共查询到20条相似文献,搜索用时 31 毫秒
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周期性机械振动主动控制算法 总被引:1,自引:0,他引:1
为提高周期性机械装置的隔振性能,减少其对底座(或地面)及周围环境的影响,采用由弹性橡胶和压电堆作动器组成的主动悬置(active control mount, ACM).针对压电堆作动器输出位移较小的情况,设计液压位移放大机构.通过对压电作动器和橡胶主簧性能的分析,建立由主动悬置构成的隔振系统的力学模型.周期性机械振动系统,其周期振动信号可用作控制同步信号,因此控制系统采用基于同步滤波-X LMS(least mean square)算法的自适应控制策略,传递到机座的残余力作为误差信号,实现对周期性机械振动系统的主动控制.计算机仿真实验结果表明,采用这种主动悬置和同步滤波-X LMS算法的主动控制系统,相对于采用普通橡胶悬置的被动系统,明显减少了对底座的力传递,减振效果明显. 相似文献
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理想的发动机悬架系统应隔离发动机工作转速范围内由发动机干扰力所引起的发动机振动,并阻止由冲击而激起的发动机弹跳,这意味着发动机悬架的动态刚度和阻尼是与频率和振幅有关的,改善依赖于频率和振幅特性的动态刚度与阻尼是发动机悬架系统发展的关键所在。传统的弹性悬架不能满足所有的要求,它仅能在静偏转和隔振之间进行折衷,特别在低频域,被动的液压悬架能比弹性悬架提供更好的特性,通常半主动技术,由于其可调性而被用来进一步改善液压悬架的特性,为了隔振、低频时主动发动机悬架系统非常硬,而在高频域内被调整的非常软,主动的发动机悬架已被认为是发动机悬架的新一代,发动机悬架系统的优化是相当可取的,但发动机悬架的优化工作出现一些局限性,文中综述国内,外发动机悬架技术的现状与进展。 相似文献
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同轴式微速差双转子系统整机动平衡方法研究 总被引:5,自引:0,他引:5
同轴式微速差双转子系统的不平衡振动信号是由内、外转子各自不平衡振动叠加而成的拍振,通过研究拍振波形的特征,提出不通过解拍,有效分离内、外转子各自不平衡振动响应的方法;通过理论分析和试验研究发现内、外转子不平衡振动之间的相互影响很小,提出用8影响系数法实现该类转子动平衡的方法。通过对双转子系统进行外转子单独平衡和内、外转子同时平衡的成功实践,证明8影响系数法能在保证足够高的平衡精度下,快速、高效地解决同轴式微速差双转子系统的动平衡问题,具有十分重要的工程应用价值。 相似文献
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This paper presents a study on rotating machine vibration signals by using computed order tracking, Vold-Kalman filtering and intrinsic mode functions from the empirical mode decomposition method. Through the sequential use of intrinsic mode function and order tracking methods, both speed synchronous and non-synchronous vibrations that modulate orders in rotating machine vibrations are distinguished, which is difficult when using each of the techniques in isolation alone. Simulation and experimental studies demonstrate the ability of extracting vibrations that modulate order signals through combining the techniques. 相似文献
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研究了具有可变刚度阻尼的发动机空气弹簧液压悬置的动特性和隔振特性。针对影响发动机空气弹簧液压悬置动特性的关键参数上液室等效体积刚度,采用理论和试验方法研究了上液室等效体积刚度的等效值,基于该等效值建立了空气弹簧液压悬置的理论模型,对空气腔开闭两种工况进行了空气弹簧液压悬置动特性的仿真和试验研究。搭建了发动机空气弹簧液压悬置系统试验台架,研究了台架各种激励频率下的空气弹簧液压悬置的隔振特性。结果表明:本研究采用的上液室等效体积刚度进行空气弹簧进行建模是正确、可行的,提高了空气弹簧建模效率和准确性;空气弹簧液压悬置在空气腔开启和关闭两种状态下,峰值动刚度增大幅值达78.5%,峰值阻尼角增大幅值达250%。台架试验表明:当台架激励频率小于25Hz时,悬置采用大刚度大阻尼;当台架激励频率大于等于25 Hz时,悬置采用小刚度小阻尼;悬置隔振率提升明显,不同频率下提升幅值达10%~67%。 相似文献
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ZHANG Yunxia ZHANG Jianwu SHANGGUAN Wenbin FENG Qishan 《机械工程学报(英文版)》2008,21(3):31-35
To investigate the dynamic characteristics and damping theory of the passive hydraulic engine mount (PHEM), numerical prediction is performed through lumped parameter model. System parameters, including volume compliance of the decoupler chamber, effective piston area, fluid inertia and resistance of inertia track and direct-decoupler, are identified by means of experiments and finite element method (FEM). Dynamic behaviors are tested with elastomer test system for purpose of validating PHEM. With incorporation of inertia track and direct-decoupler, PHEM behaves effective and efficient vibration isolation in range of both low and high frequencies. The comparison of the numerical results with the experimental observations shows that the present PHEM achieves fairly good performance for the engine vibration isolation. 相似文献
7.
