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Reduction of Wind Turbine Noise Using Optimized Airfoils and Trailing-Edge Serrations

机译:使用优化的翼型和后缘锯齿减少风轮机噪声

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Acoustic field measurements were carried out on a 94-m-diam three-bladed wind turbine with one standard blade, one blade with trailing-edge serrations, and one blade with an optimized airfoil shape. A large horizontal microphone array, positioned at a distance of about one rotor diameter from the turbine, was used to locate and quantify the noise sources in the rotor plane and on the individual blades. The acoustic source maps show that for an observer at the array position, the dominant source for the baseline blade is trailing-edge noise from the blade outboard region. Because of convective amplification and directivity, practically all of this noise is produced during the downward movement of the blade, which causes the typical swishing noise during the passage of the blades. Both modified blades show a significant trailing-edge noise reduction at low frequencies, which is more prominent for the serrated blade. However, the modified blades also show tip noise at high frequencies, which is mainly radiated during the upward part of the revolution and is most important at low wind speeds due to high tip loading. Nevertheless, average overall noise reductions of 0.5 and 3.2 dB are obtained for the optimized blade and the serrated blade, respectively.
机译:声场测量是在直径为94 m的三叶片风力涡轮机上进行的,该叶片具有一个标准叶片,一个具有后缘锯齿的叶片和一个具有优化翼型形状的叶片。大型水平传声器阵列位于距涡轮约一个转子直径的位置,用于定位和量化转子平面内以及各个叶片上的噪声源。声源图显示,对于阵列位置的观察者而言,基准叶片的主要来源是来自叶片外侧区域的后缘噪声。由于对流放大和方向性,实际上所有这些噪声都是在叶片向下运动期间产生的,这在叶片通过过程中会引起典型的sw声。两种改进型刀片在低频时均显示出明显的后缘降噪效果,这对于锯齿形刀片而言更为突出。然而,改进的叶片还在高频处显示叶尖噪声,该噪声主要在旋转的向上部分期间辐射,并且由于高叶尖负载而在低风速时最重要。不过,对于优化刀片和锯齿刀片,平均总体噪声降低分别为0.5和3.2 dB。

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