Vibration reduction evaluation of a linear system with a nonlinear energy sink under a harmonic and random excitation

This paper aims to investigate the property and behavior of the hysteretic nonlinear energy sink (HNES) coupled to a half vehicle system which is a nine-degree-of-freedom, nonlinear, and semiactive suspension system in order to improve the ride comfort and increase the stability in shock mitigation by using the computer simulation method. The HNES model is a semiactive suspension device, which comprises the famous Bouc–Wen (B-W) model employed to describe the force produced by both the purely hysteretic spring and linear elastic spring of potentially negative stiffness connected in parallel, for the half vehicle system. Nine nonlinear motion equations of the half vehicle system are derived in terms of the seven displacements and the two dimensionless hysteretic variables, which are integrated numerically by employing the direct time integration method for studying both the variables of vertical displacements, velocities, accelerations, chassis pitch angle, and the ride comfort and driver safety, respectively, based on the bump and random road inputs of the pseudoexcitation method as excitation signal. Simulation results show that, compared with the HNES model and the magnetorheological (MR) model coupled to the half vehicle system, the ride comfort and stability have been evidently improved. A successful validation process has been performed, which indicated that both the ride comfort and driver safety properties of the HNES model coupled to half vehicle significantly improved.

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Vibration Reduction of a Composite Plate with Inertial Nonlinear Energy Sink

Vibration Engineering for a Sustainable Future ◽

10.1007/978-3-030-48153-7_16 ◽

2021 ◽

pp. 121-128

Author(s):

Hong-Yan Chen ◽

Hu Ding ◽

Li-Qun Chen

Keyword(s):

Composite Plate ◽

Vibration Reduction ◽

Nonlinear Energy Sink ◽

Energy Sink ◽

Nonlinear Energy

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Nonlinear Energy Sink for Whole-Spacecraft Vibration Reduction

Journal of Vibration and Acoustics ◽

10.1115/1.4035377 ◽

2017 ◽

Vol 139 (2) ◽

Cited By ~ 51

Author(s):

Kai Yang ◽

Ye-Wei Zhang ◽

Hu Ding ◽

Tian-Zhi Yang ◽

Yang Li ◽

...

Keyword(s):

Finite Element ◽

Finite Element Model ◽

Natural Frequencies ◽

Vibration Reduction ◽

Nonlinear Energy Sink ◽

Element Model ◽

Equivalent Model ◽

Energy Sink ◽

The Finite Element Model ◽

Nonlinear Energy

A nonlinear energy sink (NES) approach is proposed for whole-spacecraft vibration reduction. Frequency sweeping tests are conducted on a scaled whole-spacecraft structure without or with a NES attached. The experimental transmissibility results demonstrate the significant reduction of the whole-spacecraft structure vibration over a broad spectrum of excitation frequency. The NES attachment hardly changes the natural frequencies of the structure. A finite element model is developed, and the model is verified by the experimental results. A two degrees-of-freedom (DOF) equivalent model of the scaled whole-spacecraft is proposed with the two same natural frequencies as those obtained via the finite element model. The experiment, the finite element model, and the equivalent model predict the same trends that the NES vibration reduction performance becomes better for the increasing NES mass, the increasing NES viscous damping, and the decreasing nonlinear stiffness. The energy absorption measure and the energy transition measure calculated based on the equivalent model reveals that an appropriately designed NES can efficiently absorb and dissipate broadband-frequency energy via nonlinear beats, irreversible targeted energy transfer (TET), or both for different parameters.

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Vibration Suppression for Beam-Like Repeating Lattice Structure Based on Equivalent Model by a Nonlinear Energy Sink

Mathematical Problems in Engineering ◽

10.1155/2021/6659598 ◽

2021 ◽

Vol 2021 ◽

pp. 1-15

Author(s):

Gen Liu ◽

Gongfa Chen ◽

Fangsen Cui

Keyword(s):

Vibration Suppression ◽

Lattice Structure ◽

Vibration Reduction ◽

Coupled System ◽

Nonlinear Energy Sink ◽

Equivalent Model ◽

External Excitation ◽

Suppression Effect ◽

Energy Sink ◽

Nonlinear Energy

Based on the fully deployed space beam-like truss, the vibration reduction of the lattice structure is studied by using the local NES (nonlinear energy sink) attachment in this paper. The beam-like lattice structure is modeled as an equivalent linear continuous system (a finite length beam) by the equivalent method and validated with the finite element results. The dynamic vibration equations for the equivalent cantilever beam are established and the governing equations for the equivalent beam with NES are approximated by the Galerkin method. The displacement responses of the beam with and without NES attached under shock excitation are obtained. With NES at different positions, the amplitude responses of the coupled system under the external excitation at different positions are calculated to evaluate the suppression effect of the NES attachment to the structure. And with different masses of the NES, the amplitude responses of the coupled structure subject to the external excitation at different positions are also investigated to get the influence of the mass of the NES attachment to the vibration reduction. It can be seen from the results that the NES attachment can attenuate the response of the beam-like truss under transient excitation efficiently. And with the mass of NES attachment increasing, the vibration amplitude of the coupled system declines more rapidly, and the energy consumption efficiency of the NES attachment is higher. Moreover, the attenuation effect of the NES with different masses is experimentally analyzed. The experimental results are in good accord with the theoretical calculation.

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