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带摩擦阻尼装置系统振动响应分析方法研究

漆文凯 高德平

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.
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.
QI Wen-kai, 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.
Citation: QI Wen-kai, 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.

带摩擦阻尼装置系统振动响应分析方法研究

Study of Vibration Response Analysis Method for the Dry Friction Damping Systems

  • 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。

     

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    [2] Bazan E,Beilak J,Griffin J H.An Efficient Method for Predicting the yibratory Response of Linear Structures with Friction Interfaces[J].Transactions of the ASME,Journal of Engineering for Gas Turbines and Power,1986,108;633 ~640.
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    [10] 郝燕平,朱梓根.带摩擦阻尼的叶片响应求解方法[J].航空学报,2001,22(5);411~414.Hao Yanping,Zhu Zigen.New Method to Resolve Vibratory Response of Blades with Friction Damping[J].Acta Aeronautica et Astronautica Sinica,2001,22 (5) ;411~414.
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出版历程
  • 收稿日期:  2005-06-08
  • 修回日期:  2005-10-25
  • 刊出日期:  2006-02-28

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