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轴流式压气机近失速状态端壁流动时频分析
引用本文:张朴,李应红,尉询楷,吴云,张百灵.轴流式压气机近失速状态端壁流动时频分析[J].航空动力学报,2005,20(2):278-281.
作者姓名:张朴  李应红  尉询楷  吴云  张百灵
作者单位:空军工程大学工程学院,推进系统实验室,陕西,西安,710038
摘    要:为准确辨识某型单轴涡喷发动机压气机近失速点的流动特征,对其端壁静压信号进行了时频分析。时频分析结果表明,近失速点的工况下,与其它各级相比,压气机第一级静子机匣壁面流动变化最为显著;随着发动机工作点沿共同工作线趋近喘振边界,压气机第一级静子机匣壁面静压信号中以550Hz为中心的宽带信号开始出现并逐步增强。所发现的压气机端壁流态特征可用于发动机节流过程中工作点接近失速边界的程度的判定,具有一定的工程应用价值。

关 键 词:航空、航天推进系统  端壁流动  时频分析  压气机  发动机  喘振  失速  流动分离
文章编号:1000-8055(2005)02-0278-04
收稿时间:2004/5/24 0:00:00
修稿时间:2004年5月24日

Time-Frequency Analysis of the Axial Flow Compressor Endwall Flow at Near Stall Conditions
ZHANG Pu,LI Ying-hong,WEI Xun-kai,WU Yun and ZHANG Bai-ling.Time-Frequency Analysis of the Axial Flow Compressor Endwall Flow at Near Stall Conditions[J].Journal of Aerospace Power,2005,20(2):278-281.
Authors:ZHANG Pu  LI Ying-hong  WEI Xun-kai  WU Yun and ZHANG Bai-ling
Abstract:To identify the flow pattern of a single-spool turbojet axial flow compressor at near stall conditions,the compressor end wall static pressure signals were analyzed using time-frequency analysis technology.The results show that at near stall conditions,the endwall flow of the first compressor stator varies dramatically compared to other stators.As the operating point runs close to the surge line along the operating line,a broad band signal centered on 550 Hz occurs and gradually builds up.The observed end wall flow patterns can be used to assess the stall margins during engine throttling,and thus,it has certain value in engineering application.
Keywords:aerospace propulsion system  endwall flow  time-frequency analysis  compressor  engine  surge  stall  flow separation  
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