具有环形阻尼间隙的波纹管型流体粘性阻尼器的建模与参数化研究

IF 1.9 3区 工程技术 Q3 MECHANICS
Xiaolei Jiao, Wenbo Li, Peiji Wang
{"title":"具有环形阻尼间隙的波纹管型流体粘性阻尼器的建模与参数化研究","authors":"Xiaolei Jiao,&nbsp;Wenbo Li,&nbsp;Peiji Wang","doi":"10.1007/s11012-024-01888-x","DOIUrl":null,"url":null,"abstract":"<div><p>Micro-vibration is an important issue that affects the observation accuracy and imaging quality of spacecraft. The micro-vibration of spacecraft has the characteristics of wide frequency (1–300 Hz) and low amplitude (μm level). Installing a micro-vibration isolation device on a disturbance source or precision payload is an effective method to suppress micro-vibration. In this paper, we propose a novel modeling method for a micro-vibration isolator with annular damping gap. Firstly, by cleverly utilizing the principle of effective area of bellows, the complex bellows are simplified into a single tube. Based on the axial vibration of the bellows, springs are used to equivalent the elasticity of the bellows, and the interaction between the fluid and bellows is considered in the model. Through this method, we greatly simplify the isolator and constructed a semi-analytical model. Then, we use the fluid–structure coupling analysis to evaluate the difference in describing the volume deformation between the single tube and the bellows with different wall thicknesses, and then propose a novel solution. We introduce the bellows volume deformation correction coefficient to modify the model. The effectiveness of the correction method for isolators with different wall thicknesses is discussed. Next, we conduct parametric research to analyze the influences of different wall thicknesses, viscosity, damping gap width and length, and excitation force amplitude on the isolation performance. Through our research, it is found that this annular damping gap has better adjustability for isolation performance than the damping orifice, which may help propose more combinations of design parameters suitable for different isolation performance requirements. Our proposed model is suitable for fluid viscous damper working at the frequency of 1–300 Hz, that used for spacecraft micro-vibration suppression (including magnetorheological dampers and adjustable damping orifice fluid viscous damper).</p></div>","PeriodicalId":695,"journal":{"name":"Meccanica","volume":"59 12","pages":"2129 - 2154"},"PeriodicalIF":1.9000,"publicationDate":"2024-10-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Modeling and parametric research of a bellows-type fluid viscous damper with annular damping gap for spacecraft micro-vibration suppression\",\"authors\":\"Xiaolei Jiao,&nbsp;Wenbo Li,&nbsp;Peiji Wang\",\"doi\":\"10.1007/s11012-024-01888-x\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>Micro-vibration is an important issue that affects the observation accuracy and imaging quality of spacecraft. The micro-vibration of spacecraft has the characteristics of wide frequency (1–300 Hz) and low amplitude (μm level). Installing a micro-vibration isolation device on a disturbance source or precision payload is an effective method to suppress micro-vibration. In this paper, we propose a novel modeling method for a micro-vibration isolator with annular damping gap. Firstly, by cleverly utilizing the principle of effective area of bellows, the complex bellows are simplified into a single tube. Based on the axial vibration of the bellows, springs are used to equivalent the elasticity of the bellows, and the interaction between the fluid and bellows is considered in the model. Through this method, we greatly simplify the isolator and constructed a semi-analytical model. Then, we use the fluid–structure coupling analysis to evaluate the difference in describing the volume deformation between the single tube and the bellows with different wall thicknesses, and then propose a novel solution. We introduce the bellows volume deformation correction coefficient to modify the model. The effectiveness of the correction method for isolators with different wall thicknesses is discussed. Next, we conduct parametric research to analyze the influences of different wall thicknesses, viscosity, damping gap width and length, and excitation force amplitude on the isolation performance. Through our research, it is found that this annular damping gap has better adjustability for isolation performance than the damping orifice, which may help propose more combinations of design parameters suitable for different isolation performance requirements. Our proposed model is suitable for fluid viscous damper working at the frequency of 1–300 Hz, that used for spacecraft micro-vibration suppression (including magnetorheological dampers and adjustable damping orifice fluid viscous damper).</p></div>\",\"PeriodicalId\":695,\"journal\":{\"name\":\"Meccanica\",\"volume\":\"59 12\",\"pages\":\"2129 - 2154\"},\"PeriodicalIF\":1.9000,\"publicationDate\":\"2024-10-08\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Meccanica\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://link.springer.com/article/10.1007/s11012-024-01888-x\",\"RegionNum\":3,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"MECHANICS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Meccanica","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1007/s11012-024-01888-x","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"MECHANICS","Score":null,"Total":0}
引用次数: 0

