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叶尖射流对风力机叶尖流场影响的数值研究
引用本文:高翔,胡骏,王志强.叶尖射流对风力机叶尖流场影响的数值研究[J].航空动力学报,2014,29(8):1863-1870.
作者姓名:高翔  胡骏  王志强
作者单位:南京航空航天大学 能源与动力学院 江苏省航空动力系统重点实验室, 南京 210016;先进航空发动机协同创新中心, 北京 100191;南京航空航天大学 能源与动力学院 江苏省航空动力系统重点实验室, 南京 210016;先进航空发动机协同创新中心, 北京 100191;南京航空航天大学 能源与动力学院 江苏省航空动力系统重点实验室, 南京 210016;先进航空发动机协同创新中心, 北京 100191
基金项目:中央高校基本科研业务费专项资金资助;江苏省普通高校研究生科研创新计划资助项目(CXZZ11_0224);国家重点基础研究发展计划(2007CB210301)
摘    要:为了设计出更加适合非并网系统的风力机,采用在叶尖加入射流的方法来改变叶尖流场分布.在风力机叶片顶端沿弦长布置3个喷口,采用CFD数值模拟方法,通过改变风力机转速获得原型和带喷口的风力机模型的气动特性以及流场分布.发现在转速低于1 200r/min时,带有安装在不同位置的喷口的风力机功率增长率几乎都为零,射流在这一转速范围内对风力机的气动性能几乎没有影响.而转速高于1 200r/min时,随着转速的增大,喷口位于叶尖中部的风力机的功率增长率快速地增大,射流影响了75%以上叶高的表面的压力分布,在大转速下吸力面低压区范围较大,其叶尖涡涡量低于其他方案中,并且在下游扩散得比其他方案快,改善了风力机下游流场,提高了风力机效率.喷口布置在叶尖前缘时其叶尖涡的局部涡量较原型叶片稍大,降低了风力机功率的输出.喷口布置在叶尖尾缘时基本和原型叶片相同.该结论为设计适用于非并网系统的定桨距变转速风力机提供了基础.

关 键 词:射流  功率增长率  风力机气动性能  风能利用系数  叶尖涡
收稿时间:2013/11/6 0:00:00

Numerical study on effects of blade tip air jet on the flow field of wind turbine blade tip
GAO Xiang,HU Jun and WANG Zhi-qiang.Numerical study on effects of blade tip air jet on the flow field of wind turbine blade tip[J].Journal of Aerospace Power,2014,29(8):1863-1870.
Authors:GAO Xiang  HU Jun and WANG Zhi-qiang
Institution:Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;Co-Innovation Center for Advanced Aero-Engine, Beijing 100191, China;Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;Co-Innovation Center for Advanced Aero-Engine, Beijing 100191, China;Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;Co-Innovation Center for Advanced Aero-Engine, Beijing 100191, China
Abstract:In order to design a more suitable wind turbine for the non-grid-connected wind power system, the method of arranging air jet on the blade tip was adopted to change the flow field of blade tip. Orifices were arranged on the top of the blade tip at three chordwise positions. Using the CFD numerical simulation method, the aerodynamic performances and flow field distribution of a wind turbine based model and models with orifices were obtained under different rotating speeds. When the rotating speed was below 1200r/min, all the power growth rates of wind turbine with orifices were almost zero, indicating air jet had no effect on the aerodynamic performance of wind turbines at this range of rotating speed. When rotating speed was higher than 1200r/min, with the increase of rotating speed, the power growth rates of the wind turbine with air jet at middle of the chord raised fast. The air jet affected the pressure distribution on the blade surface of 75% blade height, and the low pressure area on the suction side was larger at high rotating speed. The vorticity of blade tip vortex of the blade with air jet at middle position was lower than the other model. Meanwhile, the dissipation of the blade tip vortex was faster than that of the other model, improving the downstream flow field and the efficiency of the wind turbine. There was no obvious change when the orifice was set at the trailing edge. But for the model with orifice at leading edge, the output power declined, and the wrticity of blade tip vortex is slightly larger than the based model. This conclusion provides the foundation for designing wind turbine applicable for non-grid-connected wind power system.
Keywords:air jet  power growth rate  aerodynamic performance of wind turbine  power coefficient of wind  blade tip vortex
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