高堵塞横流涡轮阵列性能评价的实验技术

Aidan Hunt, B. Polagye
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引用次数: 0

摘要

横流涡轮机显示出从水流中提取能量的巨大希望,因为它们的矩形投影面积允许它们实现高阻塞。随着涡轮的堵塞比(转子投影面积与通道横截面积之比)的增加,由于自由流中的动能和势能都转化为机械能,涡轮的效率和结构载荷也随之增加。对于部署在河流或潮汐通道中的一组涡轮机,由于水位的每日或季节性波动,以及单个涡轮机因维护而停用时,阵列阻塞比将会变化。因此,了解阵列的性能特征如何随着约束的变化而变化是有实际意义的。在这里,我们描述了实验室规模的双涡轮阵列在循环水通道中不同程度的约束下的性能。阵列阻塞比从30%到60%不等,这是在自然通道中可能实现的上限。考虑了两种改变阻塞的实验方法:1)通过改变水深来改变通道横截面积,2)通过改变叶片跨度来改变阵列投影面积。在所有测试的堵塞比中,基于弦的标称雷诺数(4.0 x 104)和基于深度的标称弗劳德数(0.22)保持不变,而基于淹没的弗劳德数被最小化,以避免在测试堵塞的上端涡轮转子通风。在每个堵塞比下,涡轮性能在一个反向旋转的锁相控制方案下通过一系列的叶尖速比进行评估,其中涡轮以相同的恒定速度在相反的方向上旋转,它们之间有恒定的角相位偏移Δθ。我们的工作重点是Δθ = 0°,在这种情况下,一对涡轮机的侧向力和反作用力相等且相反,这有利于支撑结构的设计。随着阵列堵塞比的增加,我们观察到阵列性能和推力系数的显著增加,以及阵列产生功率的叶尖速比范围的增加。在最高约束条件下,峰值功率系数大于1,推力系数大大高于常规阵列设计。我们观察了相同堵塞比但不同叶跨的阵列功率和推力系数之间的差异。我们将更长的叶片跨度的更高性能归因于两个转子之间寄生支撑结构损失的相对大小的差异,以及自由表面效应。此外,我们通过叶片级性能的估计来探讨计算这些性能差异的技术的有效性。总的来说,我们的研究结果为理解横流涡轮阵列性能随阵列堵塞比的变化提供了坚实的基础,并突出了横流涡轮实验设计的注意事项。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental techniques for evaluating the performance of high-blockage cross-flow turbine arrays
Cross-flow turbines show great promise for extracting power from water currents since their rectangular projected area allows them to achieve high blockage. As a turbine’s blockage ratio—the ratio of the rotor projected area to the channel cross-sectional area—increases, its efficiency and structural loading increase since both kinetic and potential energy in the freestream are converted to mechanical power. For an array of turbines deployed in a river or tidal channel, the array blockage ratio will vary due to daily or seasonal fluctuations in the water level, as well as when individual turbines are deactivated for maintenance. Consequently, understanding how the performance characteristics of the array change as confinement is varied is of practical interest. Here, we characterize the performance of a laboratory-scale two-turbine array at various levels of confinement in a recirculating water channel. The array blockage ratio was varied from 30% to 60%—the upper end of what might be realizable in a natural channel. Two experimental approaches for varying the blockage were considered: 1) altering the channel cross-sectional area via a change in water depth, and 2) altering the array projected area by changing the blade span. Across all tested blockage ratios, the nominal chord-based Reynolds number (4.0 x 104) and nominal depth-based Froude number (0.22) were held constant, and the submergence-based Froude number was minimized to avoid ventilation of the turbine rotors at the upper end of the tested blockages. At each blockage ratio, the turbine performance was evaluated across a range of tip-speed ratios under a counter-rotating, phase-locked control scheme, wherein the turbines rotate at the same, constant speed but in opposite directions, with a constant angular phase offset, Δθ, between them. We focus this work on Δθ = 0°, an operating case in which the lateral forces and reaction torques for a pair of turbines are equal and opposite, which is advantageous for support structure design. As the array blockage ratio is increased, we observe significant increases in the array performance and thrust coefficients, as well as an increase in the range of tip-speed ratios over which the array produces power. For the highest confinements, peak power coefficients exceed unity and thrust coefficients are substantially higher than in conventional array designs. We observe disparities between the power and thrust coefficients for arrays with the same blockage ratio, but different blade spans. We attribute the higher performance for longer blade spans to differences in the relative magnitude of parasitic support structure losses between the two rotors, as well as free surface effects. Further, we explore the effectiveness of techniques for accounting for these performance differences through the estimation of blade-level performance. Overall, our results provide a solid foundation for understanding how the performance of cross-flow turbine arrays change as a function of the array blockage ratio, and highlight considerations for the design of cross-flow turbine experiments.
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