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CFD STUDY OF PROSPECTIVE 1ST STAGE CENTRIFUGAL IMPELLER DESIGN

机译:勘探第一阶段离心叶轮设计的CFD研究

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CFD analysis of two first - stage centrifugal impellers is undertaken with the main goal to obtain additional evaluation data regarding flow characteristics of the old first stage impeller design and in the proposed new cantilever impeller design. The new design is developed to reduce the 1st stage impeller cavitation erosion damage of a multistage centrifugal feed pump. This stage of work comprises computational tests of both impeller models under the same mode of operation, 3000 RPM and volumetric flow rate 0.0503 m{sup}3/s. Both impellers are planning to be tested experimentally. The inlet geometry for CFD tests is taken from the test facility draft. The outlet is made like a circular vaneless diffuser. In the old design, a hub developed upstream presents the through shaft. Computational results are compared with the head/efficiency data delivered by plane cascade theory. Computational data shows an advantage of the new design by head and efficiency although the efficiency level is underestimated. Computational data shows lower pressure zones in the proposed design are localized at the impeller inlet periphery, in the old design lower pressure zones spreads along the blade inlet height. Further computational test will be made for the whole geometry including the stage stator part and experimental validation of the proposed design will follow.
机译:两种第一阶段离心叶轮的CFD分析具有主要目标,以获得关于旧第一阶段叶轮设计的流动特性以及提出的新悬臂叶轮设计的额外评估数据。开发了新的设计,以减少多级离心饲料泵的第一级叶轮空化损坏。该工作阶段包括在相同操作模式下的叶轮模型的计算测试,3000rpm和体积流量0.0503 m {sup} 3 / s。两种叶轮都计划通过实验测试。 CFD测试的入口几何形状从测试设施草案中取出。出口是像圆形差别扩散器一样制成的。在旧设计中,一个枢纽开发的上游礼物轴。将计算结果与平面级联理论提供的头/效率数据进行比较。计算数据显示通过头部和效率的新设计的优点,尽管效率水平低估了。计算数据显示所提出的设计中的较低压力区在叶轮入口周边定位,在旧设计下压力区沿刀片入口高度铺展。进一步的计算测试将用于整个几何形状,包括级定子部件和所提出的设计的实验验证将遵循。

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