Surge experimentation research for a whole turbine-shaft engine

KUANG Gui-lan; YAO Zheng-rong; WANG Dao-bo; Wu Zhi-yong; Peng Wen-wen

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Surge experimentation research for a whole turbine-shaft engine

更新时间：2026-07-07

- Surge experimentation research for a whole turbine-shaft engine
- Vol. 24, Issue 3, (2009)
- 作者机构：
  
  1. 南京航空航天大学能源与动力学院,南京,210016
  2. 中国航空动力机械研究所,株洲,412002
  3. 南京航空航天大学自动化学院,南京,210016
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2009
- 稿件说明：
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KUANG Gui-lan, YAO Zheng-rong, WANG Dao-bo, et al. Surge experimentation research for a whole turbine-shaft engine[J]. 2009, 24(3).
DOI：

KUANG Gui-lan, YAO Zheng-rong, WANG Dao-bo, et al. Surge experimentation research for a whole turbine-shaft engine[J]. 2009, 24(3). DOI：

摘要

根据某型涡轴发动机研制的需要

在整机试验台进行了逼喘试验方法的探索

本文详述了发动机逼喘、试验方法设计、试验装置及试验过程

最后对试验结果进行了分析

研究结果表明利用该发动机上的飞机引气口接入高压气源的方法能够成功地进行该型发动机的整机逼喘试验

从而能够真实获得压气机装在整机上工作时的喘振边界线.

Abstract

For the requirement of a turbine-shaft engine research

surge experimentation had been done exploringly in a whole engine test-bed.This paper describes engine surge

the design of surge experimentation method

experimentation equipment and the process of the experimentation.In the end

the results of the experimentation have been analysed and summarized

the results make clear that the experimentation method is valid

connecting high pressure air to the engine bleeds can do the engine surge experimentation successfully.Consequently the real surge margin of the compressor installed in the overall engine can be gotten.

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Related Author

KUANG Gui-lan

WANG Dao-bon

WU Wei-li

YUE Li

YAO Zheng-rong

KUANG Gui-lan

SHAN Xiao-ming

WU Zhi-yong

Related Institution

Measurement and Control Technology Laboratory, China Aviation Powerplant Research Institute

China Aviation Powerplant Research Institute, Aviation Industry Corporation of China

School of Astronautics, Beijing University of Aeronautics and Astronautics

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