Measured health signals incorporate significant details about any malfunction in a gas turbine. The attenuation of noise and removal of outliers from these health signals while preserving important features is an important problem in gas turbine diagnostics. The measured health signals are a time series of sensor measurements such as the low rotor speed, high rotor speed, fuel flow, and exhaust gas temperature in a gas turbine. In this article, a comparative study is done by varying the window length of acausal and unsymmetrical weighted recursive median filters and numerical results for error minimization are obtained. It is found that optimal filters exist, which can be used for engines where data are available slowly (three-point filter) and rapidly (seven-point filter). These smoothing filters are proposed as preprocessors of measurement delta signals before subjecting them to fault detection and isolation algorithms.
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October 2011
Technical Briefs
Three- and Seven-Point Optimally Weighted Recursive Median Filters for Gas Turbine Diagnostics
V. N. Guruprakash,
V. N. Guruprakash
Department of Aerospace Engineering,
Indian Institute of Science
, Bangalore 560012, India
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Ranjan Ganguli
Ranjan Ganguli
Professor
Mem. ASME
Department of Aerospace Engineering,
e-mail: ganguli@aero.iisc.ernet.in
Indian Institute of Science
, Bangalore 560012, India
Search for other works by this author on:
V. N. Guruprakash
Department of Aerospace Engineering,
Indian Institute of Science
, Bangalore 560012, India
Ranjan Ganguli
Professor
Mem. ASME
Department of Aerospace Engineering,
Indian Institute of Science
, Bangalore 560012, Indiae-mail: ganguli@aero.iisc.ernet.in
J. Eng. Gas Turbines Power. Oct 2011, 133(10): 104502 (4 pages)
Published Online: May 3, 2011
Article history
Received:
August 23, 2010
Revised:
December 15, 2010
Online:
May 3, 2011
Published:
May 3, 2011
Citation
Guruprakash, V. N., and Ganguli, R. (May 3, 2011). "Three- and Seven-Point Optimally Weighted Recursive Median Filters for Gas Turbine Diagnostics." ASME. J. Eng. Gas Turbines Power. October 2011; 133(10): 104502. https://doi.org/10.1115/1.4003285
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