基于瑞利法的内燃机曲轴扭纵耦合振动 总被引:2,自引:1,他引:2
采用瑞利法对高速内燃机曲轴扭纵耦合振动进行了研究。将内燃机曲轴等效为连续分布阶梯轴模型,根据当量轴段以及集中质量的动能和势能关系,通过拉格朗日方程分别建立轴系扭振模型和纵振模型。根据刚度耦合原理,并考虑轴系强迫激励进而建立了扭纵耦合强迫振动模型。采用谐次分析法对模型求解后,通过与采用三维振动测量装置对某直列四缸柴油机曲轴自由端的振动信号进行实际测量所得到的结果进行比较,可以发现,扭振和纵振与实际测量的结果在各主要谐次都保持相当的一致。 相似文献
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G. F. Safina 《Russian Journal of Nondestructive Testing》2011,47(3):189-201
Investigations of the direct and inverse spectral problems of torsional vibrations of a shaft with disks were performed. The
Tolle method was used to solve the direct problem. The influence of the characteristics of a shaft with loads on the frequencies
of its torsional vibrations was studied using the solution of the direct problem. It was shown that an increase in the moments
of inertia of disk masses leads to a decrease in vibration frequencies and that an increase in the torsional rigidity of segments
of a shaft leads to an increase in the system’s vibration frequencies. Examples, tables, and plots of the corresponding dependences
are presented. 相似文献
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Ramin M.H. Khorasany Stanley G. Hutton 《International Journal of Mechanical Sciences》2012,54(1):1-11
A central aspect of the linear vibration theory of rotating disks involves the concept of critical speeds. At such rotation speeds an axisymmetric disk can support a standing wave as recorded by a stationary observer. In such situations an applied space fixed constant force can give rise to a resonance in the disk. Such a response is of concern in industrial applications as diverse as circular saw blades and computer floppy disks. In such situations the magnitude of response may exceed the limits of linear theory. The present paper is concerned with the effects of large displacements upon the disk response in the neighborhood of such critical speeds. The effects of geometric nonlinearities and the influence of rigid body tilting and translation (caused by the boundary conditions) are considered. The equations of motion are based on Von Karman plate theory. The eigenfunctions of two self-adjoint eigenvalue problems, corresponding to the stress function and the transverse displacement, are determined and used as approximation functions in a numerically efficient Galerkin formulation. The coupled nonlinear ordinary differential equations of motion are solved using the Runge–Kutta method. Numerical results are presented for disks that are free to translate and rotate at their inner boundary and are constrained from lateral motion by space fixed linear springs. The effects of vibration magnitude on system response in the sub and super-critical speed regions are computed and the effects of large displacements on critical speed behavior and forced response are investigated. Experiments are conducted to verify the accuracy of the numerical results obtained in this paper. 相似文献
11.
叶片的振动及其导致的高周疲劳断裂问题是当前高性能透平机械研发与运行中面临的主要问题,高负荷叶片的流动参数在尾迹的干扰下发生周期性脉动造成高倍频振动是造成高周疲劳的主要因素,因此叶片高倍频振动的监测对高周疲劳的诊断预警具有重要意义。提出了基于虚拟传感器内插法的旋转态叶片高倍频信号重构及辨识方法,可实现高倍频的求解。在传感器安装夹角为6°的情况下可实现高达60倍频以内的振动辨识,理论上只需2支传感器即可进行倍频的识别,实际应用中采用4支传感器即可保证辨识精度,且只需一次启车或停车就可实现叶片振动频率的识别,简化了测试步骤。所提出的辨识方法可应用于航空发动机等静叶片数量较多、振动形式为高阶次高倍频的高端旋转机械的振动监测识别,模拟仿真和试验结果验证了该方法的有效性及准确性。 相似文献
12.
