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Variations on the Kalman filter for enhanced performance monitoring of gas turbine engines

机译:卡尔曼滤波器的变化形式,可增强对燃气轮机性能的监控

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摘要

Since their advent in the 1940's, gas turbines have been used in a wide range of land, sea and air applications due to their high power density and reliability. In today's competitive market, gas turbine operators need to optimise the dispatch availability (it i.e., minimise operational issues such as aborted take-offs or in-flight shutdowns) as well as the direct operating costs of their assets. Besides improvements in the design and manufacture processes, proactive maintenance practices, based on the actual condition of the turbine, enable the achievement of these objectives.Generating dependable information about the health condition of the gas turbine is a requisite for a successful implementation of condition-based maintenance. In this thesis, we focus on the assessment of the performance of the thermodynamic cycle, also known as Module Performance Analysis. The purpose of module performance analysis is to detect, isolate and quantify changes in engine module performance, described by so-called health parameters, on the basis of measurements collected along the gas-path of the engine. Generally, the health parameters are correcting factors on the efficiency and the flow capacity of the modules while the measurements are inter-component temperatures, pressures, shaft speeds and fuel flow. Module performance analysis can be cast as an estimation problem that is characterised by a number of difficulties such as non-linearity of the system and noise and bias in the measurements. Moreover the number of health parameters usually exceeds the number of gas-path measurements, making the estimation problem underdetermined.This thesis starts with a survey of the state-of-the-art in module performance analysis. We then propose enhancements to a monitoring tool for steady-state data developed by Dr. P. Dewallef during his thesis at the Turbomachinery Group. Specifically, the improvements concern the fault detection and isolation tasks, respectively handled by a hypothesis testing and a sparse estimator. As a complement, we define metrics for the selection and analysis of sensor--health parameter suites based on the Information Theory. In a second step, we investigate the feasibility and the benefit that could be expected from the processing of data collected during transient operation of a gas turbine. We also discuss the impact of modelling errors on the estimation procedure and propose a solution that makes the health assessment robust with respect to modelling errors.The theoretical developments are evaluated on the basis of simulated test-cases through a series of metrics that gauge the estimation accuracy and the performance of the fault detection and isolation modules.
机译:自1940年代问世以来,由于其高功率密度和可靠性,燃气轮机已广泛用于陆地,海洋和空中应用。在当今竞争激烈的市场中,燃气轮机运营商需要优化调度的可用性(即最大限度地减少诸如中止起飞或飞行中的停机之类的运营问题)及其资产的直接运营成本。除了改进设计和制造工艺外,基于涡轮机实际状况的主动维护实践还可以实现这些目标。生成有关燃气涡轮机健康状况的可靠信息是成功实施以下条件的必要条件:基础维护。在本文中,我们着重于热力学循环性能的评估,也称为模块性能分析。模块性能分析的目的是基于沿发动机气路收集的测量值,检测,隔离和量化发动机模块性能的变化(由所谓的健康参数来描述)。通常,健康参数是对模块效率和流量的校正因子,而测量则是组件间温度,压力,轴速和燃料流量。模块性能分析可以看作是一个估计问题,其特征是许多困难,例如系统的非线性以及测量中的噪声和偏差。此外,健康参数的数量通常超过气路测量的数量,从而使估计问题变得不确定。本文从对模块性能分析的最新技术入手。然后,我们建议对P. Dewallef博士在Turbomachinery Group的论文期间开发的稳态数据监视工具进行增强。具体而言,这些改进涉及分别由假设检验和稀疏估计器处理的故障检测和隔离任务。作为补充,我们基于信息理论定义用于选择传感器和健康参数套件的度量标准。在第二步中,我们研究了在燃气轮机瞬态运行过程中收集的数据处理所带来的可行性和益处。我们还讨论了建模错误对估计过程的影响,并提出了一种使健康评估对建模错误具有鲁棒性的解决方案。在模拟测试用例的基础上,通过一系列衡量估计的指标来评估理论发展故障检测和隔离模块的准确性和性能。

著录项

  • 作者

    Borguet, Sébastien;

  • 作者单位
  • 年度 2012
  • 总页数
  • 原文格式 PDF
  • 正文语种 en
  • 中图分类

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