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向心透平叶片角动量分布的优化
引用本文:郭新生,谢立军,徐丽萍.向心透平叶片角动量分布的优化[J].航空学报,2000,21(4):289-293.
作者姓名:郭新生  谢立军  徐丽萍
作者单位:西安交通大学能源与动力工程学院!陕西西安710049(郭新生,徐丽萍),海军航空技术学院!山东青岛266041(谢立军)
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  
收稿时间:1998-03-27;
修稿时间:1998-03-27

OPTIMIZATION OF ANGULAR MOMENTUM DISTRIBUTION FOR RADIAL INWARD FLOW TURBINES
GUO Xin sheng ,XIE Li jun ,XU Li ping WTBZ.OPTIMIZATION OF ANGULAR MOMENTUM DISTRIBUTION FOR RADIAL INWARD FLOW TURBINES[J].Acta Aeronautica et Astronautica Sinica,2000,21(4):289-293.
Authors:GUO Xin sheng  XIE Li jun  XU Li ping [WTBZ]
Institution:GUO Xin sheng 1,XIE Li jun 2,XU Li ping 1 [WT6BZ]
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.
Keywords:radial turbines  angular momentum  distributions  optimization
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