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基于临界B参数的航空发动机压气机喘振监测研究

欧阳运芳 李建兰

流体机械2017,Vol.45Issue(7):34-37,51,5.
流体机械2017,Vol.45Issue(7):34-37,51,5.DOI:10.3969/j.issn.1005-0329.2017.07.007

基于临界B参数的航空发动机压气机喘振监测研究

Study on Monitoring of Compressor Surge Based on the critical B Parameter

欧阳运芳 1李建兰2

作者信息

  • 1. 上海中航商用航空发动机制造有限责任公司,上海 201306
  • 2. 华中科技大学,湖北武汉 430074
  • 折叠

摘要

Abstract

Surge is one of the most serious faults in aero-engine compressor.Effective monitoring of surge ensures the flight safety of airplane.This paper presents a new method for monitoring of aero-engine compressor surge based on critical B parameter. Based on the Moore-Greitzer incompressible compressor model,the stability of the compression system is analyzed in this paper. Furthermore,the critical B parameter expression is derived by the bifurcation theory.Finally,the whole state Bcr surface figure is obtained and the unstable behavior of the compressor in the operation state can be real-time monitored and predicted.

关键词

航空发动机/压气机/喘振/分叉分析/临界B参数

Key words

aero-engine/compressor/surge/bifurcation analysis/critical B parameter

分类

机械制造

引用本文复制引用

欧阳运芳,李建兰..基于临界B参数的航空发动机压气机喘振监测研究[J].流体机械,2017,45(7):34-37,51,5.

流体机械

OA北大核心CSCDCSTPCD

1005-0329

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