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The Dynamic Performance of a Composite Blade from a 5kW Wind Turbine Part **II: Predicted Blade Response

机译:5kW风力发电机部件的复合材料叶片的动态性能** II:预测的叶片响应

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This paper presents analytical and computational predictions of the performance of an operating 2.5 m long composite wind turbine blade and compares these predictions with the results of detailed measurements. Part 1 of this paper describes in detail the important aspects of the 5 kW wind turbine, the experimental equipment and data acquisition procedures and presents and discusses some of the results from the experimental data. Here the analytical methodology of Eggleston and Stoddard (1987) and the solutions from the computational wind turbine software package Bladed, were used to predict the performance of the blade for a particular set of experimental conditions. The solutions of Eggleston and Stoddard, where only the first order dynamic equations of a simplified blade model are solved, underestimate the root flapwise moment, streamwise blade tip deflection and lead-lag tip deflection, but gave fairly accurate predictions for the blade lead lag moment. The turbine's structural dynamics within Bladed used a more accurate model of the blade and solved the structural dynamic equations by implementing modal analysis. The results gave root flapwise moment of the same order as those determined from the measurements, close agreement with the measured lead-lag moment, a slight under-prediction of the flapwise tip deflection and large under prediction of the lead-lag tip deflection. The under prediction of the lead-lag deflection by both methods is likely to be due to the uncoupling of the lead-lag and flapping motions, and the unusual shape of the blade close to its root connection.
机译:本文介绍了运行中的2.5 m长复合材料风力涡轮机叶片性能的分析和计算预测,并将这些预测与详细测量结果进行了比较。本文的第1部分详细介绍了5 kW风力发电机的重要方面,实验设备和数据采集程序,并介绍和讨论了来自实验数据的一些结果。在此,Eggleston和Stoddard(1987)的分析方法以及来自计算风轮机软件包Bladed的解决方案用于预测特定条件下的叶片性能。 Eggleston和Stoddard的解决方案仅解决了简化叶片模型的一阶动力学方程,低估了根襟翼动量,沿流向的叶片尖端挠度和超前-滞后尖端挠度,但对叶片超前滞后矩给出了相当准确的预测。叶片式涡轮机的结构动力学使用了更精确的叶片模型,并通过实施模态分析解决了结构动力学方程。结果给出了与测量值相同的根襟翼动量矩,与所测得的超前-滞后力矩紧密吻合,襟翼型叶尖挠度略有不足,而超前滞后叶尖挠度却较大。两种方法对超前-滞后挠度的预测不足可能是由于超前-滞后运动和拍打运动的解耦,以及叶片靠近其根部连接的异常形状。

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