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涡扇发动机传感器故障诊断的快速原型实时仿真

赵成伟 叶志锋 王继强 殷彬彬

赵成伟, 叶志锋, 王继强, 殷彬彬. 涡扇发动机传感器故障诊断的快速原型实时仿真[J]. 航空动力学报, 2014, 29(2): 451-457. doi: 10.13224/j.cnki.jasp.2014.02.026
引用本文: 赵成伟, 叶志锋, 王继强, 殷彬彬. 涡扇发动机传感器故障诊断的快速原型实时仿真[J]. 航空动力学报, 2014, 29(2): 451-457. doi: 10.13224/j.cnki.jasp.2014.02.026
ZHAO Cheng-wei, YE Zhi-feng, WANG Ji-qiang, YIN Bin-bin. Rapid prototype real-time simulation of turbo-fan engine sensor fault diagnosis[J]. Journal of Aerospace Power, 2014, 29(2): 451-457. doi: 10.13224/j.cnki.jasp.2014.02.026
Citation: ZHAO Cheng-wei, YE Zhi-feng, WANG Ji-qiang, YIN Bin-bin. Rapid prototype real-time simulation of turbo-fan engine sensor fault diagnosis[J]. Journal of Aerospace Power, 2014, 29(2): 451-457. doi: 10.13224/j.cnki.jasp.2014.02.026

涡扇发动机传感器故障诊断的快速原型实时仿真

doi: 10.13224/j.cnki.jasp.2014.02.026

Rapid prototype real-time simulation of turbo-fan engine sensor fault diagnosis

  • 摘要: 为快速高效地完成涡扇发动机传感器故障诊断算法的硬件在环仿真试验,构建了以NI CompactRIO为核心的传感器故障诊断系统的快速原型实时仿真平台.基于一簇卡尔曼滤波器,在LabVIEW编程环境中建立了传感器故障诊断系统.分别在涡扇发动机模型稳态和动态工作时完成了对单个传感器故障的检测、隔离和重构的硬件在环仿真试验并验证了算法精度.经过大量试验,结果表明:基于卡尔曼滤波器理论的诊断算法能在传感器故障情况下确保控制系统安全运行,诊断精度最高可达1.4%;同时表明,该快速原型实时仿真平台的设计是成功的.研究工作为发动机传感器故障诊断系统的半物理仿真试验奠定了基础.

     

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出版历程
  • 收稿日期:  2012-12-12
  • 刊出日期:  2014-02-28

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