叶片尾部形状对双向贯流式水轮机性能的影响

    Effect of blade tail's shape on hydraulic performance of bidirectional bulb turbine

    • 摘要: 为了研究双向贯流式水轮机反向工况效率低下的问题,该文以某带有后置导叶的双向贯流式机组为对象,针对不同形状和不同厚度的叶片尾部,分析了反向工况下叶片尾部对机组性能的影响。采用UG建模软件对机组进行几何建模,基于CFX软件,采用SST k-ω湍流模型对不同形状和厚度的叶片尾部的转轮进行了数值模拟。结果表明:反向工况下采用圆形尾部的叶片其机组效率为59.55%,高于矩形尾部的58.4%和弧形尾部的58.01%,说明反向工况下矩形尾部和弧形尾部的冲击损失较大。增加叶片尾部厚度对机组反向工况的效率提高较为明显,其效率最高能抬高到79%,但叶片尾部厚度增加到一定程度后效率不再增加,叶片尾部厚度的增加使得反向工况下叶片尾部最低压力值降低了1.2×106 Pa,对其反向工况下的空化性能有较大影响,且增加了正向工况运行是出现卡门涡的概率。研究成果为双向贯流式水轮机反向工况下叶片尾部形状的优化设计提供了经验参考。

       

      Abstract: Abstract: Tidal power is pollution-free renewable energy and an effective way to reduce coal consumption and guarantee normal social electricity consumption in China. Bidirectional bulb turbine is widely used in tidal power station. Scholars at home and abroad have carried out extensive researches in bidirectional tubular turbine in terms of internal blade clearance flow, the occurrence and location of cavitation and blade airfoil optimization .Scholars in China firstly put forward improving the operating efficiency of the bidirectional tubular turbine under the reverse working condition by means of setting rear guide vanes. In order to solve the low efficiency problem under the reverse condition in bidirectional bulb turbine, how blade tail affected the units' hydraulic performance under reverse working condition by studying bade tails of different shapes and different thickness on the basis of a bidirectional bulb turbine unit with rear vanes was analyzed. The profile of computational domain was built with modeling software UG and the grid division was done with software ICEM, also the grid independence verification for runner parts was conducted. Based on the CFX software, the SST turbulence model was adopted to conduct numerical simulation on runners with blade tails of different shapes and thickness. Results showed, under reverse conditions, the efficiency of the units with circular blade tail was 59.55%, which was higher than 58.4% and 58.01% of units with rectangular and arched tailing edge respectively, indicating that the impact loss of runner with rectangular tail and curved tail was bigger. Moreover, increasing the thickness of the blade tail could improve the efficiency of the turbine relatively obvious under the reverse condition, and the efficiency could reach at 79%, but the method no longer worked when the blade tail thickness increased to a certain degree. The increase of the tail thickness changed pressure distribution on the blade suction surface, and the minimum pressure value reduced by 1 200 000 Pa under reverse condition on the blade tail, which greatly affected the cavitation performance under the reverse condition. Increasing the thickness of blade tail caused squeezing action to the passage channel, which increased the positive condition efficiency but the effect was not obvious. However, the increase of blade's tail thickness decreased the frequency of the Karman vortex at the tail outlet under positive conditions, as the frequency of the unit components was usually low frequency, the probability of the occurrence of Karman vortices on positive condition was increased. The results showed that compared with rectangular blade tail and arched blade tail, the unit with circular blade tail performed the best under reversal conditions. We can conclude that in order to improve the units efficiency under the reverse condition, thickness of blade tail can be appropriately increased. But that could been donein the premise of ensuring Karman vortices resonance wouldn't occur with other components of the unit under positive conditions. The research results provided references for optimization design of blade tail shape under the reverse condition in bidirectional turbine.

       

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