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挤压油膜阻尼器失效边界探索 被引量:5

Probe into Failure Boundaries of Squeeze Film Damper
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摘要 挤压油膜阻尼器设计不当,会导致功能失效。创建了弹支挤压油股阻尼器的双稳态区域图和减振失效边界围。只要轴承参数B和质量估心率U值不在双稳态区域内,便不会出现双稳态特性;离开诚振失效的边界,便可有效的减振。研制挤压油膜阻尼器时,应用此二图,可以带来很大的方便。 If the squeeze film damper is not designed properly, that will be caused the failure of attenuating vibration. This paper has established a bistable region diagram and a boundary diagram of the failure to attenuating vibration.Only the values of bearing parameter B and the unbalance eccentrisity U are not selected in that region, the bistable character will not be arised. B and U are selected to leave that boundaries, also the failure of attenuating vibration will not be happened. To use the two diagrams that will bring a lot of convenience for development of the squeeze film damper.
作者 王屏 刘方杰
出处 《强度与环境》 1998年第3期28-34,共7页 Structure & Environment Engineering
基金 航空基础科学基金
关键词 挤压油膜 阻尼器 燃气涡轮发动机 失效 航空器 Squeeze film bearing, Damper, Parametric analysis, Gas turbine engine, Optimun design
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参考文献7

  • 1Brown P F. Bearings and Dampers for Advanced Jet Engines. SAE, Paper, 700318.
  • 2Mohan S, Hahn E J. Design of Squeeze Film Damper Supporting for Rigid Rotors Trans ASME, J of Engineering for Industry, 1978:8:976-982.
  • 3Humes B, The Non-Linear Performance of Squeeze Film Dampers. Ph, D, Thesis University of Sussex,1977.
  • 4Cookson R A, Kossa S S, The Effectiveness of Squeeze Film Damper Bearings Supporting Rigid Rotors without a Centralising Spring. Int J Mech Sci, 1979,21(6):39-650.
  • 5Gunter E J, Barrett LE and Allaire P E. Design of Nonlinear Squeeze Film Damper for Aircraft Engines. Trans ASME Series F, January 1977:57-64.
  • 6刘方杰,沈心敏,尹秀琴.带弹性支座和挤压油膜轴承的刚性转子的稳态特性研究.北京航空学院科学研究报告.BH-B725,1981.09.
  • 7刘方杰,陈照波.挤压油膜阻尼器失效问题的实验研究[J].强度与环境,1998,25(4):17-23. 被引量:4

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