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涨圈密封挤压油膜阻尼器流场与阻尼特性
引用本文:崔颖,罗乔丹,邱凯,黄宇熙. 涨圈密封挤压油膜阻尼器流场与阻尼特性[J]. 航空动力学报, 2021, 36(12): 2474-2481. DOI: 10.13224/j.cnki.jasp.20210445
作者姓名:崔颖  罗乔丹  邱凯  黄宇熙
作者单位:大连海事大学船舶与海洋工程学院,辽宁大连116026
基金项目:辽宁省自然科学基金指导计划(201602070)
摘    要:为研究两端密封型挤压油膜阻尼器流场与阻尼特性,建立了涨圈密封挤压油膜阻尼器三维非定常流场数值仿真模型.基于Fluent软件中的Mixture多相流模型和Schnerr-Sauer空化模型数值模拟得到动态油膜压力与气相体积分数的周向分布规律.将计算得到的阻尼器油膜压力与文献中的试验数据对比,结果显示:两者具有较高的一致性...

关 键 词:挤压油膜阻尼器  涨圈密封  空化模型  动态油膜压力  等效阻尼系数
收稿时间:2021-08-12

Flow field and damping characteristics of piston ring sealed squeeze film damper
CUI Ying,LUO Qiaodan,QIU Kai,HUNAG Yuxi. Flow field and damping characteristics of piston ring sealed squeeze film damper[J]. Journal of Aerospace Power, 2021, 36(12): 2474-2481. DOI: 10.13224/j.cnki.jasp.20210445
Authors:CUI Ying  LUO Qiaodan  QIU Kai  HUNAG Yuxi
Affiliation:Naval Architecture and Ocean Engineering College,Dalian Maritime University,Dalian Liaoning 116026,China
Abstract:In order to study the flow field and damping characteristics of squeeze film damper sealed at both ends,a three-dimensional unsteady flow field numerical simulation model of squeeze film damper with piston ring seal was established.The circumferential oil film pressure distribution at different times was calculated based on the Mixture multiphase flow model and Schnerr-Sauer cavitation model in Fluent software,and compared with the experimental data in literature.The results showed that both were in good agreement.The average equivalent damping coefficient derived from the dynamic oil film force had only a deviation of 0.6% compared with the results identified by the impedance method,which verified the effectiveness of the numerical model.Further numerical calculations demonstrated that increasing the whirl amplitude,whirl frequency and the width of piston ring gap can aggravate the cavitation phenomenon in the flow field of the squeeze film damper and reduce the equivalent damping coefficient. 
Keywords:squeeze film damper  piston ring seal  cavitation model  dynamic oil film pressure  equivalent damping coefficient
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