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Fault diagnosis and isolation of the component and sensor for aircraft engine

QIU Xiao-jie HUANG Jin-quan LU Feng LIU Nan

QIU Xiao-jie, HUANG Jin-quan, LU Feng, LIU Nan. Fault diagnosis and isolation of the component and sensor for aircraft engine[J]. 航空动力学报, 2012, 27(6): 1432-1440.
引用本文: QIU Xiao-jie, HUANG Jin-quan, LU Feng, LIU Nan. Fault diagnosis and isolation of the component and sensor for aircraft engine[J]. 航空动力学报, 2012, 27(6): 1432-1440.
QIU Xiao-jie, HUANG Jin-quan, LU Feng, LIU Nan. Fault diagnosis and isolation of the component and sensor for aircraft engine[J]. Journal of Aerospace Power, 2012, 27(6): 1432-1440.
Citation: QIU Xiao-jie, HUANG Jin-quan, LU Feng, LIU Nan. Fault diagnosis and isolation of the component and sensor for aircraft engine[J]. Journal of Aerospace Power, 2012, 27(6): 1432-1440.

Fault diagnosis and isolation of the component and sensor for aircraft engine

基金项目: Program Sponsored for Scientific Innovation Research of College Graduate in Jiangsu Province(CX10B_108Z)

Fault diagnosis and isolation of the component and sensor for aircraft engine

Funds: Program Sponsored for Scientific Innovation Research of College Graduate in Jiangsu Province(CX10B_108Z)
  • 摘要: Aircraft engine component and sensor fault detection and isolation approach was proposed,which included fault type detection module and component-sensor simultaneous fault isolation module. The approach can not only distinguish among sensor fault, component fault and component-sensor simultaneous fault, but also isolate and locate sensor fault and the type of engine component fault when the engine component fault and the sensor faults occur simultaneously. The double-threshold mechanism has been proposed, in which the fault diagnostic threshold changed with the sensor type and the engine condition, and it greatly improved the accuracy and robustness of sensor fault diagnosis system. Simulation results show that the approach proposed can diagnose and isolate the sensor and engine component fault with improved accuracy. It effectively improves the fault diagnosis ability of aircraft engine.

     

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出版历程
  • 收稿日期:  2011-06-30
  • 刊出日期:  2012-06-28

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