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基于压力信号分析的轴流式压气机失速预测

张海波 徐植桂

南京航空航天大学学报2017,Vol.49Issue(5):684-692,9.
南京航空航天大学学报2017,Vol.49Issue(5):684-692,9.DOI:10.16356/j.1005-2615.2017.05.012

基于压力信号分析的轴流式压气机失速预测

Study on Stall Detection of Axial Compressor Through Pressure Signal Analysis

张海波 1徐植桂1

作者信息

  • 1. 南京航空航天大学能源与动力学院 ,南京 ,210016
  • 折叠

摘要

Abstract

In order to obtain the steady working point of compressor working state and build the relation-ship between compressor working state of near surge stall and compressor pressure signal ,the near surge stall test for the low speed two-stage axial compressor is carried out at different speeds under uni-form inlet and distortion inlet to measure the pressure signals of the compressor from normal operation to stall condition in real time ,and a compressor stall prediction algorithm based on autocorrelation coef-ficient is proposed in the time domain to predict and analyze the pressure signals of compressor inlet , outlet and the tip position of the head rotor .The results show that the proposed prediction algorithm has good stall prediction ability ,and the blade tip ,20% from the blade leading edge ,is most suitable as the observation points for the stall prediction of the compressor ,w here the compressor blade tip pres-sure self correlation data has obvious monotonic correlation with compressor surge margin .

关键词

失速预测/轴流式压气机/压力信号

Key words

stall detection/axial compressor/pressure signal

分类

航空航天

引用本文复制引用

张海波,徐植桂..基于压力信号分析的轴流式压气机失速预测[J].南京航空航天大学学报,2017,49(5):684-692,9.

基金项目

中央高校科研业务费(NZ2016103)资助项目. (NZ2016103)

南京航空航天大学学报

OA北大核心CSCDCSTPCD

1005-2615

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