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两个离心压气机叶轮的设计与性能比较

Design and Performance Comparison of Centrifugal Compressor Impellers

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【作者】 杨策胡辽平买靖东老大中王航

【Author】 YANG Ce~1,HU Liao-ping~2,MAI Jing-dong~1,LAO Da-zhong~1,WANG Hang~2 (1.School of Mechanical and Vehicular Engineering, Beijing Institute of Technology, Beijing100081, China; 2.Hunan Jiangyan Mechanical Plant, Hengyang, Hunan421005, China)

【机构】 北京理工大学机械与车辆工程学院湖南江雁机械厂湖南江雁机械厂 北京 100081湖南衡阳 421005北京 100081衡阳 421005

【摘要】 采用离心压气机计算机辅助集成设计系统,设计了两个不同子午形面和叶片角的离心压气机叶轮.对这两个离心压气机叶轮内部流场进行了三维粘性计算,给出了计算结果.计算结果表明,在一定范围内,降低叶片轮缘-轮毂方向的负荷可以提高叶轮效率,后加载方式可以改善离心压气机叶轮性能.叶轮进口尺寸相同的情况下,子午形面和叶片角的变化对叶片负荷分布有较大影响.

【Abstract】 Two centrifugal compressor impellers with different meridional shape and blade angle were designed using computer-aided integrated design systems. The flow fields of the impellers were calculated by solving three-dimensional Navier-Stokes equations. Calculation results illustrate that decreasing the blade hub-to-shroud loading level can increase the impeller adiabatic efficiency, and that aft-loaded impeller can obtain higher impeller adiabatic efficiency. Changing meridional shape and blade angle can have large effects on the blade loading distribution.

【基金】 国家部委预研项目(02020102)
  • 【文献出处】 北京理工大学学报 ,Journal of Beijing Institute of Technology , 编辑部邮箱 ,2004年09期
  • 【分类号】TH452
  • 【被引频次】7
  • 【下载频次】444
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