北京航空航天大学学报 ›› 2016, Vol. 42 ›› Issue (5): 953-960.doi: 10.13700/j.bh.1001-5965.2015.0328

• 论文 • 上一篇    下一篇

多级导流诱导轮与叶轮一体型线优化

李嘉1, 李华聪1, 王淑红2, 徐轩2   

  1. 1. 西北工业大学 动力与能源学院, 西安 710072;
    2. 中航工业西安航空动力控制科技有限公司, 西安 710077
  • 收稿日期:2015-05-21 出版日期:2016-05-20 发布日期:2016-02-18
  • 通讯作者: 李华聪,Tel.:029-88495791 E-mail:lihuacong@nwu.edu.cn E-mail:lihuacong@nwu.edu.cn
  • 作者简介:李嘉 男,博士研究生。主要研究方向:航空发动机控制。Tel.:029-88495791 E-mail:lijia89626@163.com;李华聪 男,博士,教授,博士生导师。主要研究方向:航空发动机控制系统及燃油系统设计与仿真。Tel.:029-88495791 E-mail:lihuacong@nwu.edu.cn;王淑红 女,高级工程师。主要研究方向:航空发动机控制元件仿真应用。E-mail:jjyyvivi@126.com;徐轩 男,高级工程师。主要研究方向:航空发动机控制元件仿真应用。E-mail:270571738@qq.com

Profile optimization of multi-diversion combination inducer and impeller

LI Jia1, LI Huacong1, WANG Shuhong2, XU Xuan2   

  1. 1. School of Power and Energy, Northwestern Polytechnical University, Xi'an 71007;
    2. China AVIC Xi'an Aero-engine Controls Technology Co, Ltd., Xi'an 710077, China
  • Received:2015-05-21 Online:2016-05-20 Published:2016-02-18

摘要: 通过分析型线参数化系数与结构参数的相关性联系,实现基于型线的参数化改型,从而达到多级导流一体式诱导轮与叶轮性能优化的目的。采用最小二乘法实现叶轮型线拟合,将拟合型线模型的计算流体力学(CFD)仿真结果与原模型的试验结果进行对比,结果表明:仿真结果与原模型试验结果扬程值和效率值误差均小于2%,使用的拟合方法能够实现型线优化。通过分析拟合型线参数化系数与叶轮进出口安装角等的相关性联系,对不同结构参数模型进行型线优化,并对其性能进行仿真对比。结果表明:3组型线模型的内流场整体上正常稳定,其叶轮的各个流道出口和蜗壳隔舌处存在一定范围的低压区,且由于隔舌处漩涡流动的影响使得扩散管出口存在一定区域的高速团。型线3为最优的型线模型,其扬程值与效率值均达到了优化目的,且在设计工况下,其性能提高最为明显。

关键词: 多级导流, 一体式诱导轮与叶轮, 型线优化, 计算流体力学(CFD), 数值模拟

Abstract: As the research objective is to optimize the performance of the combination multi-diversion inducer and impeller, this paper carries out the profile optimization study based on the correlation analysis of profile parameters with the structural parameters. Using the least square method, we obtained the fitting profile of the impeller, then compared the computational fluid dynamics (CFD) simulation results of the fitting model with the experimental results of the original model. The contrast shows that the error values of head and efficiency are less than 2%, and identifies the fitting method's accuracy. Finally, we compared the performances of the different fitting models through analyzing the correlation between fitting coefficient and impeller's inlet and outlet structural parameters. The results show that the internal flow fields of the three fitting models are stable. The impeller outlet and volute tongue have some low-pressure areas, and a certain high-speed group exists at the diffuse outlet because of the influence of vortex flow at the tongue. Ultimately, the head and efficiency of profile-3 are most optimized and obviously at the design point.

Key words: multi-diversion, combination inducer and impeller, profile optimization, computational fluid dynamics (CFD), numerical simulation

中图分类号: 


版权所有 © 《北京航空航天大学学报》编辑部
通讯地址:北京市海淀区学院路37号 北京航空航天大学学报编辑部 邮编:100191 E-mail:jbuaa@buaa.edu.cn
本系统由北京玛格泰克科技发展有限公司设计开发