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On-line Heat Rate Monitoring as a Basis for an On-Line Turbine Diagnostic System

机译:在线热率监测作为在线涡轮诊断系统的基础

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In this paper, a turbine on-line performance calculation system is presented. The system was implemented on a 575 MW unit of the Israel Electric Corporation and has been in operation for one year. The system was developed jointly by IEC and Berman Engineering Ltd. The main feature of the described system is the precision of the turbine heat rate calculation. This increased precision of the turbine heat rate calculation was accomplished by utilizing sophisticated statistical techniques, such as parametric and nonparametric regression, robust estimation, special filtration methods, autocorrelation methods, and uncertainty estimation methods. This high precision allows using the calculated heat rate as the main input to the turbine diagnostic system. The selection of turbine heat rate as the main diagnostic input is due to its high sensitivity to efficiency deviations of each turbine subsystem (turbine internal efficiency, condenser cleanliness, regenerative heaters' cleanliness, etc.). However, despite this high sensitivity, the turbine heat rate cannot be used directly without implementing the sophisticated statistical techniques mentioned above because: 1. relatively small variation of the calculated heat rate over the entire turbine load range (only about 3%); 2. the presence of systematic and random measurement errors; 3. low signaloise ratio as a result of the above items. In order to develop the techniques mentioned above, a detailed study of the error characteristics and error propagation was carried out. This study defined the problems which had to be solved in order to achieve an acceptably high precision of the calculation results.
机译:本文提出了一种涡轮机在线性能计算系统。该系统在以色列电力公司的575 MW机组上实施,已经运行了一年。该系统由IEC和Berman Engineering Ltd.共同开发。所述系统的主要特征是涡轮机热效率计算的精度。通过利用复杂的统计技术,例如参数和非参数回归,鲁棒估计,特殊过滤方法,自相关方法和不确定性估计方法,可以提高涡轮机热速率计算的精度。如此高的精度允许将计算出的热量用作涡轮诊断系统的主要输入。选择涡轮机热速率作为主要诊断输入是因为它对每个涡轮机子系统的效率偏差(涡轮机内部效率,冷凝器清洁度,再生加热器的清洁度等)具有很高的敏感性。但是,尽管灵敏度很高,但如果不采用上述复杂的统计技术就不能直接使用涡轮机的热量,这是因为:1.在整个涡轮机负载范围内,计算出的热量的变化相对较小(仅约3%); 2.存在系统的和随机的测量误差; 3.由于上述原因,信噪比低。为了开发上述技术,对错误特性和错误传播进行了详细的研究。这项研究确定了要达到可接受的高精度计算结果所必须解决的问题。

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