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
Link To Document :
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