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首页> 外文期刊>Applied thermal engineering: Design, processes, equipment, economics >Numerical investigation of influence of different underexcited operations on temperature distribution in the large turbine generator end domain with copper screen
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Numerical investigation of influence of different underexcited operations on temperature distribution in the large turbine generator end domain with copper screen

机译:铜筛网不同未引发的操作对大型汽轮机终极区温度分布影响的数值研究

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Overheating of the complex end parts has become one of the main problems affecting safe and stable turbine generator operation under the underexcited operation. In order to study the temperature distribution in the large turbine generator end domain with copper screen under the different underexcited operations, a 330 MW turbine generator is studied. Three-dimensional fluid-thermal coupling model for the end domain of turbine generator is established. Three-dimensional transient magnetic field of the large turbine generator end domain with copper screen is calculated with 0.85 pf underexcited operation and 0.9 pf underexcited operation. Loss values of the end metal parts from the three-dimensional transient magnetic field are applied to end domain as heat source with 0.85 pf underexcited operation and 0.9 pf underexcited operation. Outlet-pressure values and fan inlet velocity from flow network calculations are applied to the end domain as boundary conditions in the fluid and thermal coupling analysis. The three-dimensional fluid and thermal fields in the turbine generator end domain are calculated with 0.85 pf underexcited operation and 0.9 pf underexcited operation. Distribution of the radial fluid velocity component around the stator winding is determined. Temperature distribution of the end metal parts in the large turbine generator end domain with copper screen is studied with 0.85 pf underexcited operation and 0.9 pf underexcited operation. Temperature calculation results of the copper screen are compared with measured values. Calculation results are in good agreement with measured values.
机译:复杂末端零件的过热已成为在未发布的操作下影响安全稳定的涡轮发电机运行的主要问题之一。为了在不同的未引发的操作下研究大型涡轮发电机端域中的大型涡轮发电机端域中的温度分布,研究了330MW涡轮发电机。建立了涡轮发电机末端域的三维流体热耦合模型。用铜筛的大型涡轮发电机端域的三维瞬态磁场用0.85pf未发迹操作和0.9pf未发迹的操作计算。来自三维瞬态磁场的最终金属部件的损耗值施加到终领域,作为热源,0.85pf未发迹的操作和0.9pf未发迹的操作。从流量网络计算的出口 - 压力值和风扇入口速度被施加到末端域作为流体和热耦合分析中的边界条件。涡轮发电机端域中的三维流体和热场用0.85pf未发迹操作和0.9pf未发迹的操作计算。确定定子绕组周围的径向流体速度分量的分布。使用0.85PF未发迹的操作和0.9PF未发迹的操作,研究了大型涡轮发电机端域中的最终金属部件的温度分布。将铜筛的温度计算结果与测量值进行比较。计算结果与测量值很好。

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