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An experimental study of heat transfer around turbine airfoils with closed-loop cooling.

机译:带有闭环冷却的涡轮机翼型周围传热的实验研究。

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Closed-Loop cooling has been identified as one of the promising cooling schemes for the next generation gas turbine systems. The closed-loop cooling design collects the spent coolants and directs them to be recovered to do useful work in engine cycle. Due to the requirement of the closed-loop cooling and adoption of innovative cooling methods, the geometric configuration of a closed-loop cooling design is usually complicated. The complexity induces the heat transfer and flow uncertainties and necessitates the detailed heat transfer study for the cooling design. The present research was designed to examine heat transfer of innovative closed-loop cooling designs of an advanced gas turbine system. A heat transfer measurement system employing the Thermochromic Liquid Crystal (TLC) has been developed in order to study detailed heat transfer of the complicated cooling designs. A hybrid technique has been proposed to combine two models: lumped heat capacity model and one-dimension model. The technique has been successfully demonstrated to be a reliable means by studying heat transfer phenomenon on pin fin arrays. Pin fin arrays, sometimes termed pedestals, are widely used in modern gas turbines to provide heat transfer enhancement. In addition, the study on pin fins array revealed effects of heat transfer by two increasingly important, yet not much being explored geometric parameters: shape of pin fin element and gap atop pin fin array. Heat transfer study using the measurement system has revealed detailed heat transfer distribution and eliminated heat transfer uncertainties for five scaled Perplex models of the most crucial designs in the closed-loop cooling system. This study has also demonstrated the improvement in design practice with assistance of the developed system. For a design that relies on the unverified data sets and correlation, the system provides a means to eliminate the uncertainties and provide prompt feedback to designers for modification of the design.
机译:闭环冷却已被认为是下一代燃气轮机系统的有希望的冷却方案之一。闭环冷却设计收集了用过的冷却液,并引导它们回收以在发动机循环中做有用的工作。由于需要闭环冷却并采用创新的冷却方法,因此闭环冷却设计的几何结构通常很复杂。复杂性导致了传热和流量的不确定性,因此有必要对冷却设计进行详细的传热研究。本研究旨在检查先进燃气轮机系统的创新型闭环冷却设计的热传递。为了研究复杂冷却设计的详细传热,已经开发了一种采用热致变色液晶(TLC)的传热测量系统。已经提出了一种混合技术来结合两个模型:集总热容量模型和一维模型。通过研究针翅阵列上的传热现象,该技术已成功证明是可靠的手段。针翅阵列有时被称为基座,被广泛用于现代燃气轮机中以增强热传递。另外,对销鳍阵列的研究揭示了两个越来越重要但尚未探讨的几何参数:销鳍元件的形状和销鳍阵列顶部的间隙对传热的影响。使用测量系统进行的传热研究揭示了详细的传热分布,并消除了闭环冷却系统中最关键设计的五个比例Perplex模型的传热不确定性。这项研究还证明了在已开发系统的帮助下设计实践的改进。对于依赖于未经验证的数据集和相关性的设计,该系统提供了一种消除不确定性的方法,并为设计人员提供了及时反馈以修改设计。

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