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Influence of the End Ventilation Structure Change on the Temperature Distribution in the End Region of Large Water–Hydrogen–Hydrogen Cooled Turbogenerator

机译:大型水氢氢冷汽轮发电机端部通风结构变化对温度分布的影响

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Flow network was built according to the ventilation structural characteristics of a 330?MW large water–hydrogen–hydrogen cooled turbogenerator. The variation of the fan inlet velocities, and the flow rates and pressures (boundary conditions) of each end region outlet were obtained, respectively, with different air gap spacer heights and different shelter board widths between the long press fingers by flow network method, and the relative law was analyzed. In order to study the influence of the changed end ventilation structures on the temperature distribution of the end parts, 3-D transient electromagnetic field in the turbogenerator end was calculated, and the eddy current losses (heat sources) of the end parts were gained by the finite-element method. Meanwhile, the fluid and thermal mathematics and physical models of the end region were given. Using the finite-volume method, the influence of the changed end ventilation structures on the surface heat transfer coefficient and the temperature of end parts was researched. It shows that the proper changes in the air gap spacer height and shelter board width decrease the copper shield temperature and result in a reasonable temperature distribution in the end parts. It provides the useful reference for the further design of the large turbogenerators.
机译:根据330?MW大型水-氢-氢冷却涡轮发电机的通风结构特征建立了流网。通过流网法分别获得了长压指之间不同的气隙间隔高度和不同的遮蔽板宽度,分别得到了风扇入口速度的变化,以及每个端部区域出口的流量和压力(边界条件),以及对相关规律进行了分析。为了研究端部通风结构的变化对端部温度分布的影响,计算了汽轮发电机端部的3-D瞬变电磁场,并通过以下方法获得了端部的涡流损失(热源):有限元法。同时,给出了端部区域的流体和热数学和物理模型。采用有限体积法研究了端部通风结构的变化对表面传热系数和端部温度的影响。结果表明,气隙垫片高度和防护板宽度的适当变化会降低铜屏蔽层的温度,并在端部产生合理的温度分布。它为大型涡轮发电机的进一步设计提供了有用的参考。

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