An Evaluation of Engine Faults Diagnostics Using Artificial Neural Networks

Author:

Lu Pong-Jeu1,Zhang Ming-Chuan2,Hsu Tzu-Cheng1,Zhang Jin2

Affiliation:

1. National Cheng Kung University, Tainan, Taiwan

2. Beijing University of Aeronautics and Astronautics, Beijing, China

Abstract

Application of artificial neural network (ANN)-based method to perform engine condition monitoring and fault diagnosis is evaluated. Back-propagation, feedforward neural nets are employed for constructing engine diagnostic networks. Noise-contained training and testing data are generated using an influence coefficient matrix and the data scatters. The results indicate that under high-level noise conditions ANN fault diagnosis can only achieve a 50–60% success rate. For situations where sensor scatters are comparable to those of the normal engine operation, the success rates for both 4-input and 8-input ANN diagnoses achieve high scores which satisfy the minimum 90% requirement. It is surprising to find that the success rate of the 4-input diagnosis is almost as good as that of the 8-input. Although the ANN-based method possesses certain capability in resisting the influence of input noise, it is found that a preprocessor that can perform sensor data validation is of paramount importance. Auto-associative neural network (AANN) is introduced to reduce the noise level contained. It is shown that the noise can be greatly filtered to result in a higher success rate of diagnosis. This AANN data validation preprocessor can also serve as an instant trend detector which greatly improves the current smoothing methods in trend detection. It is concluded that ANN-based fault diagnostic method is of great potential for future use. However, further investigations using actual engine data have to be done to validate the present findings.

Publisher

American Society of Mechanical Engineers

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1. A Health Condition Monitoring Method of Aeroengine Gas Path System Based on Consistency Fusion and Neural Network;Applied Mechanics and Materials;2013-08

2. Aircraft Propulsion Health Management;System Health Management;2011-05-31

3. Development of a Detection Scheme for Aircraft Engine Failures Based on the Artificial Immune System Paradigm;AIAA Guidance, Navigation, and Control Conference;2010-06-26

4. Methodology of Complex Diagnosing System for Aviation GTE;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

5. Fourier Neural Networks and Generalized Single Hidden Layer Networks in Aircraft Engine Fault Diagnostics;Journal of Engineering for Gas Turbines and Power;2005-10-17

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