Vibration and Damping Analysis of Pipeline System Based on Partially Piezoelectric Active Constrained Layer Damping Treatment

Zhang, Yuanlin; Li, Xuefeng; Rong, Weichong; Gao, Peixin; Yu, Tao; Han, Hao; Xu, Langjun

doi:10.3390/ma14051209

Cited by 17 publications

(6 citation statements)

References 30 publications

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“…The constrained layer damping consists of a viscoelastic layer sandwiched between the base structure and an elastic constraining layer. The CLD treatment was proposed by Kerwin et al (Kerwin, 1959), and has been applied to outlet guide vanes, (Tomlinson, 1990) aircraft panels, (Zhang et al, 2021a) pipelines (Zhang et al, 2021c) and bridges (Liu et al, 2020) for the purpose of developing vibration control systems. Compared to the traditional PTMD, CLD-PTMD aims to quickly suppress the slight vibration of the structure and reduce the excessive pounding force.…”

Section: Introductionmentioning

confidence: 99%

Pounding tuned mass damper with constrained layer damping

Duan

Huo

2023

Advances in Structural Engineering

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The pounding tuned mass damper (PTMD), which is a passive vibration control device, has attracted much attention in recent years. However, due to the absence of additional dampers in traditional PTMD, the free vibration of structures cannot always be suppressed quickly. Another limitation for the traditional PTMD is that the primary structure is subjected to a large pounding force that may cause local damage and fatigue. To address these limitations, this paper proposes a novel PTMD with constrained layer damping (CLD-PTMD) by attaching a damping layer and the constraining layer to the surface of the stiffness element of the PTMD to provide more damping. In the experiment, the influence that the different configuration parameters have on the damping performance of CLD is examined. A shake table test is conducted to investigate the energy dissipation of a CLD-PTMD subjected to harmonic excitation. The FEM model of the CLD beam is established to determine the damping ratio and analyze more parameters. The CLD-PTMD is used for the vibration control of a simulated SDOF structure. The results demonstrate that compared with the traditional PTMD, CLD dissipates more energy than the pounding process. In addition, CLD-PTMD has a lower pounding force and pounding energy than PTMD in free and forced vibration. The free vibration with CLD-PTMD can be suppressed faster. The robustness of CLD-PTMD is better and the control performance of CLD-PTMD is more stable than traditional PTMD.

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Section: Introductionmentioning

confidence: 99%

Pounding tuned mass damper with constrained layer damping

Duan

Huo

2023

Advances in Structural Engineering

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“…Considerable research regarding the FSI nonlinear dynamics characteristics of aircraft hydraulic pipes has been reported in the past years [1][2][3][4][5][6][7][8][9][10][11][12]. The precondition for analyzing these dynamic behaviors was to establish an accurate mathematical model.…”

Section: Introductionmentioning

confidence: 99%

Frequency Domain Analysis of Fluid–Structure Interaction in Aircraft Hydraulic Pipe with Complex Constraints

et al. 2022

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This paper focuses on the frequency domain fluid–structure interaction (FSI) vibration characteristics of aircraft hydraulic pipe with complex constraints. The linear partial differential fourteen-equation model is applied to describe the nonlinear FSI dynamics of pipes conveying fluid with high-speed, high-pressure, a wide Reynolds number, and the vibration frequency range. The excitation, complex boundary, and middle constraint models of liquid-filled pipes are analytically established and added into the global model of the pipe system. These resulting models are solved by the improved Laplace transform transfer matrix method (LTTMM) in the frequency domain. Then, the dynamic response characteristics of an aircraft hydraulic pipe containing diverse constraints are investigated numerically and experimentally under four types of working conditions, and the improvement conditions for the numerical instabilities are presented. In general, the present method is highly efficient and convenient for rapid model parameter modifications, in order to be fully applicable to different pipe systems and analysis cases. The results reveal the complex resonant laws regarding aircraft hydraulic pipes with complex constraints in the broad frequency band, which can also provide theoretical reference and technical support for FSI vibration analysis and the control of aircraft hydraulic pipes.

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“…Furthermore, the studies about vibration reduction of pipeline systems have also been performed in recent years, and the vibration reduction methods include damping coatings (Gao et al, 2018;Yano et al, 2019), tuned mass (dynamic vibration reduction) (Zhang et al, 2019a(Zhang et al, , 2019bTan et al, 2019), piezoelectric and electromagnetic (Zhai et al, 2019;Zhang et al, 2021), etc. In addition to the above measures, researchers have also widely adopted the adjustment of the hoops layout to control excessive vibration of the pipeline system, which is considered to be the most convenient and economical method to reduce the vibration response of a pipeline system at the design stage.…”

Section: Introductionmentioning

confidence: 99%

Vibration response analysis and hoop layout optimization of spatial pipeline under random excitation

Wang

Sun

Gao

et al. 2022

AEAT

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Purpose In many cases, the external pipelines of aero-engine are subjected to random excitation. The purpose of this paper is to reduce the vibration response of the pipeline system effectively by adjusting the hoop layout. Design/methodology/approach In this paper, a spatial pipeline supported by multi-hoops is taken as the object, the methods of solution of the vibration response of the pipeline system by using pseudo excitation and hoop layouts optimization with amplitude reduction of vibration response as the goal are presented. First, the finite element model of the spatial pipeline system is presented. Then, an optimization model spatial pipeline is established. Finally, a case study is carried out to prove the rationality of the random vibration response analysis of the pipeline system. Furthermore, the proposed optimization model and genetic algorithm are applied to optimize the hoop layout. Findings The results show that the maximum response variance after optimization is reduced by 32.8%, which proves the rationality of the developed hoop layout optimization method. Originality/value The pseudo excitation method is used to solve the vibration response of aero-engine pipeline system, and the optimization of the hoop layout for aero-engine spatial pipelines under random excitation to reduce random vibration response is studied systematically.

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Vibration and Damping Analysis of Pipeline System Based on Partially Piezoelectric Active Constrained Layer Damping Treatment

Cited by 17 publications

References 30 publications

Pounding tuned mass damper with constrained layer damping

Pounding tuned mass damper with constrained layer damping

Frequency Domain Analysis of Fluid–Structure Interaction in Aircraft Hydraulic Pipe with Complex Constraints

Vibration response analysis and hoop layout optimization of spatial pipeline under random excitation

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