首页> 外文期刊>Journal of Sound and Vibration >Extracting full-field dynamic strain on a wind turbine rotor subjected to arbitrary excitations using 3D point tracking and a modal expansion technique
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Extracting full-field dynamic strain on a wind turbine rotor subjected to arbitrary excitations using 3D point tracking and a modal expansion technique

机译:使用3D点跟踪和模态展开技术提取受到任意激励的风轮机转子上的全场动态应变

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Health monitoring of rotating structures such as wind turbines and helicopter rotors is generally performed using conventional sensors that provide a limited set of data at discrete locations near or on the hub. These sensors usually provide no data on the blades or inside them where failures might occur. Within this paper, an approach was used to extract the full field dynamic strain on a wind turbine assembly subject to arbitrary loading conditions. A three-bladed wind turbine having 2.3-m long blades was placed in a semi-built-in boundary condition using a hub, a machining chuck, and a steel block. For three different test cases, the turbine was excited using (1) pluck testing, (2) random impacts on blades with three impact hammers, and (3) random excitation by a mechanical shaker. The response of the structure to the excitations was measured using three-dimensional point tracking. A pair of high-speed cameras was used to measure displacement of optical targets on the structure when the blades were vibrating. The measured displacements at discrete locations were expanded and applied to the Finite element model of the structure to extract the full field dynamic strain. The results of the paper show an excellent correlation between the strain predicted using the proposed approach and the strain measured with strain gages for each of the three loading conditions. The approach used in this paper to predict the strain showed higher accuracy than the digital image correlation technique. The new expansion approach is able to extract dynamic strain all over the entire structure, even inside the structure beyond the line of sight of the measurement system. Because the method is based on a non-contacting measurement approach, it can be readily applied to a variety of structures having different boundary and operating conditions, including rotating blades. (C) 2015 Elsevier Ltd. All rights reserved.
机译:通常使用常规传感器对旋转结构(例如,风力涡轮机和直升机旋翼)进行健康监控,该传感器在轮毂附近或轮毂上的离散位置提供有限的数据集。这些传感器通常在刀片或刀片内部不提供任何可能发生故障的数据。在本文中,采用一种方法来提取风力涡轮机组件在任意载荷条件下的全场动态应变。使用轮毂,机械卡盘和钢块,将具有2.3 m长叶片的三叶片风力涡轮机置于半内置边界条件下。对于三个不同的测试案例,使用(1)拔动测试,(2)用三个冲击锤对叶片的随机冲击和(3)机械振动器的随机激励来激励涡轮。使用三维点跟踪测量了结构对激发的响应。当叶片振动时,使用一对高速相机测量光学目标在结构上的位移。扩展了在离散位置处测得的位移并将其应用于结构的有限元模型,以提取全场动态应变。论文的结果表明,在三种载荷条件下,使用该方法预测的应变与使用应变计测得的应变之间具有极好的相关性。本文中用于预测应变的方法显示出比数字图像相关技术更高的准确性。新的扩展方法能够提取整个结构的动态应变,甚至是超出测量系统视线的结构内部。由于该方法基于非接触式测量方法,因此可以轻松地应用于具有不同边界和操作条件的各种结构,包括旋转叶片。 (C)2015 Elsevier Ltd.保留所有权利。

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