首页> 外文会议>ASME/JSME/KSME Joint Fluids Engineering Conference >ANALYSIS OF ANGULAR VELOCITIES, SURROUNDING AIR PRESSURE AND VELOCITIES OF VARIOUS DESIGNED MICRO VERTICAL AXIS SAVONIUS WIND TURBINES BY THE COMPUTATIONAL FLUID DYNAMICS (CFD) METHOD
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ANALYSIS OF ANGULAR VELOCITIES, SURROUNDING AIR PRESSURE AND VELOCITIES OF VARIOUS DESIGNED MICRO VERTICAL AXIS SAVONIUS WIND TURBINES BY THE COMPUTATIONAL FLUID DYNAMICS (CFD) METHOD

机译:用计算流体动力学(CFD)方法分析各种设计的微垂直轴萨文尼风轮的角速度,周围气压和速度

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The objective of this study is to analyze angular velocities, surrounding air pressure and velocities of various micro vertical axis Savonius wind turbine prototypes by the Computational Fluid Dynamics (CFD) method. The angular velocities of turbines are the basic parameters for determining the major parameters of the wind turbines, such as efficiency, torque, power and electricity etc. Eight models of the micro vertical axis Savonius wind turbine made of acrylic were designed by varying three parameters including the turbine distance between the pivot point and the tip, the distance between the apex curvature and the center plane curvature and the cross section types (circular, square, triangular and trapezoid). The eight models were divided into three groups including two models (B1, B2) with two different cross section types (triangle and rectangular) in the first group, three models (C1, C2, C3) with three different distances from the curvature tip to the centerline of 110, 85 and 40 millimeters in the second group and three models (D1, D2, D3) with different distances between the pivot point and the tip in the third group. Then, the angular velocities, the surrounding air pressure and velocities of the micro vertical axis Savonius wind turbine at the five wind speeds at 5.59, 7.67, 9.76, 10.45 and 11.84 m/s were measured and evaluated by the ANSYS program. The simulation by the CFD method of the angular velocities of the designed wind turbines was compared with the experimental results. Some discrepancies due to the absence of friction in the CFD results were observed. However, discrepancies between the simulation and the experimental results were decreased when the wind speed was increased due to the increase of torque and force in the experimental results which has overcome the turbine core friction. It has indicated that at the highest wind speed (11.84 m/s), the designed micro vertical axis Savonius circular cross section wind turbine with the curvature of the distance from the apex curvature to the center plane at 110 millimeters gave the highest turbine angular velocity of 441 rpm. At this highest turbine velocity by the CFD simulation, the high surrounding air pressure was not the smallest and the low turbine surrounding air pressure area was not the largest. This might be due to the effect of the suitable apex curvature distance to the center plane causing the efficient air flow to overcome the effect of the surrounding air pressure. The wind turbine of the second group gave the highest angular velocities followed by the first and the third group. These designed micro vertical axis Savonius wind turbines can be used as a preliminary model for the design and construction of the micro wind turbine to generate electricity at low wind speed region, such as Thailand.
机译:这项研究的目的是通过计算流体动力学(CFD)方法分析角速度,周围气压和各种微型垂直轴Savonius风力涡轮机原型的速度。涡轮的角速度是确定风力涡轮机主要参数的基本参数,例如效率,转矩,功率和电等。通过改变三个参数,设计了八种由丙烯酸制成的Savonius微型垂直轴风力涡轮机模型,其中包括涡轮机的枢轴点与尖端之间的距离,顶点曲率与中心平面曲率之间的距离以及横截面类型(圆形,正方形,三角形和梯形)。八个模型被分为三组,其中第一组中具有两个不同横截面类型(三角形和矩形)的两个模型(B1,B2),曲率尖端到曲柄尖端的三个不同距离的三个模型(C1,C2,C3)第二组的中心线为110、85和40毫米,第三组的三个模型(D1,D2,D3)的枢轴点和尖端之间的距离不同。然后,通过ANSYS程序测量并评估了五种风速下的微型垂直轴Savonius风力发电机的角速度,周围气压和速度,分别为5.59、7.67、9.76、10.45和11.84 m / s。通过CFD方法对设计的风机的角速度进行了仿真,并与实验结果进行了比较。观察到由于CFD结果中没有摩擦而导致的一些差异。然而,由于克服了涡轮机芯摩擦的实验结果中的扭矩和力的增加,当风速增加时,模拟与实验结果之间的差异减小了。它表明,在最高风速(11.84 m / s)时,设计的微型垂直轴Savonius圆形截面风力涡轮机的顶点曲率到中心平面的距离的曲率为110毫米,从而给出了最高的涡轮机角速度441 rpm。通过CFD仿真,在此最高涡轮速度下,高周围空气压力不是最小,而低涡轮周围空气压力区域不是最大。这可能是由于到中心平面的合适的顶点曲率距离的影响,导致有效的气流克服了周围气压的影响。第二组的风力涡轮机具有最高的角速度,其次是第一组和第三组。这些设计的微型垂直轴Savonius风力涡轮机可以用作微型风力涡轮机的设计和建造的初步模型,以在低风速地区(例如泰国)发电。

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