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ANALYSIS AND EVALUATION OF THE IMPACT OF DIFFERENT BLADE LOADINGS ON A 2-STAGE TURBINE WITH SHROUDED BLADES

机译:不同刀片装载对2阶段涡轮机的影响分析与评估

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An important goal in the development of turbine bladings is to increase the efficiency in order to achieve an optimized use of energy resources. For that purpose a detailed understanding of flow phenomena is required. This paper presents an experimental investigation of the impact of varying blade loadings on the flow field and leakage flow. The investigations were conducted on a 2-stage axial turbine at the Institute of Steam- and Gas Turbines, RWTH Aachen University. The flow field for different blade loadings has been determined at the inlet and outlet as well as between the two stages. Consequently, the inhomogeneity at the outlet of each stage, depending on the blade loading, may be investigated. The homogeneity at the outlet has been evaluated by using the secondary kinetic energy coefficient and the formation of the passage vortex has therefore been emphasized. Furthermore, the loading impact on the leakage mass flow and the leakage main flow interaction has been estimated. On this account, the pressure loss in each cavity within the labyrinth seal of the first shrouded rotor blades is detected. The impact on the efficiency of different loadings has moreover been determined. The efficiency has been ascertained by using 5-hole probes and temperature probes after each stage. The investigations mentioned above have been conducted on a 2D-blade profile and serve as a baseline for future profiled end wall studies. The goal of the endwall contoured blades shall reduce the passage vortex and with it, the under- and overturning which ultimately leads to a more homogeneous outflow from the stage.
机译:涡轮炸药开发的一个重要目标是提高效率,以实现优化的能源利用。为此,需要详细了解流现象。本文介绍了不同叶片载荷对流场和泄漏流动影响的实验研究。在亚琛大学蒸汽和燃气轮机研究所的一级轴流涡轮机上进行了调查。在入口和出口以及两个阶段之间确定了不同刀片装载的流场。因此,可以研究每个阶段的出口处的不均匀性,这取决于叶片载荷。因此,通过使用次要动能系数评估出口处的均匀性,因此强调了通道涡流的形成。此外,已经估计了对泄漏质量流量的负载影响和泄漏主流相互作用。在此帐户中,检测到第一罩转子叶片的迷宫密封内的每个腔内的压力损失。此外,对不同载荷效率的影响已经确定。通过在每个阶段使用5孔探头和温度探针来确定效率。上述研究已经在2D叶片轮廓上进行,并作为未来异形墙研究的基线。端壁轮廓叶片的目标应减少通道涡流,并随后推翻,最终导致阶段更加均匀的流出。

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