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挤压油膜阻尼器油膜阻尼系数识别及分析

周海仑 冯国全 张明 艾延廷

中国机械工程2016,Vol.27Issue(15):2015-2019,2020,6.
中国机械工程2016,Vol.27Issue(15):2015-2019,2020,6.DOI:10.3969/j.issn.1004-132X.2016.15.005

挤压油膜阻尼器油膜阻尼系数识别及分析

Damping Coefficient Identification and Analysis for Squeeze Film Dampers

周海仑 1冯国全 2张明 1艾延廷1

作者信息

  • 1. 沈阳航空航天大学辽宁省航空推进系统先进测试技术重点实验室,沈阳,110136
  • 2. 中国航空工业集团公司沈阳发动机设计研究所,沈阳,110015
  • 折叠

摘要

Abstract

In order to identify damping coefficients of SFD,the experimental tests were re-searched.Firstly,the bidirection excitation rig was excited by signal generator and power amplifier. Then the excitation and response data were obtained by impedance head.Lastly,damping coefficients of SFD were obtained by the least squares fit based on the principles of mechanical impedance.The in-fluence of SFD parameters on damping coefficients was researched by changing oil width and clearance.The experimental tests show that the oil damping presents a trend of nonlinear increase with the increase of oil width.Oil damping can be increased by increasing the oil width,then the damping performance of the damper is improved.With the increase of the oil film gap,oil damping presents a trend of nonlinear decrease,and damping performance is declined.

关键词

挤压油膜阻尼器/油膜阻尼/机械阻抗法/双向激励

Key words

squeeze film damper(SFD)/oil damping/mechanical impedance/bidirection excita-tion

分类

航空航天

引用本文复制引用

周海仑,冯国全,张明,艾延廷..挤压油膜阻尼器油膜阻尼系数识别及分析[J].中国机械工程,2016,27(15):2015-2019,2020,6.

基金项目

国家自然科学基金资助项目(51505300) (51505300)

航空科学基金资助项目(2014ZB54008) (2014ZB54008)

辽宁省自然科学基金资助项目(2015020126) (2015020126)

中国机械工程

OA北大核心CSCDCSTPCD

1004-132X

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