首页 | 本学科首页   官方微博 | 高级检索  
     

概率密度函数分析监测发动机气动不稳定征兆
引用本文:张朴,李应红,吴云,刘建勋,张百灵. 概率密度函数分析监测发动机气动不稳定征兆[J]. 航空动力学报, 2005, 20(4): 567-571
作者姓名:张朴  李应红  吴云  刘建勋  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:对某型单轴涡喷发动机节流过程中的喘振故障进行了试验研究。在手工关闭放气带的情况下,该型发动机的共同工作线确定地穿越喘振区域,从最大状态收油门减速将会导致该型发动机进入不稳定工作。数据分析中发现压气机第一级静子机匣壁面静压对节流最为敏感,且静压脉动分量的概率密度函数分布随节流有规律地发生变化。定义了概率密度函数特征值θ来量化这种变化。进一步的数据分析表明,θ可以反映压气机第一级端部的流动分离情况,可以作为试验发动机节流过程中的气动稳定性指标。与直接检测模态扰动和短周期扰动相比,监测θ的变化可以为该型发动机提供较长的失速预警时间。 

关 键 词:航空、航天推进系统   气动不稳定   概率密度函数   实验   压气机   旋转失速   喘振
文章编号:1000-8055(2005)04-0567-05
收稿时间:2004-05-31
修稿时间:2004-05-31

Application of Probability Density Function Analysis in the Monitoring of Engine Aerodynamic Instability Precursor
ZHANG Pu,LI Ying-hong,WU Yun,LIU Jian-xun and ZHANG Bai-ling. Application of Probability Density Function Analysis in the Monitoring of Engine Aerodynamic Instability Precursor[J]. Journal of Aerospace Power, 2005, 20(4): 567-571
Authors:ZHANG Pu  LI Ying-hong  WU Yun  LIU Jian-xun  ZHANG Bai-ling
Affiliation:Propulsion System Laboratory,Engineering Institute, Airforce Engineering University,Xi’an710038,China
Abstract:Experiments were performed to investigate surge problem of a single shaft axial flow turbojet engine during throttling.If the discharge bleed valve of the engine is closed manually,the working line of the engine will traverse the stalling region in a mass flow range,thus throttling from full speed may surely transit the engine into unstable operation.It is observed that the casing wall static pressure of the first compressor stage stator is most sensitive to throttling operation, and that probability density functions of the pulsating components of the static pressure vary accordingly.An eigenvalue,θ,is then introduced to quantify the variation of probability density functions.Further data analysis demonstrates that eigenvalue θ is capable of reflecting some aspects of flow separation in the tip region of the first compressor stage, and that θ may serve as an indicator of imminent aerodynamic instability of the engine, thus long stall warning time of the examined turbojet engine is achievable than that to directly detect modes or spikes. 
Keywords:aerospace propulsion system  aerodynamic instability  probability density function  experimental investigation  compressor  rotating stall  surge
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