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A Comparative study on the aeromechanic performances of upwind and downwind horizontal-axis wind turbines

机译:上,下风向水平轴风力发电机风机性能的比较研究

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Traditional horizontal-axis wind turbines are mainly designed as upwind configuration. In order to avoid blade strikes, the rotor blades have to be positioned far enough away from the turbine tower and have to be designed as inflexible as possible. In addition, a complicated yaw control system is required to keep the turbine rotor facing the incoming wind. Due to these drawbacks, the turbine in downwind configuration is proposed to overcome these disadvantages because, first of all, rotor blades can be designed more flexible since there is no danger of blade strikes, and secondly, yaw control system could be eliminated if nacelle is designed appropriately to follow the incoming wind direction passively. In the present study, a comparative experimental investigation was conducted to quantify the aeromechanic performance of a downwind turbine (DWT), in comparison to that of a traditional upwind turbine (UWT). The thrust coefficient of the DWT model was found to be increased slightly in the time-averaged quantity, but have a significant augment in the fluctuations. Due to the shadow effect, the power outputs of the DWT model was found to be decreased by 3.2% when they were operated in a same atmospheric boundary layer (ABL) wind. In addition, a high-resolution particle image velocimetry (PIV) system was employed to characterize the ensemble-averaged and phase-locked wake flow structures to quantify the turbulent flow characteristics in the turbine wakes. The velocity deficit in the lower half turbine wake for the UWT case was found to be greater than that of the DWT case at the location of X/D 1.0. The higher wind load fluctuations for the DWT system were found to be correlated well with the higher TKE distributions in the turbine wakes. The phase-locked PIV measurements illustrated that the wake regions can be divided into four zones, which are dominated by the vortices shedding from different turbine components. The detailed flow field measurements were correlated with the dynamic force and power measurement data to elucidate the underlying physics.
机译:传统的水平轴风力涡轮机主要设计为迎风配置。为了避免叶片撞击,转子叶片必须放置在距涡轮机塔足够远的位置,并且必须设计成尽可能不挠性。另外,需要复杂的偏航控制系统来使涡轮转子保持面对来风。由于这些缺点,提出了处于顺风构型的涡轮机以克服这些缺点,因为首先,由于没有叶片撞击的危险,转子叶片可以被设计为更加柔性,其次,如果机舱被安装,则可以消除偏航控制系统。进行适当设计以被动地遵循传入的风向。在本研究中,进行了对比实验研究,以量化与传统上风向涡轮(UWT)相比,下风向涡轮(DWT)的航空机械性能。发现DWT模型的推力系数在时间平均量上略有增加,但在波动方面有明显增加。由于阴影效应,当在相同的大气边界层(ABL)风中运行时,DWT模型的功率输出降低了3.2%。此外,采用高分辨率粒子图像测速(PIV)系统表征集合平均和锁相尾流结构,以量化涡轮尾流中的湍流特性。在X / D <1.0的位置,对于UWT情况,下半涡轮机尾流的速度损失大于DWT情况。发现DWT系统较高的风荷载波动与涡轮尾流中较高的TKE分布密切相关。锁相PIV测量结果表明,尾流区域可分为四个区域,这些区域主要由来自不同涡轮机部件的涡流散发。详细的流场测量与动态力和功率测量数据相关联,以阐明基本物理原理。

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