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TRAILING EDGE MODIFICATIONS FOR WIND TURBINE AIRFOIL

机译:风轮机翼的尾缘修改

摘要

A wind turbine blade airfoil trailing edge (TE) with a first waveform profile (44B, 44C, 44E) as seen from behind, formed by ruffles or alternating ridges (21) and valleys (22) formed on the airfoil (20) and ending at the trailing edge. The trailing edge may further include a second waveform profile (48B, 48C, 48E) as seen from above, resulting from serrations formed by an oblique termination plane (32B) of the trailing edge or by other geometry. The ridges and/or serrations may be asymmetric (44E, 48E) to increase a stall fence effect of the ridges on the suction side (SS) of the trailing edge. The first and second waveforms may have the same period (44B, 48B) or different periods (44C, 48C).
机译:从后面看具有第一波形轮廓(44B,44C,44E)的风轮机叶片翼型后缘(TE),该翼型后缘由形成在翼型(20)上并形成端部的褶皱或交替的脊(21)和谷(22)形成在后缘。从后方看,后缘还可以包括第二波形轮廓(48B,48C,48E),该第二波形轮廓是由后缘的倾斜终止平面(32B)或其他几何形状形成的锯齿产生的。脊和/或锯齿可以是不对称的(44E,48E),以增加在后缘的吸力侧(SS)上的脊的失速栅栏效应。第一波形和第二波形可以具有相同的周期(44B,48B)或不同的周期(44C,48C)。

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