可变风速下保证最大升力和低噪声运行的风力机廓线建模

V. Radulescu
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引用次数: 0

摘要

本文提出了一种基于最大升力概念的风力机廓形建模新方法,该方法可以在不同风速值下产生。该剖面是根据近十年来出现的新概念设计和实现的,以最大升力运行风力涡轮机。其目的是在运行期间提供低噪音,因为对风力涡轮机(风电场)中长期运行的负面影响是影响鸟类飞行,陆生动物生活,特别是人类社区的噪音。各种源在风廓线上产生独立的声发射,如湍流流动、尾缘湍流边界层区域的相互作用、流动分离、尾缘区域内形成的涡的边界层分离等。还考虑了视风对廓线入射变化的影响。为了保持相对于风速的最佳迎角,固定的叶片倾角必须增加其速度以与风成正比。因此,为了最大限度地提高气动性能,当风强度增加时,转子必须旋转得更快。声信号的测量需要电子设备,这些设备对从电压或电流的压力变化的转换中获得的电信号进行操作。紊流引起的噪声主要是由尖锐的前缘产生的,不能消除。文中给出了一些与现场实测相关联的数值结果。
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Modeling the Wind Turbine Profiles Assuring the Maximum Lift Force With Low-Noise Operation for Variable Wind Velocities
The paper presents a new solution for the wind turbine profile shape modeling based on the concept of the maximum lift force, capable to be produced at different values of the wind velocities. The profile is designed and realized in accordance with the new concept emerged in the last decade, on the operation of the wind turbines with maximum lifting force. The purpose is to provide a low-noise during operation because a negative effect on the medium and long-term operation of the wind turbines (wind farms) is the noise that affects the flight of birds, terrestrial animal life, and especially human communities. Various sources generate independent acoustic emissions on wind profiles, such as the turbulent flow, the interaction of the turbulent boundary layer area of the trailing edge, the flow separation, and the boundary layer separation of vortices formed in the zone of the trailing edge. There is also considered the influence of the apparent wind on the incidence variation of the profile. In order to maintain an optimum angle of attack relative to the wind velocity, a fixed blade inclination must increase its speed to be proportional to the wind. Thus, to maximize the aerodynamic performance, the rotor must spin faster when the wind intensity increases. Measurement of the acoustic signal requires electronic devices that operate on electric signals obtained from the conversion of the pressure variations in voltage or variations in electrical current. The noise caused by the turbulent flow is generated primarily by the sharply pointed leading edge and cannot be diminished. There are presented some numerical results correlated with the measurements made in the field.
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