首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >COMBINED EFFECTS OF PERFORATED BLOCKAGES AND PIN FINS IN A TRAILING EDGE INTERNAL COOLING DUCT
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COMBINED EFFECTS OF PERFORATED BLOCKAGES AND PIN FINS IN A TRAILING EDGE INTERNAL COOLING DUCT

机译:尾部内部冷却管道中渗透性阻塞和销钉的综合效应

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Pin fin arrays and perforated blockages are both important methods for gas turbine trailing edge cooling. Perforated blockages result in higher heat transfer coefficients with larger pressure loss penalty. For enhanced heat transfer with medium pressure loss, we installed a perforated blockage at the inlet of pin fin arrays and studied the combined effects between impingement and pin fin. Heat transfer coefficients were measured with the transient liquid crystal method and the lumped capacitance model. Flow field was investigated using the RNG k-e model. Six configurations with different flow area ratio, hole distribution and hole aspect ratio were examined at duct Reynolds number between 9,000 and 20,000. The results reveal that under impingement condition, Nusselt number for the first two rows of pin fins near the stagnation point is 2~3 times larger than the baseline case without impingement. The most important parameter for heat transfer and friction loss is the area ratio. The average Nusselt number increases 20%~50% with impingement, and the friction factor increases 4~20 times. Heat transfer and friction loss for the combined configurations satisfy the correlation Nu=0.1766Re~(0.702)f~(0.188).
机译:针鳍阵列和穿孔堵塞都是燃气轮机后缘冷却的重要方法。穿孔的阻塞导致更高的传热系数和更大的压力损失损失。为了在中等压力损失的情况下增强传热效果,我们在针鳍阵列的入口处安装了穿孔阻塞物,并研究了撞击和针鳍之间的综合作用。用瞬态液晶法和集总电容模型测量传热系数。使用RNG k-e模型研究了流场。在管道雷诺数在9,000和20,000之间的情况下,检查了六个具有不同流动面积比,孔分布和孔长宽比的配置。结果表明,在撞击条件下,停滞点附近前两排针状鳍的努塞尔特数是无撞击情况下基线的2〜3倍。传热和摩擦损失最重要的参数是面积比。碰撞时平均努塞尔数增加20%〜50%,摩擦系数增加4〜20倍。组合构型的传热和摩擦损失满足相关系数Nu = 0.1766Re〜(0.702)f〜(0.188)。

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