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Design & optimization of a small wind turbine blade for operation at low wind speed

机译:用于低风速运行的小型风力涡轮机叶片的设计和优化

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A small wind turbine blade was designed and optimized in this research paper. The blade plays an important role, because it is the most important part of the energy absorption system. Consequently, the blade has to be designed carefully to enable to absorb energy with its greatest efficiency. The main objective of this paper is to optimized blade number and selection of tip speed ratio corresponding to the solidity. The power performance of small horizontal axis wind turbines was simulated in detail using blade element momentum methods (BEM). In this paper for wind blade design various factors such as tip loss, hub loss, drag coefficient, and wake were considered. The design process includes the selection of the wind turbine type and the determination of the blade airfoil, twist angle distribution along the radius, and chord length distribution along the radius. A parametric study that will determine if the optimized values of blade twist angle and chord length create the most efficient blade geometry. The 3-bladed, 5-bladed and 7-bladed rotor achieved maximum values of Cp 0.46,0.5 and 0.48 at the tip speed ratio 7, 5 and 4 respectively. It was observed that using BEM theory, maximum Cp varied with strongly solidity and weakly with the blade number. The studies showed that the power coefficient increases upto blade number B = 5, while the blade number if increased above 5 then the power coefficient decreases at operating pitch angle equal to 3°. Highest Cp would have solidity between 4% to 6% for number of blade 3 and design point tip speed ratio of about "7". Highest Cp would have solidity ranging from 5% to 10% for number of blade 5 and 7 and design point tip speed ratio of about 5 and 4 respectively.
机译:本研究论文设计并优化了一个小型风力涡轮机叶片。叶片起着重要的作用,因为它是能量吸收系统中最重要的部分。因此,叶片必须精心设计以能够以最大效率吸收能量。本文的主要目的是优化叶片数量和对应于坚固性的叶尖速比的选择。使用叶片单元动量法(BEM)详细模拟了小型水平轴风力发电机的功率性能。在本文中,对于风叶设计,考虑了各种因素,例如叶尖损失,轮毂损失,风阻系数和尾流。设计过程包括选择风轮机类型和确定叶片翼型,沿半径的扭转角分布以及沿半径的弦长分布。将确定叶片扭曲角和弦长的最佳值是否创建最有效的叶片几何形状的参数研究。 3叶片,5叶片和7叶片转子在叶尖速比7、5和4时分别达到Cp 0.46、0.5和0.48的最大值。观察到,使用BEM理论,最大Cp随坚固度的变化而变化,随叶片数的变化而变化。研究表明,功率系数增加到叶片数量B = 5,而叶片数量增加到5以上时,功率系数在等于3°的工作俯仰角处减小。对于叶片3的数量,最高Cp的坚固度在4%至6%之间,设计点尖端的速比约为“ 7”。对于叶片5和7的数量,最高Cp的坚固性范围为5%到10%,并且设计点尖端的速比分别约为5和4。

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