航空学报 > 2000, Vol. 21 Issue (4): 289-293

向心透平叶片角动量分布的优化

郭新生1, 谢立军2, 徐丽萍1   

  1. 1. 西安交通大学能源与动力工程学院,陕西西安710049;2. 海军航空技术学院,山东青岛266041
  • 收稿日期:1998-03-27 修回日期:1999-06-10 出版日期:2000-08-25 发布日期:2000-08-25

OPTIMIZATION OF ANGULAR MOMENTUM DISTRIBUTION FOR RADIAL INWARD FLOW TURBINES

GUO Xinsheng1, XIE Lijun2, XU Liping1   

  1. 1. College of Energy & Power Engineering, Xi′an Jiaotong University, Xi′an 710049, China;2. Navy Aviation Technique Academy, Qingdao 266041, China
  • Received:1998-03-27 Revised:1999-06-10 Online:2000-08-25 Published:2000-08-25

摘要:

以n条子午流线,给出满足约束条件的各自角动量分布的若干不同组合构成初始复合形,做复合形每一顶点处该向心透平叶轮S2 流面与跨叶片面势流场分析,并以二元紊流边界层动量厚度计算经三元修正,分析叶轮效率,最终使复合形法成功应用于向心透平叶片角动量分布的优化。该方法也适用于离心叶轮中叶片加载量的优化。

关键词: 径向透平, 角动量, 分布, 优化

Abstract:

A complex method is used in optimization of angular momentum distribution for radial inward flow turbines. Firstly, select a number of points {X j}={(λ 1 λ 2 … λ n) T j} which satisfy all restriction conditions and are taken as the apexes of an initial complex. Then, at every kind of angular momentum distribution ( λ 1 λ 2 … λ n) T j do computation of the main flow field for the S 2 flow surface and for the S 1 flow surface of the turbine impeller, do computation of momentum thickness of the blade’s two dimensional turbulent boundary layer, and do correction of the three dimensional effect on the thickness. By that, estimate the impeller efficiency η . Finally, it can make object function f (X)=1-η have a minimum value. This method can also suit centrifugal impellers. In this paper, an application example is given for a radial inward flow turbine. This optimization of angular momentum distribution can make the turbine have isentropic efficiency 86% and have better off design characteristics.

Key words: radial turbines, angular momentum, distributions, optimization

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