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SIMULATION OF THE INTERACTION OF LABYRINTH SEAL LEAKAGE FLOW AND MAIN FLOW IN AN AXIAL TURBINE

机译:迷路密封泄漏流动与轴向汽轮机主流的仿真

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This paper presents the simulation of the flow in a 1.5 stage low-speed axial turbine with shrouded rotor blades and focuses on the interaction of the labyrinth seal leakage flow with the main flow. The presented results were obtained using the Navier-Stokes code ITSM3D developed at University of Stuttgart. A comparison of the computational results with experimental data of this test case gained at Ruhr-Universitaet Bochum verifies that the flow solver is capable of reproducing the leakage flow effects to a sufficient extent. The computational results are used to examine the influence of the leakage flow on the flow field of the turbine. By varying the clearance height of the labyrinth in the simulations, the impact of the re-entering leakage flow on the main flow is studied. As demonstrated in this paper, leakage flow not only introduces mixing losses but can also dominate the secondary flow and induce severe losses. In agreement with the experimental data the computational results show that at realistic clearance heights the leakage flow gives rise to negative incidence over a considerable part of the downstream stator which causes the flow to separate.
机译:本文介绍了1.5级低速轴向涡轮机的流动模拟,带罩转子叶片,专注于迷宫密封泄漏流与主流的相互作用。使用在斯图加特大学开发的Navier-Stokes代码ITSM3D获得了所提出的结果。计算结果与在Ruhr-Universitaet波鸿的该测试用例的实验数据的比较验证了流动求解器能够在足够的程度上再现泄漏流动效应。计算结果用于检查漏流对涡轮机的流场的影响。通过改变模拟中迷宫的间隙高度,研究了重新进入泄漏流对主流的影响。如本文所示,泄漏流不仅引入混合损失,而且还可以占据二次流动并引起严重损失。在实验数据方面,计算结果表明,在现实的间隙高度处,泄漏流动在下游定子的相当大部分中产生负发射,这导致流动分离。

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