Achieving very restricted noise, vibration and harshness targets in modern vehicles, makes using the hydraulic engine mount crucial. Hydraulic engine mounts have both solid and fluid media in their structures that make their dynamic behavior complex to figure out. We present a three-dimensional model of HEM with using finite element method that encompasses elastomeric material’s nonlinearity and fluid-structure-interaction. Dynamic equivalent modulus of elasticity for elastomeric material is identified through iterative model updating procedure. To do model updating, the results (here, namely, natural frequencies and frequency response function graphs) are compared with real hydraulic engine mount behavior that derived from modal tests. The results showed that the dynamic characteristic of elastomeric material is frequency dependent and can be divided into two distinct regions: below 30 Hz (low frequency) and above 30 Hz (high frequency) with different trends. 相似文献
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Jin Ho Lee Hyo Young Kim Ki Hyun Kim Myeong Hyeon Kim Seok Woo Lee 《Journal of Mechanical Science and Technology》2017,31(12):5711-5719
Precision vibration control is a major issue in nanotechnology. In particular, nano-precision measurement systems such as Atomic force microscopes (AFM) and Scanning probe microscopes (SPM) are sensitive to ground vibrations. The amplitude of a ground vibration is typically sub-micrometer and ground vibrations adversely affect both the precision and accuracy of these measuring equipment. Consequently, hybrid active-passive vibration isolation systems are typically used as they reduce ground vibrations. This paper presents a hybrid vibration isolation system composed of four spiral metal springs for passive isolation and eight voice coil motors for active isolation. H-infinite and Proportional–integral–derivative (PID) controllers are applied to its 6-DOF vibration control system using six velocity sensors to measure system vibrations. The transmissibility of the presented hybrid isolation system is in the range -10 to -48 dB at its passive resonance frequency and is at least -4 dB better than hybrid isolation systems employing acceleration sensors. The results of various tests conducted to verify the control performance of the developed system with a separately developed shaker indicate that it can serve as a bench-top device for precision measurement machines. 相似文献
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Vedang Chauhan Brian Surgenor 《The International Journal of Advanced Manufacturing Technology》2017,89(9-12):2491-2501
The geometry of rotary aircraft engine components is usually defined by thin mechanical elements and complex surfaces that are only achievable by 5-axis machining due to either limited access or the design itself. Such thin-walled characteristics make these components susceptible to vibrations while machining and usually require careful manipulation of the toolpath parameters to minimize cutting forces and vibration. Moreover, the tool suppliers’ approach leans towards the feature-build design of cutter geometry to increase the productivity and quality of a machined surface. Some examples of those recent improvements for rotary aircraft engine components are barrel-shaped tools that attempt to increase the contact radius on the tool-part interface to minimize step-over while conserving the scallop height to meet roughness tolerances. This research aims to fill a gap in the current literature by proposing a stability model for barrel-shaped tools. Stability contour maps make use of a mechanistic dynamic force model for barrel-shaped tools. The force model is also capable of including tool runout and orientation angles, tilt and lead, as named in most CAM software. By simulating dynamic forces on the time domain, a contour map is presented to address unstable vibrations. Since forced vibrations and surface location error (SLE) may also appear when milling aircraft parts, SLE and surface roughness are also determined. Finally, given the complexity and number of parameters, validation of the stability maps is performed through experimental chatter tests using a thin wall component. 相似文献
19.
A. Ghorbanpour Arani A. Loghman A. R. Shajari S. Amir 《Journal of Mechanical Science and Technology》2010,24(10):2107-2118
In this paper, a semi-analytical solution for magneto-thermo-elastic problem in functionally graded (FG) hollow rotating disks
with variable thickness placed in uniform magnetic and thermal fields is presented. Stresses and perturbation of magnetic
field vector in FG rotating disks are determined using infinitesimal theory of magneto-thermo-elasticity under plane stress
conditions. The material properties except Poisson’s ratio are modeled as power-law distribution of volume fraction. The profile
of disk thickness is assumed to be a parabolic function of radius. The non-dimensional distribution of temperature, displacement,
stresses and perturbation of magnetic field vector throughout radius are shown. Effects of material grading index, geometry
of the disk and magnetic field on the stress and displacement fields are investigated. The results of stresses and radial
displacements for two different boundary conditions with and without the effect of magnetic field are compared for a FG rotating
disk with concave thickness profile. It has been found that imposing a magnetic field significantly decreases tensile circumferential
stresses. Therefore the fatigue life of the disk will be significantly improved by applying the magnetic field. Results of
this investigation could be applied for optimum design of FG hollow rotating disks with variable thickness. 相似文献
20.
The stability of active balancing control using influence coefficients for a variable rotor system 总被引:2,自引:0,他引:2
Jong-Soo Kim Soo-Hun Lee 《The International Journal of Advanced Manufacturing Technology》2003,22(7-8):562-567
High-speed rotating machines can be very sensitive to rotating mass unbalance that is a major source of harmful vibration for many types of rotating machinery. A balancing procedure is therefore needed for all high-speed rotating systems. To save the time and cost of off-line balancing, many researchers have developed on-line balancing devices and methods. In this paper, an active balancing device, which is of an electro-magnetic type, has been developed and an active balancing method using the influence coefficient method is proposed. The stability of active balancing control is studied in this paper. A stable condition for active balancing control is derived by estimating the errors of influencing coefficients. A gain scheduling control using influence coefficients of the standard model is proposed when the dynamic characteristics of a rotor system are changed. The stability of the balancing method is verified by experiments. 相似文献