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EFFECTS OF IMPELLER SQUEALER TIP ON CENTRIFUGAL COMPRESSOR PERFORMANCE

机译:叶轮剥皮器技巧对离心压缩机性能的影响

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This paper summarizes the main results sorted out from a Design of Experiment (DoE) based on a validated Computational Fluid Dynamics (CFD). Several tip recessed geometries applied to an unshrouded impeller were considered in conjunction with two tip clearance levels. The computations show that recessed tip geometries have positive effects when considering high flow coefficient values while in part-load conditions the gain is reduced. Starting from the results obtained when studying tip cavities, a single rim tip squealer geometry was then analysed: the proposed geometry leads to performance improvements for all the tested conditions considered in this work.
机译:本文总结了基于经过验证的计算流体动力学(CFD)从实验设计(DoE)中挑选出的主要结果。结合两个尖端间隙水平,考虑了应用于无罩叶轮的几种尖端凹入几何形状。计算表明,当考虑高流量系数值时,凹入式尖端的几何形状具有积极作用,而在部分负载条件下,增益会降低。从研究吸头腔时获得的结果开始,然后分析了单个轮辋吸头器的几何形状:提出的几何形状导致本工作中考虑的所有测试条件下的性能提高。

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