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Design Optimization of a Utility Scale Wind Turbine Blade Using a Genetic Algorithm

机译:基于遗传算法的通用规模风力发电机叶片设计优化。

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Driven by the increasing fossil fuel prices, global warming and climatic change, the world is currently witnessing an increasing development in renewable energy technologies, particularly those of wind energy. As such, engineers around the world are trying to optimize the design of wind turbines to maximize the captured energy while simultaneously minimizing the cost. This work aims to develop a mathematical tool to be used to compare different wind turbine designs and hence to reach the ultimate goal of an optimized wind turbine rotor designed specifically to operate in the Saharan regions of North Africa and the Middle East. As a case study, the main aerodynamic and structural parameters of the NREL 5MW virtual rotor have been optimized for the wind conditions prevalent at the Zaafarana site in Egypt. Specifically, the airfoil chord lengths and twist angles -smoothed using Bezier curves- as well as the layup sequence of the spar caps have been considered i n the optimization process which was carried out using a Genetic Algorithm (GA) developed i n MATLAB and coupled with NREL's FAST Modularization Framework. The results showed that the NREL 5MW wind turbine design optimized for the site specific wind conditions of Zaafarana using airfoil families with low-sensitivity to dust accumulation, achieved a drop of 2.41% of the Levelized Cost of Energy of Energy (LCOE) over that of the baseline design. The developed turbine rotor design is tested for structural integrity commensurate with IEC standards.
机译:在化石燃料价格上涨,全球变暖和气候变化的驱动下,世界目睹了可再生能源技术,尤其是风能技术的不断发展。因此,世界各地的工程师都在尝试优化风力涡轮机的设计,以最大程度地提高捕获的能量,同时又将成本降到最低。这项工作旨在开发一种数学工具,用于比较不同的风力涡轮机设计,从而达到专门为在北非和中东的撒哈拉地区运行而设计的优化风力涡轮机转子的最终目标。作为一个案例研究,NREL 5MW虚拟转子的主要空气动力学和结构参数已针对埃及Zaafarana现场普遍存在的风况进行了优化。具体而言,在优化过程中考虑了使用贝塞尔曲线平滑的翼型弦长和扭转角,以及翼梁盖的摆放顺序,该优化过程是使用在MATLAB中开发的遗传算法(GA)与NREL结合进行的。 FAST模块化框架。结果表明,针对Zaafarana的特定场所风况进行优化的NREL 5MW风力发电机设计使用对粉尘积聚敏感度低的机翼系列,与平均能源成本(LCOE)相比降低了2.41%基线设计。所开发的涡轮转子设计经过了IEC标准的结构完整性测试。

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