从风洞试验分析新研制的椭圆叶片Savonius转子轴和端板的影响

N. Alom, Nitish Kumar, U. Saha
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引用次数: 3

摘要

近年来,基于阻力的垂直轴风力涡轮机转子由于其性能潜力和可靠性在海上应用中获得了越来越多的兴趣。其结构简单、易于制造、维护成本低等优点引起了研究者对其进一步改进设计的关注。然而,这种类型的转子仍然存在效率低于基于升力的Darrius和水平轴风力涡轮机转子的问题。最近开发的椭圆叶片Savonius转子显示出其更有效地收集风能的潜力。但是,该转子的展弦比、重叠比、叶片数、轴数、端板数等几何参数,以及雷诺数、升力、阻力系数等气动参数都需要进行优化,以进一步提高其性能。本文通过风洞试验,分析了新研制的椭圆叶片垂直轴Savonius风力发电机转子轴和端板的影响。在一定的叶尖速比范围内进行了实验,以找出两种单独情况下双叶片转子系统的转矩和功率系数,即带轴转子和带端板转子。为了进行直接比较,还得到了同一转子不带轴和不带端板的实验数据。风洞试验结果表明,带端板转子的功率系数提高了26.31%。
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Analyzing the Effect of Shaft and End-Plates of a Newly Developed Elliptical-Bladed Savonius Rotor From Wind Tunnel Tests
In recent times, drag-based vertical-axis wind turbine rotors have gained increasing interests in offshore applications because of their performance potential and reliability. Their advantages like simplicity, easier manufacture and lower maintenance cost have attracted the researcher’s attention toward improving their design further. However, this type of rotor is still suffering from lower efficiency than the lift-based Darrius and the horizontal-axis wind turbine rotors. A recently developed elliptical-bladed Savonius rotor has shown its potential to harvest wind energy more efficiently. However, the geometric parameters of this rotor such as aspect ratio, overlap ratio, number of blades, shaft and end plates, the aerodynamic parameters such as Reynolds number, lift and drag coefficients are needed to be optimized for further improvement of its performance. In the present investigation, the wind tunnel tests have been conducted to analyze the effect of shaft and end-plates of a newly developed elliptical-bladed vertical-axis Savonius wind turbine rotor. Experiments have been conducted over a range of tip speed ratios to find the torque and power coefficients of a two-bladed rotor system for two individual cases viz., the rotor with a shaft and the rotor with end-plates. In order to have a direct comparison, the experimental data are also obtained for the same rotor without the shaft and without the end-plates. The wind tunnel tests have demonstrated an improvement of power coefficient by 26.31% for the rotor with the end plates.
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