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航空发动机砂尘吸入物静电监测仿真实验

孙见忠 姜衡 陈颖达

孙见忠, 姜衡, 陈颖达. 航空发动机砂尘吸入物静电监测仿真实验[J]. 航空动力学报, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.011
引用本文: 孙见忠, 姜衡, 陈颖达. 航空发动机砂尘吸入物静电监测仿真实验[J]. 航空动力学报, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.011
Aero engine sand dust ingestion electrostatic monitoring simulation experiment[J]. Journal of Aerospace Power, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.011
Citation: Aero engine sand dust ingestion electrostatic monitoring simulation experiment[J]. Journal of Aerospace Power, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.011

航空发动机砂尘吸入物静电监测仿真实验

doi: 10.13224/j.cnki.jasp.2018.12.011

Aero engine sand dust ingestion electrostatic monitoring simulation experiment

  • 摘要: 提出了航空发动机砂尘吸入物静电监测的仿真实验方法,实验以软件ANSYS电磁场分析模块建立有限元模型为基础,模拟不同粒径、荷质比、运动速度及质量浓度情况下砂尘吸入物的静电感应信号,并分别从时域与频域对感应电荷与电压信号进行分析,研究砂尘吸入物的粒径及其他宏观参数与静电监测信号之间的关系,建立用以表征砂尘颗粒粒径大小的特征指标。基于IDMS(进气监测系统)感应电压信号功率谱密度分布建立了特征向量,并以其曼哈顿距离与欧氏距离作为特征指标表征砂尘颗粒粒径大小。经仿真实验验证:特征指标与砂尘粒径呈正相关,且不受砂尘吸入物运动速度及荷质比变化的影响,但受砂尘吸入物质量浓度影响。进一步研究将利用质量浓度对特征指标进行修正,并开展验证实验。

     

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出版历程
  • 收稿日期:  2017-11-19
  • 刊出日期:  2018-12-28

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