摘要

微振动是影响航天器观测精度和成像质量的重要问题。航天器微振动具有宽频率(1 ~ 300hz)、低幅值(μm级)的特点。在干扰源或精密载荷上安装微振动隔离装置是抑制微振动的有效方法。本文提出了一种新的环形阻尼间隙微隔振器的建模方法。首先,巧妙地利用波纹管有效面积原理,将复杂的波纹管简化为单管。基于波纹管的轴向振动,采用弹簧等效波纹管的弹性,并考虑流体与波纹管的相互作用。通过这种方法,我们大大简化了隔离器,并建立了半解析模型。在此基础上,利用流固耦合分析方法分析了不同壁厚的波纹管与单管体积变形的差异,并提出了一种新的求解方法。引入波纹管体积变形修正系数对模型进行修正。讨论了不同壁厚隔离器校正方法的有效性。接下来,我们进行了参数化研究,分析了不同壁厚、粘度、阻尼间隙宽度和长度以及激励力幅值对隔振性能的影响。通过研究发现,环形阻尼间隙对隔震性能的可调性优于阻尼孔,这有助于提出更多适合不同隔震性能要求的设计参数组合。该模型适用于工作频率为1 ~ 300 Hz的航天器微振动抑制用流体粘性阻尼器(包括磁流变阻尼器和可调阻尼孔型流体粘性阻尼器)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modeling and parametric research of a bellows-type fluid viscous damper with annular damping gap for spacecraft micro-vibration suppression

Micro-vibration is an important issue that affects the observation accuracy and imaging quality of spacecraft. The micro-vibration of spacecraft has the characteristics of wide frequency (1–300 Hz) and low amplitude (μm level). Installing a micro-vibration isolation device on a disturbance source or precision payload is an effective method to suppress micro-vibration. In this paper, we propose a novel modeling method for a micro-vibration isolator with annular damping gap. Firstly, by cleverly utilizing the principle of effective area of bellows, the complex bellows are simplified into a single tube. Based on the axial vibration of the bellows, springs are used to equivalent the elasticity of the bellows, and the interaction between the fluid and bellows is considered in the model. Through this method, we greatly simplify the isolator and constructed a semi-analytical model. Then, we use the fluid–structure coupling analysis to evaluate the difference in describing the volume deformation between the single tube and the bellows with different wall thicknesses, and then propose a novel solution. We introduce the bellows volume deformation correction coefficient to modify the model. The effectiveness of the correction method for isolators with different wall thicknesses is discussed. Next, we conduct parametric research to analyze the influences of different wall thicknesses, viscosity, damping gap width and length, and excitation force amplitude on the isolation performance. Through our research, it is found that this annular damping gap has better adjustability for isolation performance than the damping orifice, which may help propose more combinations of design parameters suitable for different isolation performance requirements. Our proposed model is suitable for fluid viscous damper working at the frequency of 1–300 Hz, that used for spacecraft micro-vibration suppression (including magnetorheological dampers and adjustable damping orifice fluid viscous damper).

求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
Meccanica
Meccanica 物理-力学
CiteScore
4.70
自引率
3.70%
发文量
151
审稿时长
7 months
期刊介绍: Meccanica focuses on the methodological framework shared by mechanical scientists when addressing theoretical or applied problems. Original papers address various aspects of mechanical and mathematical modeling, of solution, as well as of analysis of system behavior. The journal explores fundamental and applications issues in established areas of mechanics research as well as in emerging fields; contemporary research on general mechanics, solid and structural mechanics, fluid mechanics, and mechanics of machines; interdisciplinary fields between mechanics and other mathematical and engineering sciences; interaction of mechanics with dynamical systems, advanced materials, control and computation; electromechanics; biomechanics. Articles include full length papers; topical overviews; brief notes; discussions and comments on published papers; book reviews; and an international calendar of conferences. Meccanica, the official journal of the Italian Association of Theoretical and Applied Mechanics, was established in 1966.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信