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The Achieving of Gas Turbine's Gas Path Fault Criterion

机译:燃气轮机气路故障准则的实现

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In this paper the mathematical model of a certain kind of gas turbine was built based on parts thermodynamic characteristics and matching of components considering outside and boundary conditions. On the basis of this model, small deviation equations were produced by using small deviation method. Then, the standard fault model was acquired through introducing fault factors into the small deviation equations, which, further imported with actual operating data, educed the small deviation influence coefficient matrix. This matrix, combined with gas path fault variable criterion of performance parameters, would then ascertain the membership size relationship between typical gas path faults and measurement parameters. Finally, the typical gas path fault variable criterion of measurement parameters was deduced, which lays the foundation for gas path fault diagnosis of gas turbine.
机译:本文基于零件的热力学特性和考虑外部和边界条件的零件匹配,建立了某种燃气轮机的数学模型。在此模型的基础上,采用小偏差方法产生了小偏差方程。然后,通过将故障因素引入小偏差方程中,获得标准故障模型,然后将其与实际运行数据一起输入,从而得出小偏差影响系数矩阵。然后,该矩阵与性能参数的气路故障变量准则相结合,将确定典型气路故障与测量参数之间的隶属关系。最后推导了典型的测量参数气路故障变量判据,为燃气轮机气路故障诊断奠定了基础。

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