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首页> 外文期刊>International Journal of Performability Engineering >Diagnostics and Damage Prediction Model for Heavy Duty Gas Turbine Combustor Hardware Failure
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Diagnostics and Damage Prediction Model for Heavy Duty Gas Turbine Combustor Hardware Failure

机译:重型燃气轮机燃烧室硬件故障诊断与损伤预测模型

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摘要

The focus of this paper is on the degradation of the combustion liner and developing the risk prediction model to predict the damage based on hours, starts and key operating parameters. The multivariate K-means clustering technique is used for classifying the data into different sets of clusters i.e. hours, starts or hours to start ratio vs. deformation. The effect of hour to start ratio on the liner deformation was studied, with the significant clusters obtained from K-means clustering. It is concluded that the hours-to-start ratio (N-ratio) can be a good indicator of component life and provides useful information while modeling the metallurgical damage for component life prediction. The damage growth model is developed using Liner Bulging data and it is shown that N-Ratio is a critical factor in damage prediction as well. The analysis is illustrated with the help of a limited set of combustor liner inspection data for actual heavy-duty gas turbine operation. Future guidelines provided in the paper are expected to spawn additional work in the area of advanced gas turbine diagnostics.
机译:本文的重点是燃烧衬套的退化,并开发风险预测模型以根据小时数,启动次数和关键运行参数来预测损坏。多元K均值聚类技术用于将数据分类为不同的聚类集,即小时,开始或小时开始比率与变形之比。研究了小时开始比对衬板变形的影响,并从K均值聚类获得了显着的聚类。结论是,小时开始时间比(N-ratio)可以很好地指示零件寿命,并在为零件寿命预测的冶金学损伤建模时提供有用的信息。使用衬里膨胀数据开发了损伤增长模型,结果表明N比率也是损伤预测的关键因素。借助于有限的一组燃烧器衬套检查数据来说明该分析,以进行实际的重型燃气轮机运行。本文提供的未来指南有望在先进的燃气轮机诊断领域产生更多的工作。

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