首页> 外文会议>2nd international conference on energy sustainability 2008 >DEVELOPMENT OF A WIND TUNNEL TEST APPARATUS FOR HORIZONTAL AXIS WIND TURBINE ROTOR TESTING
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DEVELOPMENT OF A WIND TUNNEL TEST APPARATUS FOR HORIZONTAL AXIS WIND TURBINE ROTOR TESTING

机译:水平轴风轮机转子风洞试验装置的研制

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摘要

The engineering of wind turbines is not fully mature. There are still phenomena, particularly dynamic stall that cannot be accurately modeled. Dynamic stall contributes to fatigue stress and premature failure in many turbine components. The three dimensionality of dynamic stall make these structures unique for wind turbines. Currently flow visualization of dynamic stall on a wind turbine rotor has not been achieved, but these visualizations can reveal a great deal about Ihe structures that contribute to dynamic stall.rnParticle Image Velocimetry (PIV) is a powerful experimental technique that can take non-intrusive How measurements of planar flow simultaneously. High-speed cameras enable time resolved PIV can reveal the transient development. This technique is suited to gain a better understanding of dynamic stall. A custom 3.27 m diameter wind turbine has been built to allow such measurements on the blade. The camera is mounted on the hub and will take measurements within the rotating domain. Mirrors are used so that laser illumination rotates with the blade. The wind turbine will operate in controlled conditions provided by a large wind tunnel. High-speed pressure data acquisition will be used in conjunction with PIV to get an understanding of the forces associated with the How structures.rnMany experiments will be made possible by this apparatus. First the flow structures responsible for the forces can be identified. Quantitative measurements of the flow field will identify therndevelopment of the stall vortex. The quantified flow structures can be used to verify and improve models. The spatial resolution of PIV can map the three dimensional structure in great detail. The experimental apparatus is independent of the blade geometry; as such multiple blades can be used to identify the effect of blade geometry. Finally flow control research in the field of aviation can be applied to control dynamic stall. These experiments will be subject of much of the future work at the University of Waterloo. Potentially this work will unlock the secrets of dynamic stall and improve the integrity of wind turbines.
机译:风力涡轮机的工程尚未完全成熟。仍然存在无法准确建模的现象,尤其是动态失速。动态失速会导致许多涡轮部件的疲劳应力和过早失效。动态失速的三维特性使这些结构对于风力涡轮机而言是独一无二的。当前,尚未实现风力涡轮机转子上动态失速的流动可视化,但是这些可视化可以揭示出大量有助于动态失速的结构。粒子图像测速技术(PIV)是一项功能强大的实验技术,可以采用非侵入式如何同时测量平面流。高速摄像机使时间分辨力PIV可以显示瞬态发展。此技术适合于更好地了解动态失速。定制的直径为3.27 m的风力涡轮机已经建成,可以在叶片上进行此类测量。摄像机安装在轮毂上,并将在旋转域内进行测量。使用反光镜,使激光照明随刀片旋转。风力涡轮机将在大型风洞提供的受控条件下运行。高速压力数据采集将与PIV结合使用,以了解与结构结构有关的力。这种设备将使许多实验成为可能。首先,可以确定负责这些力的流动结构。流场的定量测量将确定失速涡旋的发展。量化的流量结构可用于验证和改进模型。 PIV的空间分辨率可以非常详细地映射三维结构。实验装置与叶片的几何形状无关。因为可以使用多个叶片来识别叶片几何形状的影响。最终,可以将航空领域的流量控制研究应用于动态失速控制。这些实验将成为滑铁卢大学未来许多工作的主题。这项工作很有可能会揭开动态失速的秘密,并提高风力涡轮机的完整性。

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  • 会议地点 Jacksonville FL(US);Jacksonville FL(US)
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    Department of Mechanical and Mechatronics Engineering University of Waterloo Waterloo, Ontario, Canada N2L 3G1;

    Department of Mechanical and Mechatronics Engineering University of Waterloo Waterloo, Ontario, Canada N2L 3G1;

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