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A Multiple Model-Based Approach for Fault Diagnosis of Jet Engines

机译:基于多模型的喷气发动机故障诊断方法

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摘要

In this brief, a novel real-time fault detection and isolation (FDI) scheme that is based on the concept of multiple model is proposed for aircraft jet engines. A modular and a hierarchical architecture is developed which enables the detection and isolation of both single faults as well as multiple concurrent faults in the jet engine. The nonlinear dynamics of a dual spool jet engine is linearized and a set of linear models corresponding to various operating modes of the jet engine (namely healthy and different faulty modes) at each operating point is obtained. Using the multiple model approach the probabilities corresponding to each operating point of the jet engine are generated and the current operating mode of the system is detected based on evaluating the maximum probability criteria. It is shown that the proposed methodology is also robust to the failure of pressure and temperature sensors and extensive levels of noise outliers in the sensor measurements. Simulation results are presented that demonstrate the effectiveness and capabilities of our proposed multiple model FDI algorithm for both structural faults and an actuator fault in the aircraft jet engine.
机译:在此简介中,针对飞机喷气发动机,提出了一种基于多重模型概念的新颖的实时故障检测与隔离(FDI)方案。开发了模块化和分层的体系结构,该体系结构使得能够检测和隔离喷气发动机中的单个故障以及多个并发故障。使双滑阀喷气发动机的非线性动力学线性化,并获得与每个喷气机在每个工作点的各种运行模式(即正常运行和不同故障模式)相对应的一组线性模型。使用多模型方法,将生成与喷气发动机每个工作点相对应的概率,并基于评估最大概率标准来检测系统的当前运行模式。结果表明,所提出的方法对于压力和温度传感器的故障以及传感器测量中广泛的噪声离群值也具有鲁棒性。仿真结果表明了我们提出的多模型FDI算法对飞机喷气发动机的结构性故障和执行器故障的有效性和功能。

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