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Optimization Design and Performance Analysis of a Pit Turbine with Ultralow Head

机译:超低水头井式水轮机的优化设计与性能分析

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摘要

A developed pit turbine with ultralow head was optimization designed under the design head of about 2 meters to achieve the goal of improving the turbine unit's efficiency. At the same time, the turbine's synthetic characteristic curve was drawn to predict the turbine's overall performance. Navier-Stokes equations and SIMPLEC algorithm were used for pit turbine's whole flow passage numerical simulation of the 3D, steady, incompressible, turbulent flow field. Through the CFD numerical simulation, the influence to ultralow head turbine's performance was analyzed by runner blade's different setting angles and guide vane's different axes. Considering the hydraulic performance of various methods, the best blade's setting angle and guide vane's axis were chosen. The results show that, the turbine unit has the best performance on efficiency, hydraulic loss, and so forth, with the blade's setting angle 23° and the angle 72° between the guide vane and the centerline of unit, meeting the power station's design requirements. The development pit turbine with ultralow head shows the highest efficiency of 87.6% under condition of design head of 2.1 meters and design discharge of 10 m~3/s. The energy performance of pit turbine with ultralow head was researched by the model test of GD-WS-35 turbine. The model turbine's characteristic curve was drawn. The model turbine's high efficiency area is wide and the efficiency changes mildly. The numerical simulation results are essentially consistent with the model test results, while the former one is slightly higher than the latter one. The error range is ±3%.
机译:在约2米的设计扬程下对开发的具有超低扬程的坑式涡轮机进行了优化设计,以达到提高涡轮机效率的目的。同时,绘制了涡轮机的综合特性曲线,以预测涡轮机的整体性能。将Navier-Stokes方程和SIMPLEC算法用于pit涡轮机对3D稳定,不可压缩,湍流场的整个流道数值模拟。通过CFD数值模拟,通过叶轮叶片的不同设定角和导叶的不同轴对超低水头水轮机性能的影响进行了分析。考虑到各种方法的液压性能,选择了最佳叶片的设定角和导向叶片的轴线。结果表明,该机组具有效率,水力损失等最佳性能,叶片的设定角为23°,导向叶片与机组中心线之间的夹角为72°,满足电站的设计要求。 。在设计水头为2.1米,设计排水量为10 m〜3 / s的条件下,超低水头的开发坑式涡轮机的最高效率为87.6%。通过GD-WS-35透平的模型试验研究了超低扬程的基坑透平的能量性能。绘制了模型涡轮机的特性曲线。模型涡轮机的高效率区域很广,效率变化适中。数值模拟结果与模​​型测试结果基本吻合,而前者略高于后者。误差范围为±3%。

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