首页> 外国专利> FLAPWISE FATIGUE TESTING METHOD AND DUAL-AXIS RESORNACE FATIGE TESTING METHOD OF A WIND TURBINE BLADE USING EXCITATION IN HORIZONTAL DIRECTION

FLAPWISE FATIGUE TESTING METHOD AND DUAL-AXIS RESORNACE FATIGE TESTING METHOD OF A WIND TURBINE BLADE USING EXCITATION IN HORIZONTAL DIRECTION

机译:水平方向上激励的风轮机叶片襟翼疲劳试验方法及双轴共振疲劳试验方法

摘要

The present invention relates to a flap-directional fatigue test method of a wind turbine blade using horizontal excitation and a biaxial resonance test fatigue test method capable of remarkably reducing a test period by removing a role of an exciter with respect to gravity in an existing flap-directional fatigue test method vertically performed and exciting the blade at a huge amplitude using the exciter with a low load capacity by mounting the blade to a fixing device to make the edge of the blade about perpendicular to the ground and exciting the blade about a horizontal direction. To achieve the same, the flap-directional fatigue test method of the wind turbine blade to reduce the test period by increasing the amplitude of the blade includes a first step (S110) of fixing the blade on a fixing device at 80 to 100 degrees between the edge of the blade and the ground surface to be a cantilever shape; a second step (S120) of mounting the exciter to the surface of the blade at -10 to +10 degrees between the edge of the blade and a line or a face where a moving mass moves; and a third step (S130) of performing the test by exciting the blade at -10 degrees to +10 degrees around resonance frequency of the overall blade structure using the exciter.
机译:本发明涉及一种使用水平激励的风力涡轮机叶片的襟翼方向疲劳测试方法以及一种双轴共振测试疲劳测试方法,该方法能够通过消除现有襟翼中的激励器相对于重力的作用而显着缩短测试时间。方向疲劳测试方法垂直执行,并通过将叶片安装到固定装置上以使叶片的边缘垂直于地面并沿水平方向激发叶片,使用低负载的激振器以大幅度激发叶片。方向。为此,通过增加叶片的振幅来减少测试周期的风力涡轮机叶片的襟翼方向疲劳测试方法包括将叶片以80至100度之间的角度固定在固定装置上的第一步(S110)。叶片的边缘和地面为悬臂形状;第二步骤(S120),将激振器以叶片边缘与运动质量移动的线或面之间的-10至+10度安装在叶片表面。第三步骤(S130),通过使用激振器,以整个叶片结构的共振频率为中心,在-10度至+10度的范围内激发叶片来进行测试。

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