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Reduction of Wind Turbine Noise using Optimized Airfoilsand Trailing-Edge Serrations

机译:使用优化的缺水袋减少风力涡轮机噪声和后缘锯齿

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Acoustic field measurements were carried out on a 94-m diameter 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. Due to 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 most 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 (i.e. high tip loading). Nevertheless, average overall noise reductions of 0.5 dB and 3.2 dB are obtained for the optimized and for the serrated blade, respectively.
机译:在直径为94米的三刃风力涡轮机上进行声场测量,其中一个标准刀片,一个带有后缘锯齿的刀片,以及一个具有优化翼型形状的叶片。用于从涡轮机的大约一个转子直径的距离位于涡轮机的距离处的大型水平麦克风阵列定位并定量转子平面中的噪声源和各个叶片。声源图表明,对于阵列位置的观察者,基线叶片的主导源是来自刀片舷外区域的后缘噪声。由于对流放大和方向性,实际上在叶片的向下运动期间产生所有这些噪声,这导致叶片通过过程中典型的摇噪声。两个改进的刀片都在低频下显示出显着的后缘降噪,这对于锯齿状刀片最突出。然而,改进的刀片还在高频下显示尖端噪声,其主要在旋转的向上部分辐射,并且在低风速下最重要(即高尖端装载)。然而,为优化和锯齿状刀片分别获得0.5dB和3.2dB的平均整体噪声减少。

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