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离心压气机管式扩压器设计与计算分析
引用本文:王博,严明.离心压气机管式扩压器设计与计算分析[J].航空动力学报,2012,27(6):1303-1311.
作者姓名:王博  严明
作者单位:北京航空航天大学 能源与动力学院 航空发动机气动热力国家级重点试验室,北京 100191
摘    要:采用程序化建模方法,对离心压气机管式扩压器的三维几何造型进行参数化设计,并采用定常数值模拟的方法分析管式扩压器内流场特性,攻角特性,对影响管式扩压器性能的几何参数进行分析与优化,同时对照某原型叶片式扩压器,分析传统圆形进口管式扩压器的性能优劣,提出类椭圆进口管式扩压器的概念,并揭示其能够有效提高离心压气机性能的机理. 

关 键 词:离心压气机    扩压器    管式扩压器    前掠    数值模拟
收稿时间:7/8/2011 12:00:00 AM

Design and numerical simulation of pipe diffuser in centrifugal compressor
WANG BO and YAN Ming.Design and numerical simulation of pipe diffuser in centrifugal compressor[J].Journal of Aerospace Power,2012,27(6):1303-1311.
Authors:WANG BO and YAN Ming
Institution:National Key Laboratory of Science and Technology on Aero-Engines Aero-thermodynamics, School of Jet Propulsion,Beijing University of Aeronautics and Astronautics, Beijing 100191,China
Abstract:Parameterized design for three-dimensional geometry of the pipe diffuser was preformed based on programmed model-construct method.The flow field and attack angle characteristics were investigated using time-averaged numerical method,and design parameters of the pipe diffuser were analyzed and optimized subsequently.Compared with the prototype vane diffuser,the performance of a pipe diffuser with traditional circle inlet was evaluated.Further study initiated a pipe diffuser with ellipse-like inlet which would expand the working range of centrifugal compressor,and suggested the mechanism of the improvement.
Keywords:centrifugal compressor  diffuser  pipe diffuser  forward-swept  numerical simulation
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