| Autor: |
Seonghee Kho, Changduk Kong, Hyeok Ryu, Youngju Koo |
| Rok vydání: |
2009 |
| Předmět: |
|
| Zdroj: |
International Journal of Aeronautical and Space Sciences. 10:34-42 |
| ISSN: |
2093-274X |
| DOI: |
10.5139/ijass.2009.10.2.034 |
| Popis: |
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. |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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