含浮环式挤压油膜阻尼器的转子系统响应分析

周海仑; 罗贵火; 冯国全; 陈果

含浮环式挤压油膜阻尼器的转子系统响应分析

1.
南京航空航天大学民航学院, 南京 210016
2.
南京航空航天大学能源与动力学院, 南京 210016
3.
中国航空工业集团公司沈阳发动机设计研究所, 沈阳 110015

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- 被引次数: 0
出版历程
- 收稿日期: 2011-04-12
- 修回日期: 2011-09-01
- 刊出日期: 2012-03-28

Dynamic response analysis of a rotor supported on floating-ring squeeze film dampers

1.
College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2.
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
3.
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China

摘要

摘要: 针对浮环式挤压油膜阻尼器,研究了阻尼器特性;建立了含浮环式挤压油膜阻尼器转子系统的动力学模型,模型考虑了转子与浮环式挤压油膜阻尼器两层油膜之间的相互耦合作用.利用数值仿真分析了系统的动力特性及其他影响因素,仿真结果表明:浮环式挤压油膜阻尼器能有效抑制系统双稳态响应,选择一个质量适当的浮动环,有利于转子高速运转的稳定.利用含浮环式挤压油膜阻尼器的转子动力学试验台,验证了仿真结果的正确性.
- 双稳态 /
- 转子动力学 /
- 耦合动力学 /
- 挤压油膜阻尼器 /
- 浮环
Abstract: Characteristics were studied for the floating-ring squeeze film damper.The dynamic model of a rotor supported on the dampers was established.The coupling effect between the rotor and two layers film of the damper was considered in the model.Characteristics of the rotor system responses and other influence factors were analysed making use of numerical integral method.The results of numerical integral show that the bi-stable characteristics of rotor supported on the dampers can be effectively restrained,and the rotor can steadily run if floating-ring mass is appropriate.The results of numerical integral were validated with the experiments of the rotor supported on dampers.
- bi-stable /
- rotor dynamics /
- coupling dynamics /
- squeeze film damper /
- floating-ring

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参考文献(16)

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