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Blade Element Momentum Study of Rotor Aerodynamic Performance and Loading for Active and Passive Microjet Systems

机译:主动和被动微喷系统叶片气动性能和载荷的叶片元动量研究

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摘要

This study investigates the performance of microjets for load reduction on the NREL-5 MW wind turbine and identifies optimal system parameters. Microjets provide blowing normal to the blade surface and can rapidly increase or decrease lift on a blade section, enabling a wind turbine to respond to local, short-term changes in wind condition. As wind turbine rotors become larger, control methods that act on a single blade or blade section are increasingly necessary to reduce critical fatigue and extreme loads. However, microjets require power to operate, and thus, it is crucial that the fatigue reduction justifies any energy input to the system. To examine the potential for fatigue reduction of a range of potential microjet system configurations, a blade element momentum (BEM) code and a flow energy solver were used to estimate the energy input and the change in primary fatigue metrics. A parametric analysis was conducted to identify the optimal spanwise position and length of the microjets over a range of air mass flow rates. Both active and passive air supply methods were considered. A passive microjet system applied to the NREL 5-MW rotor produced a 3.7% reduction in the maximum flapwise root bending moment (FRBM). The reduction in the peak bending moment increased to 6.0% with a 5 kPa blower that consumes approximately 0.1% of the turbine output power. The most effective configurations placed microjets between the blade midspan to three-quarters span. Load reduction was achieved for both active and passive modes of air supply to the microjet system.
机译:这项研究调查了用于降低NREL-5 MW风力发电机负荷的微型喷气机的性能,并确定了最佳系统参数。微型喷气机可垂直于叶片表面吹气,并且可以迅速增加或减少叶片部分的升力,从而使风力涡轮机能够响应局部的短期风况变化。随着风力涡轮机转子变得越来越大,作用在单个叶片或叶片部分上的控制方法越来越需要减少临界疲劳和极端负荷。但是,微型喷气机需要动力才能运行,因此,至关重要的是,降低疲劳度应证明向系统输入的任何能量都是合理的。为了检查一系列潜在的微喷系统配置的降低疲劳的潜力,使用了叶片元件动量(BEM)代码和流动能量求解器来估算能量输入和主要疲劳度量的变化。进行了参数分析,以确定在一定的空气质量流量范围内,微型喷嘴的最佳翼展方向位置和长度。同时考虑了主动和被动供气方法。应用于NREL 5-MW转子的被动式微喷系统使最大襟翼根部弯矩(FRBM)降低了3.7%。使用5 kPa的鼓风机时,峰值弯曲力矩的减小增加到6.0%,这大约消耗了涡轮机输出功率的0.1%。最有效的配置是在叶片中跨到四分之三的跨度之间放置微型喷嘴。通过向微型喷射系统供气的主动和被动模式都实现了负载减少。

著录项

  • 来源
    《Journal of Energy Resources Technology》 |2019年第5期|051213.1-051213.8|共8页
  • 作者单位

    Univ Calif Davis, Mech & Aerosp Engn, One Shields Ave, Davis, CA 95616 USA|Bay Area Rapid Transit, Oakland, CA 94612 USA;

    Univ Calif Davis, Mech & Aerosp Engn, One Shields Ave, Davis, CA 95616 USA|Rescale, San Francisco, CA 94105 USA;

    Univ Calif Davis, Mech & Aerosp Engn, One Shields Ave, Davis, CA 95616 USA|Sandia Natl Labs, Livermore, CA 94550 USA;

    Univ Calif Davis, Mech & Aerosp Engn, One Shields Ave, Davis, CA 95616 USA;

    Univ Calif Davis, Mech & Aerosp Engn, One Shields Ave, Davis, CA 95616 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-18 04:13:51

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