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

机译:不同叶片载荷对带叶片的二级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:涡轮叶片开发中的一个重要目标是提高效率,以实现能源的优化利用。为此,需要对流动现象有详细的了解。本文提出了一个实验研究,研究了不同叶片载荷对流场和泄漏流的影响。研究是在亚琛工业大学蒸汽与燃气轮机研究所的两级轴流式涡轮机上进行的。在入口和出口以及两级之间已经确定了不同叶片负载的流场。因此,可以研究每个阶段出口处的不均匀性,具体取决于叶片负载。已经通过使用二次动能系数评估了出口处的均匀性,因此强调了通道涡流的形成。此外,已经估计了载荷对泄漏质量流量和泄漏主流相互作用的影响。因此,在第一带罩的转子叶片的迷宫式密封件内的每个空腔中的压力损失被检测到。此外,已经确定了对不同负载的效率的影响。在每个阶段之后通过使用5孔探针和温度探针来确定效率。上面提到的研究是在2D刀片轮廓上进行的,并作为将来轮廓墙端壁研究的基准。端壁轮廓叶片的目标应减少通道涡流,并降低通道涡流和下倾角,最终导致从平台流出更均匀。

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