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المؤلفNaderi, E.
المؤلفMeskin, Nader
المؤلفKhorasani, K.
تاريخ الإتاحة2022-04-14T08:45:46Z
تاريخ النشر2011
اسم المنشورProceedings of the ASME Turbo Expo
المصدرScopus
المعرّفhttp://dx.doi.org/10.1115/GT2011-45143
معرّف المصادر الموحدhttp://hdl.handle.net/10576/29837
الملخصIn this paper, a nonlinear fault detection and isolation (FDI) scheme that is based on the concept of multiple model (MM) approach is proposed for jet engines. A modular and a hierarchical architecture is proposed which enables the detection and isolation of both single as well as concurrent permanent faults in the engine. A set of nonlinear models of the jet engine in which compressor and turbine maps are used for performance calculations corresponding to various operating modes of the engine (namely, healthy and different fault modes) is obtained. Using the multiple model approach the probabilities corresponding to the engine modes of operation are first generated. The current operating mode of the system is then detected based on evaluating the maximum probability criteria. The performance of our proposed multiple model FDI scheme is evaluated by implementing both the Extended Kalman Filter (EKF) and the Unscented Kalman Filter (UKF). Simulation results presented demonstrate the effectiveness of our proposed multiple model FDI algorithm for both structural and actuator faults in the jet engine. Copyright 2011 by ASME.
اللغةen
الناشرASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011
الموضوعActuator fault
Fault modes
Hierarchical architectures
Maximum probability
Model based approach
Modes of operation
Multiple models
Non-linear model
Nonlinear faults
Operating modes
Performance calculation
Permanent faults
Unscented Kalman Filter
Aircraft engines
Alternative fuels
Bearings (machine parts)
Exhibitions
Fault detection
Jet engines
العنوانNonlinear fault diagnosis of jet engines by using a multiple model-based approach
النوعConference Paper
الصفحات63-75
رقم المجلد1


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