首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于多级环境下的双排对转压气机优化设计
引用本文:王雷,刘波,梁俊,王庆伟.基于多级环境下的双排对转压气机优化设计[J].航空动力学报,2010,25(6):1381-1388.
作者姓名:王雷  刘波  梁俊  王庆伟
作者单位:西北工业大学 动力与能源学院,西安 710072
基金项目:国家自然科学基金,863计划项目 
摘    要:以某双排对转压气机为研究对象,采用三维Navier-Stokes方程计算、叶片参数化造型、神经网络构建近似函数、遗传算法寻优相结合的优化方法,对转子2叶片进行级环境下的全三维叶型优化方案探索.优化目标是在控制流量和压比的情况下,最大化等熵效率.优化结果显示,设计点压气机效率提高1.5%左右.通过流场细微结构分析表明新叶型的气动布局得到合理改善,转子2中,尖部流场低速区域有所减少,分离现象有所减弱. 

关 键 词:对转    压气机    优化环境    流场分析
收稿时间:2009/5/27 0:00:00
修稿时间:2009/11/5 0:00:00

Optimization of dual stage counter-rotating compressor in multistage environment
WANG Lei,LIU Bo,LIANG Jun and WANG Qing-wei.Optimization of dual stage counter-rotating compressor in multistage environment[J].Journal of Aerospace Power,2010,25(6):1381-1388.
Authors:WANG Lei  LIU Bo  LIANG Jun and WANG Qing-wei
Institution:School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,China
Abstract:With the optimization platform of three-dimensional(3-D) design,the optimization design was carried out for rotor 2 of a two stage counter-rotating compressor in multistage environment based on the methods such as: three-dimensional Navier-Stokes(N-S) flow computation,blade section parameterization,artificial neural networks and genetic algorithm.The optimization objective is to maximize the isentropic efficiency while the mass flow and total pressure ratio are controlled.Numerical results show that efficiency is increased by 1.5% at design point after optimization of rotor 2.The gain in aerodynamic performance is largely attributable to the reduction of losses due to flow separation in suction side,as observed through flow field analysis. 
Keywords:counter-rotating  compressor  optimization environment  flow field analysis
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号