DocumentCode
1929670
Title
Vibration analysis via neural network inverse models to determine aircraft engine unbalance condition
Author
Hu, Xiao ; Vian, John ; Slepski, Joseph R. ; Wunsch, Donald C., II
Author_Institution
Appl. Comput. Intelligence Lab., Missouri Univ., Rolla, MO, USA
Volume
4
fYear
2003
fDate
20-24 July 2003
Firstpage
3001
Abstract
This paper describes the use of artificial neural networks (ANNs) with the vibration data from real flight tests for detecting engine health condition - mass imbalance herein. Order-tracking data, calculated from time series is used as the input to the neural networks to determine the amount and location of mass imbalance on aircraft engines. Several neural network methods, including multilayer perceptron (MLP), extended Kalman filter (EKF) and support vector machines (SVMs) are used in the neural network inverse model for the performance comparison. The promising performances are presented at the end.
Keywords
aerospace computing; aerospace engines; condition monitoring; fault diagnosis; mechanical engineering computing; neural nets; vibration measurement; aircraft engine unbalance condition; artificial neural networks; engine health condition; extended Kalman filter; mass imbalance; multilayer perceptron; neural network inverse model; neural network inverse models; order tracking data; real flight tests; support vector machines; time series; vibration analysis; vibration data; Aircraft propulsion; Artificial neural networks; Condition monitoring; Engines; Inverse problems; Multi-layer neural network; Neural networks; Predictive models; Testing; Turbines;
fLanguage
English
Publisher
ieee
Conference_Titel
Neural Networks, 2003. Proceedings of the International Joint Conference on
ISSN
1098-7576
Print_ISBN
0-7803-7898-9
Type
conf
DOI
10.1109/IJCNN.2003.1224049
Filename
1224049
Link To Document