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Design and optimization of airfoils and a 20 kW wind turbine using multi-objective genetic algorithm and HARP_Opt code

机译:使用多目标遗传算法和HARP_Opt代码设计和优化翼型和20 kW风力发电机

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Small wind turbines (SWTs) are ideal for supplying electricity to small remote communities that do not have grid access. However, literature review and trends point out that SWTs are far from fully developed. While larger wind turbines have been researched extensively and perfected, SWTs lack improvements in efficiency and capacity factor. In the present work, airfoil sections for a 20 kW wind turbine were generated using Multi-Objective Genetic Algorithm. The USP07-45XX family of airfoils was designed to achieve maximum lift-to-drag ratio from 4 to 10 degrees angles of attack and to be insensitive to leading edge roughness. The USP07-45XX airfoils showed only slight change during clean and soiled conditions both in experiments and in numerical studies. The optimized airfoils were used in the design of a 20 kW wind turbine. The turbine design and optimization code developed by National Renewable Energy Laboratory (NREL) - HARP_Opt - was used to design and optimize the 20 kW turbine. The turbine was designed using soiled airfoil characteristics of the USP07-45XX family of airfoils. Power curves show cut in speed of 2 m/s and a rated speed of 9 m/s. This gives an annual energy production (AEP) of 4.787 x 10(4) kWh while having leading edge soiling on blades. The high resistance of the airfoil to soiling means that the AEP will not vary from its design value due to the turbine blades getting dirty or soiled. (C) 2018 Elsevier Ltd. All rights reserved.
机译:小型风力涡轮机(SWT)是向没有电网接入的小型偏远社区供电的理想选择。但是,文献综述和趋势表明,SWTs还远远不够完善。尽管已经对大型风力涡轮机进行了广泛的研究和完善,但SWT却缺乏效率和容量因子的提高。在当前工作中,使用多目标遗传算法生成了20 kW风力发电机的翼型截面。 USP07-45XX机翼系列的设计旨在在4至10度的迎角范围内实现最大的升阻比,并且对前缘粗糙度不敏感。在实验和数值研究中,USP07-45XX机翼在清洁和脏污的条件下仅显示出轻微变化。优化的机翼用于20 kW风力涡轮机的设计中。由国家可再生能源实验室(NREL)开发的涡轮机设计和优化代码-HARP_Opt-用于设计和优化20 kW涡轮机。该涡轮机是根据USP07-45XX机翼系列的机翼污染特性设计的。功率曲线显示切入速度为2 m / s,额定速度为9 m / s。这样一来,每年的能源生产量(AEP)为4.787 x 10(4)kWh,同时叶片上的尖端被弄脏。机翼对污染的高抵抗力意味着AEP不会因涡轮叶片变脏或弄脏而偏离其设计值。 (C)2018 Elsevier Ltd.保留所有权利。

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