A broadband variable fluid damper with frequency selective valves for spacecraft micro-vibration isolation

In order to improve the vibration isolation performance of current three-parameter damper using bellow and fluid damping, a concept of fluid damper with variable damping and secondary variable stiffness was proposed, a prototype has been designed with several frequency selective valves to adjust the damping characteristics at specific frequency bands, especially that in the low-frequency range. Followed mathematical modelling and simulation of the damper have been carried out, the results show that the designed damper has obtained excellent damping characteristics both in the high- and low-frequency ranges, the micro-vibration isolation efficiency of the damper under realistic excitation of a Control Moment Gyroscope used in a manned spacecraft reaches a significant 71.03 %.The proposed damper concept and designed prototype have laid the foundation for further testing and optimization of high-end isolators for modern spacecrafts.

Authors

Publication Details

Journal
Vibroengineering PROCEDIA
Published
2024-09-27
DOI
https://doi.org/10.21595/vp.2024.24190
Citations
1
Primary Topic
Vibration Control and Rheological Fluids
Type
article
Field-Weighted Citation Impact
0.26

Funders

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article

A broadband variable fluid damper with frequency selective valves for spacecraft micro-vibration isolation

R. J. T. Chen, Wenlin Wang, Yang Ding, Haoyu Li et al.
1 citations
Vibroengineering PROCEDIA
Vibration Control and Rheological Fluids
0.26
article

A broadband variable fluid damper with frequency selective valves for spacecraft micro-vibration isolation

R. J. T. Chen, Wenlin Wang, Yang Ding, Haoyu Li, Yong Liu
article en
1 citations

Abstract

In order to improve the vibration isolation performance of current three-parameter damper using bellow and fluid damping, a concept of fluid damper with variable damping and secondary variable stiffness was proposed, a prototype has been designed with several frequency selective valves to adjust the damping characteristics at specific frequency bands, especially that in the low-frequency range. Followed mathematical modelling and simulation of the damper have been carried out, the results show that the designed damper has obtained excellent damping characteristics both in the high- and low-frequency ranges, the micro-vibration isolation efficiency of the damper under realistic excitation of a Control Moment Gyroscope used in a manned spacecraft reaches a significant 71.03 %.The proposed damper concept and designed prototype have laid the foundation for further testing and optimization of high-end isolators for modern spacecrafts.

Vibroengineering PROCEDIAVol. 55
National Natural Science Foundation of China
Openalex Percentile: Top 45%
Vibration Control and Rheological Fluids
0.26
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