Hybrid-Lambda: a low-specific-rating rotor concept for offshore wind turbines

Daniel Ribnitzky, Frederik Berger, V. Petrović, Martin Kühn
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引用次数: 1

Abstract

Abstract. We introduce an aerodynamic rotor concept for an offshore wind turbine which is tailored for an increased power feed-in at low wind speeds by a substantial increase in the rotor diameter while maintaining the rated power. The main objective of the conceptual design is to limit the steady-inflow loads (blade flapwise root bending moment (RBM) and thrust) to the maximum values of a reference turbine. The outer part of the blade (i.e. outer 30 % span) is designed for a higher design tip speed ratio (TSR) and a lower axial induction than the inner part. By operating at the high TSR in light winds, the slender outer part fully contributes to the increased power capture. In stronger winds the TSR is reduced and the torque generation is shifted to the inner section of the rotor. Moreover, the blade design efficiently reduces the power losses when the flapwise RBM is limited through peak shaving, below rated wind speed. This is of high importance, given the wind speed distribution at offshore sites. The characteristics of the rotor are first investigated with stationary blade element momentum simulations and further analysed with aeroelastic simulations, considering the flexibility of blades and tower to show that a structural design is feasible even for a blade of this size and complexity. The economic revenue and the cost of valued energy of the turbine are estimated and compared to the IEA 15 MW offshore reference turbine, considering a fictitious wind-speed-dependent feed-in price. Our results for the turbine concept with an increase in rotor diameter by 36 % show that the revenue can be increased by 30 % and the cost of valued energy can be reduced by 16 % compared to the reference turbine.
混合-Lambda:用于近海风力涡轮机的低具体额定转子概念
摘要我们介绍了一种用于海上风力涡轮机的空气动力转子概念,通过大幅增加转子直径,在保持额定功率的情况下,提高低风速时的馈入功率。概念设计的主要目标是将稳流载荷(叶片襟翼根部弯矩 (RBM) 和推力)限制在参考涡轮机的最大值。叶片的外侧部分(即外侧 30% 的跨度)设计为比内侧部分更高的设计叶尖速度比 (TSR)和更低的轴向感应。在风力较小的情况下,细长的外侧叶片以较高的风尖速比运行,可充分提高功率捕获量。在强风中,TSR 会降低,产生的扭矩会转移到转子的内部。此外,在低于额定风速的情况下,通过削峰方式限制襟翼式 RBM 时,叶片设计可有效减少功率损失。考虑到海上风场的风速分布,这一点非常重要。首先通过静态叶片元素动量模拟对转子的特性进行了研究,然后考虑到叶片和塔架的灵活性,进一步通过气动弹性模拟进行了分析,结果表明,即使是这种尺寸和复杂程度的叶片,结构设计也是可行的。我们估算了涡轮机的经济收益和能源价值成本,并与国际能源署 15 兆瓦海上参考涡轮机进行了比较,同时考虑了与风速相关的虚构上网价格。我们对转子直径增加 36% 的涡轮机概念的研究结果表明,与参考涡轮机相比,收入可增加 30%,有价能源成本可降低 16%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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