Quantification of wind turbine energy loss due to leading-edge erosion through infrared-camera imaging, numerical simulations, and assessment against SCADA and meteorological data

被引:12
作者
Panthi, Keshav [1 ]
Iungo, Giacomo Valerio [1 ,2 ]
机构
[1] Univ Texas Dallas, Mech Engn Dept, Wind Fluids & Expt WindFluX Lab, Richardson, TX USA
[2] Univ Texas Dallas, Mech Engn Dept, Wind Fluids & Expt WindFluX Lab, 800 West Campbell Rd,WT 10, Richardson, TX 75080 USA
基金
美国国家科学基金会;
关键词
infrared camera; leading edge erosion; wind farm; wind turbine; THERMOGRAPHIC FLOW VISUALIZATION; PERFORMANCE; BLADES; AERODYNAMICS; ROUGHNESS;
D O I
10.1002/we.2798
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Quantification of the performance degradation on the annual energy production (AEP) of a wind farm due to leading-edge (LE) erosion of wind turbine blades is important to design cost-effective maintenance plans and timely blade retrofit. In this work, the effects of LE erosion on horizontal axis wind turbines are quantified using infrared (IR) thermographic imaging of turbine blades, as well as meteorological and SCADA data. The average AEP loss of turbines with LE erosion is estimated from SCADA and meteorological data to be between 3% and 8% of the expected power capture. The impact of LE erosion on the average power capture of the turbines is found to be higher at lower hub-height wind speeds (peak around 50% of the turbine rated wind speed) and at lower turbulence intensity of the incoming wind associated with stable atmospheric conditions. The effect of LE erosion is investigated with IR thermography to identify the laminar to turbulent transition (LTT) position over the airfoils of the turbine blades. Reduction in the laminar flow region of about 85% and 87% on average in the suction and pressure sides, respectively, is observed for the airfoils of the investigated turbines with LE erosion. Using the observed LTT locations over the airfoils and the geometry of the blade, an average AEP loss of about 3.7% is calculated with blade element momentum simulations, which is found to be comparable with the magnitude of AEP loss estimated through the SCADA data.
引用
收藏
页码:266 / 282
页数:17
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