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Development of On-line Performance Diagnostic Program of a Helicopter Turboshaft Engine
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 Title & Authors
Development of On-line Performance Diagnostic Program of a Helicopter Turboshaft Engine
Kong, Chang-Duk; Koo, Young-Ju; Kho, Seong-Hee; Ryu, Hye-Ok;
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 Abstract
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.
 Keywords
On-line Performance Diagnostic Program;On-line Condition Monitoring;Fuzzy Logic;Neural Network;Turboshaft Engine;
 Language
English
 Cited by
1.
Study on Fault Diagnostics of a Turboprop Engine Using Inverse Performance Model and Artificial Intelligent Methods, International Journal of Turbo and Jet Engines, 2011, 28, 4  crossref(new windwow)
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Jayoung Ki, Changduk Kong, Seonghee Kho, Jaehwan Kim, Ieeki Ahn, Daesung Lee, "Development of On-line Performance Diagnostics Program of a Helicopter Propulsion System", ASME TURBO EXPO 2009, 2009-GT-59519.

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