值模拟,研究串列风力机之间间距变化时,上游风力机产生的尾流对下游风力机的干扰影响.     

Analysis of Beams with Piezoelectric Actuators

ＩｎｔｒｏｄｕｃｔｉｏｎＤｕｅｔｏｔｈｅｅｘｔｅｎｓｉｖｅａｐｐｌｉｃａｔｉｏｎｓｏｆｐｉｅｚｏｅｌｅｃｔｒｉｃｍａｔｅｒｉａｌｓｉｎｓｍａｒｔｓｔｒｕｃｔｕｒｅｓ,ｉｔｉｓｖｅｒｙｉｍｐｏｒｔａｎｔｔｏｐｒｏｂｅｉｎｔｏｔｈｅｉｒｍｅｃｈａｎｉｓｍａｓａｃｔｕａｔｏｒｓａｎｄｓｅｎｓｏｒｓ[1].Ｏｎｅｏｆｔｈｅｆｉｒｓｔｉｍｐｏｒｔａｎｔｓｔｕｄｉｅｓｉｎｖｏｌｖｉｎｇｔｈｅｍｏｄｅｌｉｎｇｏｆｔｈｅｐｅｒｆｏｒｍａｎｃｅｏｆｐｉｅｚｏｅｌｅｃｔｒｉｃａｃｔｕａｔｏｒｓｗｈｉｃｈａｒｅｓｕｒｆａ…