Development of On-line Performance Diagnostic Program of a Helicopter Turboshaft Engine
Gas turbine performance diagnostics is a method for detecting, isolating and quantifying faults in gas turbine gas path components. On-line precise fault diagnosis can promote greatly reliability and availability of gas turbine in real time operation. This work proposes a GUI-type on-line diagnostic...
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Published in | International journal of aeronautical and space sciences Vol. 10; no. 2; pp. 34 - 42 |
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Main Authors | , , , |
Format | Journal Article |
Language | Korean |
Published |
2009
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Subjects | |
Online Access | Get full text |
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Summary: | Gas turbine performance diagnostics is a method for detecting, isolating and quantifying faults in gas turbine gas path components. On-line precise fault diagnosis can promote greatly reliability and availability of gas turbine in real time operation. This work proposes a GUI-type on-line diagnostic program using SIMULINK and Fuzzy-Neuro algorithms for a helicopter turboshaft engine. During development of the diagnostic program, a look-up table type base performance module are used for reducing computer calculating time and a signal generation module for simulating real time performance data. This program is composed of the on-line condition monitoring program to monitor on-line measuring performance condition, the fuzzy inference system to isolate the faults from measuring data and the neural network to quantify the isolated faults. Evaluation of the proposed on-line diagnostic program is performed through application to the helicopter engine health monitoring. |
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Bibliography: | KISTI1.1003/JNL.JAKO200913060409690 |
ISSN: | 2093-274X 2093-2480 |