首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >CENTRIFUGAL PUMP PERFORMANCE ENHANCEMENT BY BLADE SHAPE MODIFICATION
【24h】

CENTRIFUGAL PUMP PERFORMANCE ENHANCEMENT BY BLADE SHAPE MODIFICATION

机译:通过修改叶片形状来提高离心泵性能

获取原文

摘要

The effect of impeller blades shape modification on the centrifugal pump performance has been investigated numerically. Impeller blades' shape have been modified by new technique called "bladelet". This technique has been called the "bladelet" after the name of the aeroplane winglet because of the great similarity between them in shape and function. The shapes of the blade trailing edge greatly affect the performance of the turbomachines. So, the purpose of the blade tilting (bladelet) is to decrease the recirculating flow at the pump trailing edge due to the high pressure difference and enhance the hydraulic performance of the centrifugal pump. The bladelet technique has two main geometrical parameters: radial position R_(BL) and bladelet inclination angle θ_(BL). 3-D validated numerical simulation model has been carried out using commercial software, ANSYS® CFX, to study the effect of the bladelet technique and its different parameters on the pump performance at different flow rates. In this study nine cases with different bladelet parameters have been numerically simulated in order to check its effect on the centrifugal pump performance. These nine cases have been chosen by considering the geometrical constrain of the bladelet parameters. The results of these nine cases have been compared with the basic impeller (the same impeller but without bladelet) at the same operating condition in order to discuss the effect of the bladelet parameters variation on the centrifugal pump performance. It was found that the use of the bladelet technique decrease the pressure difference between the pressure and the suction side at the blade trailing edge. This decrease in pressure difference at the blade trailing edge decreases the flow recirculation at the impeller outlet from pressure side to suction side. Also, bladelet technique improves the hydraulic efficiency at the part-load operating zone. In addition, the bladelet has a regression effect on the pump head for some cases with high inclination angle and low radial position. However, the bladelet technique increases the impeller blades' overlap.
机译:数值研究了叶轮叶片形状改变对离心泵性能的影响。叶轮叶片的形状已通过称为“叶片”的新技术进行了修改。由于这种技术在飞机小翼的名称和功能上非常相似,因此被称为“小翼”。叶片后缘的形状极大地影响了涡轮机的性能。因此,叶片倾斜(叶片)的目的是减少由于高压差而在泵后缘处的再循环流量,并增强离心泵的液压性能。叶片技术具有两个主要的几何参数:径向位置R_(BL)和叶片倾斜角θ_(BL)。已使用商业软件ANSYS®CFX建立了经过3-D验证的数值模拟模型,以研究叶片叶片技术及其不同参数对不同流速下泵性能的影响。在这项研究中,已经对9种不同叶片参数的情况进行了数值模拟,以检查其对离心泵性能的影响。通过考虑小叶片参数的几何约束来选择这九种情况。为了讨论叶片参数变化对离心泵性能的影响,将这九种情况的结果与在相同工况下的基本叶轮(相同的叶轮但没有叶片的叶轮)进行了比较。已经发现,使用叶片技术减小了叶片后缘处的压力与吸力侧之间的压力差。叶片后缘处压力差的减小减小了叶轮出口处从压力侧到吸力侧的气流再循环。同样,叶片技术提高了部分负荷操作区的液压效率。另外,在某些倾斜角大而径向位置低的情况下,小叶片对泵头具有消退作用。然而,小叶片技术增加了叶轮叶片的重叠。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号