Dynamic response analysis of a rotor supported on floating-ring squeeze film dampers
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Dynamic response analysis of a rotor supported on floating-ring squeeze film dampers
Vol. 27, Issue 3, (2012)
作者机构:
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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Published:2012
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ZHOU Hai-lun, LUO Gui-huo, FENG Guo-quan, et al. Dynamic response analysis of a rotor supported on floating-ring squeeze film dampers[J]. 2012, 27(3).
DOI:
ZHOU Hai-lun, LUO Gui-huo, FENG Guo-quan, et al. Dynamic response analysis of a rotor supported on floating-ring squeeze film dampers[J]. 2012, 27(3).DOI:
Dynamic response analysis of a rotor supported on floating-ring squeeze film dampers
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.
Experimental comparison of vibration isolation ability of centralized and uncentralized squeeze film damper
Sudden unbalance response analysis of rotor system supported on floating ring squeeze film damper
Dynamic characteristics of misaligned gear coupling⁃bearing⁃rotor system
转子系统挤压油膜阻尼器设计与动力特性
基于三维接触摩擦单元的套齿连接解析建模研究
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毛川
李鹏飞
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AI Yan-ting
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Guoyuan ZHANG
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Related Institution
浙江大学 电气工程学院
先进航空发动机协同创新中心
Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System, Faculty of Aerospace Engineering, Shenyang Aerospace University
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Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation