Development of the Viscous Plane Damper Applicable in Limited Space within Structures Subjected to Dynamic Loads

Shipping impact and wave loads impose dynamic loads on jetties and platforms in the sea, which cause the vibration of structures. Recently, many advanced viscous damper devices have been developed for implementation in structures to diminish structural vibration due to earthquakes or wind. However,...

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Published in:Applied Sciences (Switzerland)
Main Author: Bin Mohd Ali M.R.; Hejazi F.
Format: Article
Language:English
Published: Multidisciplinary Digital Publishing Institute (MDPI) 2024
Online Access:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85206585684&doi=10.3390%2fapp14199029&partnerID=40&md5=c28a30c526986254043291be78c342a0
id 2-s2.0-85206585684
spelling 2-s2.0-85206585684
Bin Mohd Ali M.R.; Hejazi F.
Development of the Viscous Plane Damper Applicable in Limited Space within Structures Subjected to Dynamic Loads
2024
Applied Sciences (Switzerland)
14
19
10.3390/app14199029
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85206585684&doi=10.3390%2fapp14199029&partnerID=40&md5=c28a30c526986254043291be78c342a0
Shipping impact and wave loads impose dynamic loads on jetties and platforms in the sea, which cause the vibration of structures. Recently, many advanced viscous damper devices have been developed for implementation in structures to diminish structural vibration due to earthquakes or wind. However, the longitudinal configuration of conventional viscous damper devices requires adequate space to locate the damper device within the frame structure, which limits the application of viscous dampers for use in jetties or platforms to dissipate the vibrations imposed by ship impact or wave force. For this reason, in this study, an attempt has been made to develop a new viscous plane damper device applicable in limited space positions where the longitudinal damper device is not able to fit. For this purpose, the initial design for the viscous plane damper device is proposed, and the prototype of the device is manufactured. Then, the performance of the fabricated viscous plane damper is examined through experimental tests by applying cyclic loads using a dynamic actuator. In order to investigate the effect of the diameter and configuration of the piston’s orifices, five different diameters for the orifices of 1, 2, 5, 8, and 10 mm are included, and three different distribution configurations of the orifices in the piston plate as Configurations A, B, and C are manufactured and tested experimentally. The lab testing is conducted by applying cyclic loads with different frequencies to evaluate the performance of the developed plane damper device under various load velocities. Accordingly, the dynamic performance of the damper device, including the damping force, effective damping and stiffness and the energy dissipation capacity obtained from the hysteresis response (force–displacement result), is investigated. The results of the experimental tests prove the functionality of the developed device to generate the desired damping force and vibration energy dissipation during applied cyclic loads. Therefore, the new plane damper device can be implemented in any structure to dissipate the effect of imposed vibration. © 2024 by the authors.
Multidisciplinary Digital Publishing Institute (MDPI)
20763417
English
Article
All Open Access; Gold Open Access
author Bin Mohd Ali M.R.; Hejazi F.
spellingShingle Bin Mohd Ali M.R.; Hejazi F.
Development of the Viscous Plane Damper Applicable in Limited Space within Structures Subjected to Dynamic Loads
author_facet Bin Mohd Ali M.R.; Hejazi F.
author_sort Bin Mohd Ali M.R.; Hejazi F.
title Development of the Viscous Plane Damper Applicable in Limited Space within Structures Subjected to Dynamic Loads
title_short Development of the Viscous Plane Damper Applicable in Limited Space within Structures Subjected to Dynamic Loads
title_full Development of the Viscous Plane Damper Applicable in Limited Space within Structures Subjected to Dynamic Loads
title_fullStr Development of the Viscous Plane Damper Applicable in Limited Space within Structures Subjected to Dynamic Loads
title_full_unstemmed Development of the Viscous Plane Damper Applicable in Limited Space within Structures Subjected to Dynamic Loads
title_sort Development of the Viscous Plane Damper Applicable in Limited Space within Structures Subjected to Dynamic Loads
publishDate 2024
container_title Applied Sciences (Switzerland)
container_volume 14
container_issue 19
doi_str_mv 10.3390/app14199029
url https://www.scopus.com/inward/record.uri?eid=2-s2.0-85206585684&doi=10.3390%2fapp14199029&partnerID=40&md5=c28a30c526986254043291be78c342a0
description Shipping impact and wave loads impose dynamic loads on jetties and platforms in the sea, which cause the vibration of structures. Recently, many advanced viscous damper devices have been developed for implementation in structures to diminish structural vibration due to earthquakes or wind. However, the longitudinal configuration of conventional viscous damper devices requires adequate space to locate the damper device within the frame structure, which limits the application of viscous dampers for use in jetties or platforms to dissipate the vibrations imposed by ship impact or wave force. For this reason, in this study, an attempt has been made to develop a new viscous plane damper device applicable in limited space positions where the longitudinal damper device is not able to fit. For this purpose, the initial design for the viscous plane damper device is proposed, and the prototype of the device is manufactured. Then, the performance of the fabricated viscous plane damper is examined through experimental tests by applying cyclic loads using a dynamic actuator. In order to investigate the effect of the diameter and configuration of the piston’s orifices, five different diameters for the orifices of 1, 2, 5, 8, and 10 mm are included, and three different distribution configurations of the orifices in the piston plate as Configurations A, B, and C are manufactured and tested experimentally. The lab testing is conducted by applying cyclic loads with different frequencies to evaluate the performance of the developed plane damper device under various load velocities. Accordingly, the dynamic performance of the damper device, including the damping force, effective damping and stiffness and the energy dissipation capacity obtained from the hysteresis response (force–displacement result), is investigated. The results of the experimental tests prove the functionality of the developed device to generate the desired damping force and vibration energy dissipation during applied cyclic loads. Therefore, the new plane damper device can be implemented in any structure to dissipate the effect of imposed vibration. © 2024 by the authors.
publisher Multidisciplinary Digital Publishing Institute (MDPI)
issn 20763417
language English
format Article
accesstype All Open Access; Gold Open Access
record_format scopus
collection Scopus
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