Theoretical and experimental study on the self-excited vibration of a flexible rotor system with floating spline

IF 5.3 1区 工程技术 Q1 ENGINEERING, AEROSPACE Chinese Journal of Aeronautics Pub Date : 2023-12-01 DOI:10.1016/j.cja.2023.03.030
Haimin ZHU , Li ZHANG , Qingzhang CHEN , Miaomiao LI , Dan WANG , Jia YAO , Rupeng ZHU
{"title":"Theoretical and experimental study on the self-excited vibration of a flexible rotor system with floating spline","authors":"Haimin ZHU ,&nbsp;Li ZHANG ,&nbsp;Qingzhang CHEN ,&nbsp;Miaomiao LI ,&nbsp;Dan WANG ,&nbsp;Jia YAO ,&nbsp;Rupeng ZHU","doi":"10.1016/j.cja.2023.03.030","DOIUrl":null,"url":null,"abstract":"<div><p>The internal friction of floating spline can cause self-excited vibration of a supercritical flexible rotor system. To address this issue, a high-efficiency dynamic modeling method is proposed to investigate the self-excited vibration behavior and instability evolution of the rotor. Experiments are conducted to validate the theoretical results. The coupled dynamic equations for the rotor system connected with the floating spline are derived through the combination of finite element method and lumped parameter model. A hybrid numerical approach of precise integration and Runge-Kutta method is adopted to examine the effects of the friction coefficient of spline’s tooth surface, torque, and eccentricity on the self-excited vibration of the rotor system. The results show that the spline friction leads to negative damping and inputs energy into the rotor system under supercritical conditions, triggering self-excited vibration when the input energy exceeds a specific level. With the same parameters, the experimentally obtained axial trajectory and primary frequency components are consistent with the theoretical results, verifying the accuracy of the proposed theoretical model. This study can serve as a useful theoretical guide for the dynamic stability design of flexible rotor systems with the floating spline.</p></div>","PeriodicalId":55631,"journal":{"name":"Chinese Journal of Aeronautics","volume":"36 12","pages":"Pages 247-267"},"PeriodicalIF":5.3000,"publicationDate":"2023-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S1000936123000912/pdfft?md5=e00d19d83662897ffe70f5bef24bd9f2&pid=1-s2.0-S1000936123000912-main.pdf","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Chinese Journal of Aeronautics","FirstCategoryId":"1087","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1000936123000912","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 1

Abstract

The internal friction of floating spline can cause self-excited vibration of a supercritical flexible rotor system. To address this issue, a high-efficiency dynamic modeling method is proposed to investigate the self-excited vibration behavior and instability evolution of the rotor. Experiments are conducted to validate the theoretical results. The coupled dynamic equations for the rotor system connected with the floating spline are derived through the combination of finite element method and lumped parameter model. A hybrid numerical approach of precise integration and Runge-Kutta method is adopted to examine the effects of the friction coefficient of spline’s tooth surface, torque, and eccentricity on the self-excited vibration of the rotor system. The results show that the spline friction leads to negative damping and inputs energy into the rotor system under supercritical conditions, triggering self-excited vibration when the input energy exceeds a specific level. With the same parameters, the experimentally obtained axial trajectory and primary frequency components are consistent with the theoretical results, verifying the accuracy of the proposed theoretical model. This study can serve as a useful theoretical guide for the dynamic stability design of flexible rotor systems with the floating spline.

查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
浮动花键柔性转子系统自激振动的理论与实验研究
浮动花键的内部摩擦会引起超临界柔性转子系统的自激振动。针对这一问题,提出了一种高效的动态建模方法来研究转子的自激振动行为和不稳定性演变。实验验证了理论结果。通过结合有限元法和叠加参数模型,推导出了与浮动花键连接的转子系统的耦合动态方程。采用精确积分和 Runge-Kutta 混合数值方法,研究了花键齿面摩擦系数、扭矩和偏心率对转子系统自激振动的影响。结果表明,在超临界条件下,花键摩擦会导致负阻尼并向转子系统输入能量,当输入能量超过特定水平时会引发自激振动。在参数相同的情况下,实验得到的轴向轨迹和主频分量与理论结果一致,验证了所提理论模型的准确性。这项研究可为采用浮动花键的柔性转子系统的动态稳定性设计提供有益的理论指导。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics 工程技术-工程:宇航
CiteScore
10.00
自引率
17.50%
发文量
3080
审稿时长
55 days
期刊介绍: Chinese Journal of Aeronautics (CJA) is an open access, peer-reviewed international journal covering all aspects of aerospace engineering. The Journal reports the scientific and technological achievements and frontiers in aeronautic engineering and astronautic engineering, in both theory and practice, such as theoretical research articles, experiment ones, research notes, comprehensive reviews, technological briefs and other reports on the latest developments and everything related to the fields of aeronautics and astronautics, as well as those ground equipment concerned.
期刊最新文献
Editorial Board - Inside Front Cover Table of Content Inhibiting plastic tensile instability of non-symmetric thin-walled shell component via increasing regional metal inflow based on heterogeneous pressure-carrying medium Technologies and studies of gas exchange in two-stroke aircraft piston engine: A review Mechanism of capture section affecting an intake for atmosphere-breathing electric propulsion
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1