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单-厚盘转子过两阶临界转速的瞬态振动分析

刘政 王建军

刘政, 王建军. 单-厚盘转子过两阶临界转速的瞬态振动分析[J]. 北京航空航天大学学报, 2015, 41(11): 2144-2157. doi: 10.13700/j.bh.1001-5965.2014.0699
引用本文: 刘政, 王建军. 单-厚盘转子过两阶临界转速的瞬态振动分析[J]. 北京航空航天大学学报, 2015, 41(11): 2144-2157. doi: 10.13700/j.bh.1001-5965.2014.0699
LIU Zheng, WANG Jianjun. Analysis of transient vibration of single-thick-disk rotor crossing two orders of critical speeds[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2144-2157. doi: 10.13700/j.bh.1001-5965.2014.0699(in Chinese)
Citation: LIU Zheng, WANG Jianjun. Analysis of transient vibration of single-thick-disk rotor crossing two orders of critical speeds[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2144-2157. doi: 10.13700/j.bh.1001-5965.2014.0699(in Chinese)

单-厚盘转子过两阶临界转速的瞬态振动分析

doi: 10.13700/j.bh.1001-5965.2014.0699
详细信息
    作者简介:

    刘政(1991-),男,陕西汉中人,硕士研究生,liuzheng@buaa.edu.cn

    通讯作者:

    王建军(1956-),男,江苏徐州人,教授,wangjianjun@buaa.edu.cn,主要研究方向为结构系统动力特性和振动抑制.

  • 中图分类号: V231.96

Analysis of transient vibration of single-thick-disk rotor crossing two orders of critical speeds

  • 摘要: 航空发动机特殊的鼓式压气机结构可简化为径向转动惯量大于轴向转动惯量的厚盘转子系统,其做正进动时存在两个固有频率.计算了单-厚盘转子分别以定角加速度和定功率过两阶临界转速时对不平衡激振力的瞬态响应,其中定功率厚盘转子还与外界能源发生非线性耦合.结果发现,单-厚盘转子的低阶振型为轴的弯曲,高阶振型为盘的偏摆,其中高阶模态是厚盘转子特有模态;过临界转速时瞬态振动由转子的自由振动和强迫振动合成;当功率不足够提供转子通过临界转速时,出现外界能源与转子系统的能量耦合,造成瞬态振动急剧增大而"失速".

     

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出版历程
  • 收稿日期:  2014-11-17
  • 修回日期:  2015-02-12
  • 网络出版日期:  2015-11-20

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