• DocumentCode
    1175589
  • Title

    Denoising jet engine gas path measurements using nonlinear filters

  • Author

    Verma, Rajeev ; Ganguli, Ranjan

  • Author_Institution
    Dept. of Adv. Eng., Ashok Leyland Ltd., Chennai, India
  • Volume
    10
  • Issue
    4
  • fYear
    2005
  • Firstpage
    461
  • Lastpage
    464
  • Abstract
    Traditionally, linear filters have been used to smooth time series of gas path measurements before performing fault detection and isolation. However, linear filters can smooth out sharp trend shifts in the signal and are also not good at removing outliers. Since most fault detection and isolation algorithms are optimized for Gaussian noise, they can show performance degradation when outliers are present. In this study, numerical results with simulated data for engine deterioration and abrupt fault show that the nonlinear rational filter with median preprocessor are useful for gas turbine health monitoring applications resulting in noise reduction of 73%-96% while preserving signal features and removing outliers.
  • Keywords
    Gaussian noise; aerospace computing; aircraft maintenance; computerised instrumentation; condition monitoring; fault location; gas turbines; jet engines; nonlinear filters; signal denoising; time series; Gaussian noise; engine deterioration; fault detection; fault isolation; gas turbine health monitoring; jet engine gas path measurement; measurement denoising; nonlinear rational filters; time series; Degradation; Fault detection; Gaussian noise; Jet engines; Noise reduction; Nonlinear filters; Numerical simulation; Performance evaluation; Time measurement; Turbines; Fault diagnosis; gas turbines; signal processing;
  • fLanguage
    English
  • Journal_Title
    Mechatronics, IEEE/ASME Transactions on
  • Publisher
    ieee
  • ISSN
    1083-4435
  • Type

    jour

  • DOI
    10.1109/TMECH.2005.852454
  • Filename
    1512170