International Journal of Turbo and Jet Engines · 2011 · 13 citations · 6 references
Fault DiagnosisEngineeringMeasurementDiagnosisFault ForecastingDiagnostic StagesSystem DiagnosisEngine BaselineNonlinear System IdentificationCondition MonitoringReliability EngineeringSystems EngineeringModeling And SimulationStatisticsComputer EngineeringStructural Health MonitoringNeural NetworksEnergy PredictionComparative StudyGas Turbine MonitoringDiagnostic SystemProblem DetectionProcess ControlGas Turbine EnginePrognosticsData Modeling
Gas turbine health monitoring includes the common stages of problem detection, fault identification, and prognostics. To extract useful diagnostic information from raw recorded data, these stages require a preliminary operation of computing differences between measurements and an engine baseline, which is a function of engine operating conditions. These deviations of measured values from the baseline data can be good indicators of engine health. However, their quality and the success of all diagnostic stages strongly depend on the adequacy of the baseline model employed and, in particular, on the mathematical techniques applied to create it.
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