The Experimental Research on a New Method for Extending the Axial-Compressor’s Stall Margin

LI Zhi-ping; LI Qiu-shi; YUAN Wei; LU Ya-jun; JIANG Hua-bing

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The Experimental Research on a New Method for Extending the Axial-Compressor’s Stall Margin

更新时间：2026-07-07

- The Experimental Research on a New Method for Extending the Axial-Compressor’s Stall Margin
- Vol. 21, Issue 3, (2006)
- 作者机构：
  
  北京航空航天大学航空航天大学能源与动力工程学院航空发动机气动热力重点实验室,北京,100083
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2006
- 稿件说明：
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LI Zhi-ping, LI Qiu-shi, YUAN Wei, et al. The Experimental Research on a New Method for Extending the Axial-Compressor’s Stall Margin[J]. 2006, 21(3).
DOI：

LI Zhi-ping, LI Qiu-shi, YUAN Wei, et al. The Experimental Research on a New Method for Extending the Axial-Compressor’s Stall Margin[J]. 2006, 21(3). DOI：

摘要

采用外部绕流激励的方法研究非定常绕流对压气机气动稳定性的影响规律

并在此基础上探索了该措施的工程应用前景。通过模型实验验证了利用压气机内叶排间绕流的非定常耦合作用

优化匹配其周向气动布局方案

可有效的提升压气机稳定工作裕度

并改善其气动稳定性。结果表明:当绕流撞击强度达到某一阈值

并且当非定常绕流频率与非定常旋涡脱落特征频率发生耦合时

可较大幅度的提高压气机稳定工作裕度

其相对值可提高约22.1%。这一结论在压气机不同的折合转速工作状态下仍然得到了验证。

Abstract

Firstly

investigating the influences of unsteady disturbance on compressor’s aerodynamic stability by exterior excitation

and then exploring the new method’s outlook for engineering application by utilizing the unsteady wake impact cooperative effect in adjacent blades of compressor.Furtherly

the model experiment proved that the goal which increasing the compressor’s aerodynamic performance and aerodynamic stability can be realized by optimizing the unsteady aerodynamic circumference configuration technique in compressor.The experiment results indicated that the stall margin can be increased greatly when excitation amplitude exceeded the threshold value and excitation frequency cooperated with the typical vortex shedding frequency

the stall margin can be increased 22.1% relatively.On the other hand

the cooperative effects of WIE(Wake Impact Effect

WIE) at different correct rotating speed were investigated in detail.

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Related Author

JIANG Hua-bing

LU Ya-jun

YUAN Wei

LI Qiu-shi

HOU An-ping

SUN Da-kun

HOU Rui-wei

SUN Xiao-feng

Related Institution

National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics

School of Jet Propulsion, Beijing University of Aeronautics and Astronautics

The Engineering Institute, Air Force Engineering University

Institute of Engineering Thermophysics, Chinese Academy of Sciences

Graduate School, Chinese Academy of Sciences

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