首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >DESIGN OF FAULT DETECTION SYSTEM FOR A HEAVY DUTY GAS TURBINE WITH STATE OBSERVER AND TRACKING FILTER
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DESIGN OF FAULT DETECTION SYSTEM FOR A HEAVY DUTY GAS TURBINE WITH STATE OBSERVER AND TRACKING FILTER

机译:带有状态观测器和跟踪滤波器的重型燃气轮机故障检测系统的设计

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There exist many approaches for gas turbine engine condition monitoring and fault diagnosis. Among them, gas path analysis depends on the relations between deviations of performance parameters and deviations of measurements, such as pressure, temperature, at some positions in the flow path. A dynamic tracking filter combined with a nonlinear gas turbine model can be used to implement a fault detection system. The dynamic tracking filter is composed with multiple feedback loops in which the residuals between model output and measurement are driven to zero by adjusting the performance parameters. In many cases, the number of measurement parameters is less than that of performance parameters, which impose a limit on the application of tracking filter in practical situations. In the present study, the tracking filter is retrofitted to be driven by the error between state of the model and the estimated state reconstructed from the engine measurement. For the time being, only linear time-invariant (LTI) state observer is considered. A nonlinear simulation model of the heavy-duty gas turbine under study is used to derive the linear system model needed for the design of LTI state observer. Input vector and output vector are chosen according to the practical situations. The linear system model obtained around the nominal operating point is observable, so a state observer can be designed. With 6 state variables observable from the engine, 6 performance parameters can be tracked with the proper design of tracking filter. The structure of the tracking filter consists of a static decoupling matrix DM and in series with 6 PI controllers. Deviations of performance parameters are implanted into the gas turbine model by scaling the performance maps used; and then simulation results are taken as measurements needed for the tracking filter to run. Tracking results of performance parameters in different cases are given to show the tracking capability for isolated performance deviations and concurrent performance deviations.
机译:存在许多用于燃气涡轮发动机状态监测和故障诊断的方法。其中,气路分析取决于在流路中某些位置的性能参数偏差和测量偏差(例如压力,温度)之间的关系。动态跟踪滤波器与非线性燃气轮机模型相结合可用于实现故障检测系统。动态跟踪滤波器由多个反馈回路组成,其中通过调整性能参数将模型输出与测量之间的残差驱动为零。在许多情况下,测量参数的数量少于性能参数的数量,这在实际情况下限制了跟踪滤波器的应用。在本研究中,对跟踪滤波器进行了改造,使其由模型状态与根据发动机测量值重建的估计状态之间的误差所驱动。目前,仅考虑线性时不变(LTI)状态观察器。使用研究中的重型燃气轮机的非线性仿真模型来推导设计LTI状态观测器所需的线性系统模型。输入向量和输出向量根据实际情况选择。在标称工作点附近获得的线性系统模型是可观察的,因此可以设计状态观察器。通过从引擎可观察到的6个状态变量,可以通过适当设计的跟踪滤波器来跟踪6个性能参数。跟踪滤波器的结构由静态去耦矩阵DM组成,并与6个PI控制器串联。通过缩放所使用的性能图,将性能参数的偏差植入到燃气轮机模型中。然后将模拟结果作为跟踪滤波器运行所需的测量值。给出了不同情况下性能参数的跟踪结果,以显示对孤立性能偏差和并发性能偏差的跟踪能力。

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