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双级离心压气机回流器流动特点分析
引用本文:高星,刘宝杰.双级离心压气机回流器流动特点分析[J].航空动力学报,2009,24(2):432-438.
作者姓名:高星  刘宝杰
作者单位:北京航空航天大学能源与动力工程学院航空发动机气动热力重点实验室,北京,100191
摘    要:设计了高负荷的双级离心压气机回流器,采用数值模拟的方法,分析了回流器内部主要流动结构,及其流动机理.基于对流动机理的认识,进一步对比分析了进口流场,叶片数,负荷分布形式对回流器流动结构和性能的影响.结果表明,改善进口流场、增加叶片数能够抑制回流器内部的二次流,增加回流器出口流场均匀性;负荷分布形式对回流器流动结构和性能影响较大,前加载的负荷分布形式能够得到更好的性能.

关 键 词:双级离心压气机  回流器  二次流  负荷分布
收稿时间:1/8/2008 12:00:00 AM
修稿时间:2008/6/20 0:00:00

Analysis of the flow in return vanes of a two-stage centrifugal compressor
GAO Xing and LIU Bao-jie.Analysis of the flow in return vanes of a two-stage centrifugal compressor[J].Journal of Aerospace Power,2009,24(2):432-438.
Authors:GAO Xing and LIU Bao-jie
Institution:National Key Laboratory on Aero-Engines;School of Jet Propulsion;Beijing University of Aeronautics and Astronautics;Beijing 100191;China
Abstract:To examine the influences of some typical design parameters(the inlet flow condition,blade number,and vane loading distribution) on the performances of the return vanes in a two-stage centrifugal compressor,a series of return vanes were designed and analyzed numerically by 3-D viscous code.It was found that the secondary flows in the return vane were usually very strong;however,improving the inlet flow uniformity,increasing the blade number and optimizing the vane loading distribution could weaken the secon...
Keywords:two-stage centrifugal compressor  return vane  secondary flow  loading distribution  
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