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Measurements of Tip Vortex Characteristics and the Effect of an Anti-Cavitation Lip on a Model Kaplan Turbine Blade

机译:Kaplan型涡轮叶片的尖端涡流特性测量和抗气蚀唇的影响

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摘要

Motivated by the problem of cavitation erosion, the position and strength of the roll-up vortex on the suction side of a Kaplan-type turbine blade with various endings is investigated. Measurements are made on different models with simplified two-dimensional geometries using mainly particle image velocimetry. It is found that the greatest danger of cavitation erosion exists when the casing of the turbine is of the "semi-spherical" type, so that there is a large and closing clearance gap at the leading edge of the blade. Furthermore, the anti-cavitation lip used in this study is shown to be ineffective at increasing the distance of the vortex from the blade, although it does reduce the circulation of the vortex and presumably the danger of cavitation. Our measurements are found to be in good agreement with existing models for the position of the vortex when appropriately interpreted.
机译:受空化腐蚀问题的影响,研究了具有各种末端的卡普兰型涡轮叶片吸力侧上的涡旋的位置和强度。主要使用粒子图像测速技术在具有简化的二维几何形状的不同模型上进行测量。已经发现,当涡轮机的壳体为“半球形”类型时,存在气蚀的最大危险,因此在叶片的前缘处存在大的闭合间隙。此外,本研究中使用的抗气蚀唇口虽然不能减少涡流的循环并可能会产生气蚀的危险,但在增加涡旋与叶片之间的距离方面无效。经适当解释,我们的测量结果与涡流位置的现有模型非常吻合。

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