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简谐激励下柔性卡箍支承管路系统响应

李占营 王建军 邱明星

李占营, 王建军, 邱明星. 简谐激励下柔性卡箍支承管路系统响应[J]. 航空动力学报, 2017, 32(11): 2705-2712. doi: 10.13224/j.cnki.jasp.2017.11.018
引用本文: 李占营, 王建军, 邱明星. 简谐激励下柔性卡箍支承管路系统响应[J]. 航空动力学报, 2017, 32(11): 2705-2712. doi: 10.13224/j.cnki.jasp.2017.11.018
Responses of pipe system with flexible clamp under harmonic excitation[J]. Journal of Aerospace Power, 2017, 32(11): 2705-2712. doi: 10.13224/j.cnki.jasp.2017.11.018
Citation: Responses of pipe system with flexible clamp under harmonic excitation[J]. Journal of Aerospace Power, 2017, 32(11): 2705-2712. doi: 10.13224/j.cnki.jasp.2017.11.018

简谐激励下柔性卡箍支承管路系统响应

doi: 10.13224/j.cnki.jasp.2017.11.018

Responses of pipe system with flexible clamp under harmonic excitation

  • 摘要: 针对柔性卡箍支承航空发动机管路系统振动问题,研究了柔性卡箍的刚度特性及其对管路系统响应特性的影响。建立了包含管路和柔性卡箍的管路系统流固耦合有限元模型,给出了系统时域响应的Newmark积分方法。采用解析推导和试验测试两种方法对柔性卡箍刚度特性进行了研究,研究结果表明:柔性卡箍的刚度具有明显的分段线性特性。通过对基础简谐激励作用下管路系统时域受迫响应分析,研究了柔性卡箍支承刚度对系统非线性行为的影响。发现柔性卡箍刚度的不对称性较大时,系统的幅频响应特性曲线出现明显的非线性突跳现象;在特定频率范围,响应中存在激励频率的亚谐和超谐分量;随着流体流速和压力的增加,系统固有频率减小。

     

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出版历程
  • 收稿日期:  2016-04-04
  • 刊出日期:  2017-11-28

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