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INVESTIGATIONS AT THE OVER-TIP CASING OF A HIGH PRESSURE TURBINE INCLUDING OFF-DESIGN CONDITIONS AND HEAT TRANSFER CORRELATIONS

机译:高压透平机尖套的研究,包括不合格条件和传热相关性

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Turbine inlet temperature is reaching values far above acceptable material temperatures. Thus the thermally highly loaded components have to be cooled intensively. One of the most thermally loaded components is the over-tip casing.In recent years research on heat transfer at the over-tip casing received a big boost by availability of faster and more accurate measurement techniques. So far the investigations are limited to design condition, no information is available at off-design conditions. This paper aims to contribute to a better understanding of the major phenomena governing heat transfer in the over-tip casing region, including the influence of different operating conditions.Using an HP-turbine at different flow conditions, extended measurements were performed at DLR's wind tunnel for Rotating Cascades (RGG), Gottingen, including the flow field in the tip gap and close to the over-tip casing.The Nusselt correlation for a flat plate was investigated for it's applicability to the over-tip casing. The influence of the incidence angle on the heat transfer levels at the upstream part of the over-tip casing is investigated. Also the influence of the rotational speed on tip-leakage flow and casing heat transfer will be discussed. These results are compared to flat plate heat transfer correlations for design and off-design conditions.
机译:涡轮机入口温度达到的值远高于可接受的材料温度。因此,必须高度冷却热负荷较高的组件。热负荷最大的组件之一是顶盖式外壳。 近年来,通过使用更快,更准确的测量技术,对顶部套管传热的研究得到了极大的推动。到目前为止,调查仅限于设计条件,在非设计条件下没有可用的信息。本文旨在帮助人们更好地理解控制超顶套管区域传热的主要现象,包括不同工况的影响。 在不同的流量条件下使用HP涡轮机,在哥廷根DLR的旋转梯级(RGG)的风洞中进行了扩展的测量,包括叶尖间隙和靠近叶尖外壳的流场。 研究了平板的Nusselt相关性,因为它适用于尖顶套管。研究了入射角对顶壳上游部分传热水平的影响。还将讨论转速对尖端泄漏流和套管传热的影响。将这些结果与设计和非设计条件下的平板传热相关性进行比较。

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