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带摩擦阻尼装置系统振动响应分析方法研究
引用本文:漆文凯,高德平.带摩擦阻尼装置系统振动响应分析方法研究[J].航空动力学报,2006,21(1):161-167.
作者姓名:漆文凯  高德平
作者单位:南京航空航天大学,能源与动力学院,江苏,南京,210016
摘    要:引入整体-局部一体化滑动模型,提出了带摩擦阻尼装置平板叶片的振动响应分析方法,通过与实验结果对比,验证了分析方法的有效性;定义了无量纲正压力,通过不同无量纲正压力下平板叶片的振动响应分析,获得了振动响应与无量纲正压力的关系曲线.计算结果表明:在局部滑动阶段摩擦阻尼对系统振动的抑制仍然有明显的效果,因此在摩擦阻尼减振分析中,引入局部滑动模型具有重要意义,并可通过无量纲正压力对阻尼器的参数进行优化,使系统在共振时的响应达到最小.

关 键 词:航空、航天推进系统  干摩擦阻尼  局部滑动  整体滑动  振动响应分析
文章编号:1000-8055(2006)01-0161-07
收稿时间:6/8/2005 12:00:00 AM
修稿时间:2005年6月8日

Study of Vibration Response Analysis Method for the Dry Friction Damping Systems
QI Wen-kai and GAO De-ping.Study of Vibration Response Analysis Method for the Dry Friction Damping Systems[J].Journal of Aerospace Power,2006,21(1):161-167.
Authors:QI Wen-kai and GAO De-ping
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:The macro-micro slip model was used to analyze vibration response of plate blades with a dry friction damping.Compared to the experimental results,the analytical method was proved to be feasible.Non-dimensional normal force was defined,and by the use of it,the relationship between the vibration responses and non-dimensional normal force of the plate blades with a dry friction damper were obtained.The calculation results indicate that in the micro-slip stage,the friction damper can markedly reduce the responses of the vibration system,so that the introduction of micro-slip model is very important,and the non-dimensional normal force can be used as a design variable of dry friction dampers to optimize parameters of damper making the response of a vibration system to be minimum while resonance occurs.
Keywords:aerospace propulsion system  dry friction damping  micro-slip  macro-slip  vibration response analysis
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