首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >EXPERIMENTAL INVESTIGATION OF HEAT TRANSFER DEPENDENCY ON CONJUGATE AND CONVECTIVE THERMAL BOUNDARY CONDITIONS IN PIN FIN CHANNEL
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EXPERIMENTAL INVESTIGATION OF HEAT TRANSFER DEPENDENCY ON CONJUGATE AND CONVECTIVE THERMAL BOUNDARY CONDITIONS IN PIN FIN CHANNEL

机译:销鳍通道共轭和对流热边界条件传热率的实验研究

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The present work experimentally quantifies the effects of thermal boundary conditions, i.e., conjugate and convective boundary conditions, on heat transfer performance for the pin fin channel in trailing edge of gas turbine blade. The geometry of pin fin arrays is typical of x/D=y/D=2.5 and H/D=1. For conjugate case, model is constructed with a relatively high conductivity material so that the Biot number of the model matches engine condition. Uniform heat flux is imposed along the external wall of pin fin arrays and highly resolved temperature distributions of internal wall is obtained with steady liquid crystal, meanwhile external temperature is measured through thermocouples. For convective case, model is constructed with low thermal conductivity material to ensure the usage of transient liquid crystal to obtain heat transfer coefficients of the internal wall on the same configuration. Both the measurements are used as boundary conditions to conduct simulation of solid part of pin fin array. Internal and external wall non-dimensional temperature distributions, as well as isothermal lines distribution, of the two cases are compared, results indicate that it will produce large errors in temperature predictions without considering conjugate effect. Further analysis are made about the mechanism of thermal boundary conditions in determining wall temperature, which demonstrates the necessity of taking conjugate heat transfer effect in turbine cooling design.
机译:本工作通过实验量化了热边界条件,即共轭和对流边界条件,对燃气轮机叶片后缘的针翅通道的传热性能的影响。针鳍阵列的几何形状通常为x / D = y / D = 2.5和H / D = 1。对于共轭情况,用相对较高电导率的材料构造模型,以使模型的比奥特数与发动机工况匹配。沿翅片阵列的外壁施加均匀的热通量,并使用稳定的液晶获得内壁高度解析的温度分布,同时通过热电偶测量外部温度。对于对流情况,使用低导热率材料构造模型,以确保使用瞬态液晶来获得相同配置下内壁的传热系数。两次测量均用作边界条件,以进行引脚鳍片阵列的实体部分的仿真。比较了两种情况下的内,外壁无量纲温度分布以及等温线分布,结果表明,在不考虑共轭效应的情况下,它将在温度预测中产生较大的误差。对确定壁温的热边界条件机理进行了进一步分析,这表明在涡轮机冷却设计中必须考虑共轭传热效应。

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