Novelty detection in jet engine vibration spectra

2015 ◽  
Vol 5 (2) ◽  
pp. 2-7 ◽  
Author(s):  
D A Clifton ◽  
L Tarassenko
Author(s):  
Dan M. Ghiocel

The paper proposes a refined stochastic fault classifier for jet engine vibration diagnostic based on advanced stochastic concepts. The statistical data to be analyzed are the spectrum profiles of vibration measured at different locations in the engine. The statistical spectrum profiles are idealized by non-homogeneous stochastic fields with non-Gaussian probability distributions. The proposed stochastic classifier is based on the decomposition of the statistical correlation matrix of spectrum profiles using a Karhunen-Loeve (KL) expansion. Two stochastic classifiers are proposed, namely a “global” and a “specific” fault classifier. The “global” KL classifier, which is a scalar quantity, is an efficient anomaly/novelty detection tool for identifying incipient fault diagnosis with small amplitude fluctuations. The “specific” KL classifier, which is a vector quantity, is a refined diagnostic tool for identifying the engine malfunction causes. An illustrative example of a turbofan engine is included.


2007 ◽  
Vol 347 ◽  
pp. 305-310 ◽  
Author(s):  
David A. Clifton ◽  
Peter R. Bannister ◽  
Lionel Tarassenko

A novelty detection approach to condition monitoring of aerospace gas-turbine engines is presented, providing a consistent framework for on- and off-line analysis, each with differing typical implementation constraints. On-line techniques are introduced for observing abnormality in engine behaviour during aircraft flights, and are shown to provide early warning of engine events in real-time. Off-line techniques within the same analysis framework are shown to allow the tracking of single engines and fleets of engines from ground-based monitoring stations on a flight-by-flight basis. Results are validated by comparison to conventional techniques, in application to aerospace engines and other industrial high-integrity systems.


1999 ◽  
Vol 6 (1) ◽  
pp. 53-66 ◽  
Author(s):  
Alexandre Nairac ◽  
Neil Townsend ◽  
Roy Carr ◽  
Steve King ◽  
Peter Cowley ◽  
...  

Author(s):  
David A. Clifton ◽  
Peter R. Bannister ◽  
Lionel Tarassenko
Keyword(s):  

1967 ◽  
Author(s):  
Fred L. Young ◽  
William J. Bays ◽  
Edwin C. Reynolds
Keyword(s):  

Author(s):  
Paul Hayton ◽  
Simukai Utete ◽  
Dennis King ◽  
Steve King ◽  
Paul Anuzis ◽  
...  

Novelty detection requires models of normality to be learnt from training data known to be normal. The first model considered in this paper is a static model trained to detect novel events associated with changes in the vibration spectra recorded from a jet engine. We describe how the distribution of energy across the harmonics of a rotating shaft can be learnt by a support vector machine model of normality. The second model is a dynamic model partially learnt from data using an expectation–maximization-based method. This model uses a Kalman filter to fuse performance data in order to characterize normal engine behaviour. Deviations from normal operation are detected using the normalized innovations squared from the Kalman filter.


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