共查询到19条相似文献,搜索用时 225 毫秒
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《工程热物理学报》2015,(11)
本文采用笛卡尔动网格方法数值模拟研究了叶顶端板对H型垂直轴风力机非定常气动特性与三维黏性绕流场的影响。选用SST湍流模型,假设全流场为湍流流动。叶尖速比为1.86~2.57,以实验模型为研究对象,对未加装叶顶端板的H型风力机进行了三维数值模拟研究。在实验模型的基础上给每个叶片的顶部分别加装了端板,采用同样的数值模拟方法,选择低、中、高三个叶尖速比研究了带有叶顶端板的H型风力机的三维非定常气动特性。利用不带端板和带有端板的风力机模型计算得到的功率系数与实验数据进行了比较,讨论了单个叶片和风轮载荷沿周向的变化,分析了一个旋转周期叶顶附近相对速度的变化规律,揭示了加装端板后风力机气动载荷提高的原因。 相似文献
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一种改进的诱导因子计算方法 总被引:1,自引:0,他引:1
本文利用开发的程序,对BEM计算模型中诱导因子的计算方法进行研究.比较分析了已有几种计算方法的优劣,在此基础上提出一种改进的计算方法,并以美国可再生能源实验室(NREL)直径为10 m水平轴风力机叶片气动试验数据为依据,验证了本文算法的准确性和优越性. 相似文献
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通过风洞试验对某高速动车组整车、受电弓及转向架远场气动噪声特性进行分析。试验结果表明,高速动车组远场气动噪声是一宽频噪声,总声能随速度的6.6次方增加;由受电弓引起的远场气动噪声主要集中在中高频,噪声峰值频率随速度变化线性增加;由转向架引起的远场气动噪声主要集中在中低频,噪声峰值频率与速度无关。在此基础上,通过大涡模拟和声扰动方程获得该高速动车组近场噪声。高速动车组远场噪声测点仿真结果与试验结果的最大差值2.2 dB(A),最大相对误差2.5%,表明仿真模型的准确性。仿真结果表明,车头近场噪声以车头鼻尖为界,底部气动噪声能量大于上部流线型气动噪声能量,其中转向架舱位置噪声能量最大,因此进行车内外降噪方案设计时,应重点关注车头转向架舱位置。 相似文献
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随着风力机大型化发展,叶片尾缘襟翼控制技术,作为叶片流场主动控制的一种有效手段,能够有效、快速、灵活地降低叶片载荷,提高风力机,特别是大型风力机的可靠性、经济性,该技术受到国内外的广泛关注。为深入了解叶片襟翼实际作用效果及降载机制,在大量数值仿真计算工作基础上,需进一步开展带有襟翼控制的模型风力机风洞实验工作。本文在相似准则基础上,引入叶片展向环量、Polar线相似条件,对NREL 5 MW风力机叶片按1:105进行缩比设计,采用伺服电机驱动襟翼的结构方案对叶片参数进行修正,并根据BEM理论优化带有襟翼叶片的气动性能,最终确定带有襟翼控制的风力机叶片设计方案。最后利用气弹耦合仿真计算平台对带有襟翼控制的模型风力机进行性能计算,确定理想实验工况点及对应的降载效果。本文所开展的工作不仅能够为叶片缩比设计提供新思路,更有意义的是为襟翼控制系统在叶片中的实现提供有效借鉴。 相似文献
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波浪与风载的共同作用下,海上风电机组平台存在多自由度运动,同时伴随着海上复杂的风况,其气动特性变化较为复杂。以NREL5MW风电机组为研究对象,在风剪切来流下,依据波浪和风载的作用规律,研究平台纵摇和纵荡运动对机组气动特性和绕流场细节的影响。结果表明:平台运动会造成风电机组气动性能的周期性波动,而风剪切作用使得风电机组平均发电量降低并加剧功率和推力的波动。风剪切会增大纵摇运动过程中展向截面的法向载荷幅值且波动加剧,但会降低与功率输出有关的切向受力;风剪切作用推迟了纵荡运动过程中展向截面法向和切向载荷峰值出现时刻,加剧载荷的波动。外叶展截面的法向和切向力系数曲线出现平台,加剧了叶片疲劳载荷,减小了功率输出。 相似文献
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In-plane vibrations of wind turbine blades are of concern in modern multi-megawatt wind turbines. Today?s turbines with capacities of up to 7.5 MW have very large, flexible blades. As blades have grown longer the increasing flexibility has led to vibration problems. Vibration of blades can reduce the power produced by the turbine and decrease the fatigue life of the turbine. In this paper a new active control strategy is designed and implemented to control the in-plane vibration of large wind turbine blades which in general is not aerodynamically damped. A cable connected active tuned mass damper (CCATMD) system is proposed for the mitigation of in-plane blade vibration. An Euler–Lagrangian wind turbine model based on energy formulation has been developed for this purpose which considers the structural dynamics of the system and the interaction between in-plane and out-of-plane vibrations and also the interaction between the blades and the tower including the CCATMDs. The CCATMDs are located inside the blades and are controlled by an LQR controller. The turbine is subject to turbulent aerodynamic loading simulated using a modification to the classic Blade Element Momentum (BEM) theory with turbulence generated from rotationally sampled spectra. The turbine is also subject to gravity loading. The effect of centrifugal stiffening of the rotating blades has also been considered. Results show that the use of the proposed new active control scheme significantly reduces the in-plane vibration of large, flexible wind turbine blades. 相似文献
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Field and laboratory experiments were performed to unravel the structure of the power output fluctuations of horizontal-axis wind turbines based on incoming flow turbulence. The study considers the power data of three wind turbines of rotor sizes 0.12, 3.2, and 96 m, with rated power spanning six decades from the order of 100 to 106 W. The 0.12 m wind turbine was tested in a wind tunnel while the 3.2 and 96 m wind turbines were operated in open fields under approximately neutrally stratified thermal conditions. Incoming flow turbulence was characterised by hotwire and sonic anemometers for the wind tunnel and field set-ups. While previous works have observed a filtering behaviour in wind turbine power output, this exact behaviour has not, to date, been properly characterised. Based on the spectral structure of the incoming flow turbulence at hub height, and the mechanical and structural properties of the turbines, a physical basis for the behaviour of temporal power fluctuations and their spectral structure is found with potential applications in turbine control and numerical simulations. Consistent results are observed across the geometrical scales of the wind turbines investigated, suggesting no Reynolds number dependence in the tested range. 相似文献