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首页> 外文期刊>Journal of turbomachinery >One-Dimensional and Three- Dimensional Design Strategies for Pressure Slope Optimization of High-Flow Transonic Centrifugal Compressor Impellers
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One-Dimensional and Three- Dimensional Design Strategies for Pressure Slope Optimization of High-Flow Transonic Centrifugal Compressor Impellers

机译:高流量跨音速离心压缩机叶轮压力斜率优化的一维和三维设计策略

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摘要

This paper deals with the numerical and theoretical investigations of the effect of geometrical dimensions and one-dimensional (1D)-design parameters on the impeller pressure slope of a transonic centrifugal compressor stage for industrial process application. A database being generated during the multi-objective and multipoint design process of a high flow coefficient impeller, comprising 545 computational fluid dynamics (CFD) designs is investigated in off-design and design conditions by means of Reynolds-averaged Navier-Stokes (RANS) simulation of an impeller with vaneless diffuser. For high flow coefficients of 0.16 phi(des) 0.18, the CFD-setup has been validated against measurement data regarding stage and impeller performance taken from MAN test rig experimental data for a centrifugal compressor stage of similar flow coefficient. This paper aims at answering the question how classical design parameter, such as the impeller blade angle distribution, impeller suction diameter, and camber line length affect the local and total relative diffusion and pressure slope toward impeller stall operation. A second-order analysis of the CFD database is performed by cross-correlating the CFD data with results from impeller two-zone 1D modeling and a rapid loading calculation process by Stanitz and Prian. The statistical covariance of first-order 1D-analysis parameters such as the mixing loss of the impeller secondary flow, the slip factor, impeller flow incidence is analyzed, thereby showing strong correlation with the design and off-design point efficiency and pressure slope. Finally, guide lines are derived in order to achieve either optimized design point efficiency or maximum negative pressure slope characteristics toward impeller stall operation.
机译:本文研究了几何尺寸和一维(1D)设计参数对跨音速离心压缩机级工业工艺应用的叶轮压力斜率的影响的数值和理论研究。在非设计和设计条件下,通过雷诺平均Navier-Stokes(RANS)研究了高流量系数叶轮的多目标和多点设计过程中生成的数据库,其中包括545个计算流体动力学(CFD)设计。无叶片扩压器叶轮的仿真对于0.16 hi(des)<0.18的高流量系数,CFD设置已针对从流量测试相似的离心式压缩机级的MAN试验台实验数据中获得的有关级和叶轮性能的测量数据进行了验证。本文旨在回答经典设计参数(例如叶轮叶片角度分布,叶轮吸入直径和外倾线长度)如何影响叶轮失速运行的局部和总体相对扩散以及压力斜率的问题。通过将CFD数据与叶轮两区域一维建模以及Stanitz和Prian的快速载荷计算过程的结果相互关联,对CFD数据库进行二阶分析。一阶一维分析参数的统计协方差,例如叶轮二次流的混合损失,滑移系数,叶轮流入射,得到了分析,从而显示出与设计点和设计外点效率和压力斜率的强相关性。最后,导出指导线以实现优化的设计点效率或叶轮失速运行的最大负压斜率特性。

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  • 来源
    《Journal of turbomachinery》 |2019年第5期|051002.1-051002.11|共11页
  • 作者

    Hildebrandt A.; Ceyrowsky T.;

  • 作者单位

    MAN Energy Solut SE, Steinbrinkstr 1, D-46145 Oberhausen, Germany;

    MAN Energy Solut SE, Steinbrinkstr 1, D-46145 Oberhausen, Germany;

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  • 正文语种 eng
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