首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.2; 20060506-11; Barcelona(ES) >A GENERALIZED FAULT CLASSIFICATION FOR GAS TURBINE DIAGNOSTICS ON STEADY STATES AND TRANSIENTS
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A GENERALIZED FAULT CLASSIFICATION FOR GAS TURBINE DIAGNOSTICS ON STEADY STATES AND TRANSIENTS

机译:基于稳态和暂态的燃气轮机诊断的广义故障分类

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摘要

Gas turbine diagnostic techniques are often based on the recognition methods using the deviations between actual and expected thermodynamic performances. The problem is that the deviations depend on real operating conditions. However, our studies show that such a dependency can be reduced. In this paper, we propose the generalized fault classification that is independent of the operating conditions. To prove this idea, the averaged probabilities of the correct diagnosis are computed and compared for two cases: the proposed classification and the traditional one based on the fixed operating conditions. The probabilities are calculated through a stochastic modeling of the diagnostic process, in which a thermodynamic model generates deviations that are induced by the faults. Artificial neural networks recognize these faults. The proposed classification principle has been realized for both, steady state and transient operation of the gas turbine units. The results show that the acceptance of the generalized classification practically does not reduce the diagnosis trustworthiness.
机译:燃气轮机诊断技术通常基于使用实际和预期热力学性能之间的偏差的识别方法。问题在于,偏差取决于实际工作条件。但是,我们的研究表明可以减少这种依赖性。在本文中,我们提出了与操作条件无关的广义故障分类。为了证明这一想法,计算并比较了两种情况下正确诊断的平均概率:建议的分类和基于固定操作条件的传统分类。通过诊断过程的随机模型来计算概率,其中热力学模型会生成由故障引起的偏差。人工神经网络可以识别这些故障。对于燃气轮机单元的稳态和瞬态运行,已经实现了提出的分类原理。结果表明,对通用分类的接受实际上并没有降低诊断的可信度。

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