周向畸变下轴流压气机的失速预警方法研究及应用

doi:10.13675/j.cnki.tjjs.200344

推进技术 ›› 2020, Vol. 41 ›› Issue (9): 1967-1974.DOI: 10.13675/j.cnki.tjjs.200344

周向畸变下轴流压气机的失速预警方法研究及应用

刘洋^1,2,3,4，李继超^1,2,3,4，杜娟^1,2,3,4，张宏武^1,2,3,4，聂超群^1,2,3,4

1.中国科学院工程热物理研究所先进燃气轮机实验室,北京 100190;2.中国科学院先进能源动力重点实验室,北京 100190;3.中国科学院轻型动力创新研究院,北京 100190;4.中国科学院大学工程科学学院,北京 100049

出版日期:2020-09-15 发布日期:2020-09-15
作者简介:刘洋，博士生，研究领域为叶轮机械非定常流、气动稳定性。E-mail：liuyang18@iet.cn
基金资助:
国家自然科学基金面上项目（51676184）；国家自然科学基金重大科研仪器研制项目（51727810）；国家自然科学基金重点项目（51636001）；国家重大科技专项（2017-Ⅱ-0005-0018，2017-Ⅱ-0005-0017）。

Stall Warning Method Investigation and Application in an Axial-Flow Compressor with Circumferential Distortion

1.Advanced Gas Turbine Laboratory,Institute of Engineering Thermophysics,Chinese Academy of Sciences, Beijing 100190,China;2.Key Laboratory of Advanced Energy and Power,Chinese Academy of Sciences,Beijing 100190,China;3.Innovation Academy for Light-Duty Gas Turbine,Chinese Academy of Sciences,Beijing 100190,China;4.School of Engineering Science,University of Chinese Academy of Sciences,Beijing 100049,China

Online:2020-09-15 Published:2020-09-15

摘要/Abstract

摘要： 为了探究进气畸变条件下轴流压气机的有效失速预警方法并将其应用于主动控制系统中，在一台低速单转子轴流压气机上对均匀进气和周向畸变条件下的失速预警方法进行了实验研究。实验通过在进口布置高度可调节的插板来产生不同强度的周向畸变，并通过在转子叶顶布置的动态压力传感器测得非定常压力信号，运用自相关、互相关和均方根算法对其进行分析，比较了周向畸变下三种失速预警方法的可靠性。分析结果表明：只有传感器安装在畸变区时自相关和均方根分析才有效；互相关分析不依赖于传感器的安装位置，在畸变区和非畸变区均能有效感受到畸变的影响，且互相关系数随着周向畸变的产生或消失相应地下降或上升，因此在周向畸变下互相关分析为更有效的失速预警方法；最后在基于互相关分析的基础上对该单转子轴流压气机实施了喷气主动控制应用，在24.75%畸变强度条件下，主动喷气能取得9.32%的失速裕度改善，与定常喷气相比，获得几乎相等的失速裕度改善的同时节省了约40%的喷气量。

关键词: 轴流压气机;进气畸变;失速预警;主动控制;喷气

Abstract: To investigate the feasible stall warning method for active control application in axial compressors with inlet distortion, stall warning methods were experimentally studied in a low-speed isolated-rotor axial compressor under uniform inflow and circumferential distortion. A flat-baffle was installed with different height to generate different distortion intensity. Unsteady pressures were obtained by high-response transducers at tip region and analyzed by auto-, cross- and root mean square (RMS) algorithms to compare the reliability of three stall warning methods with circumferential distortion. The analytical results show that compared to auto-correlation and root mean square analysis which are reliable only at distorted region, cross-correlation analysis can sensibly react to the circumferential distortion not dependent on the transducers’ location. Moreover, cross-correlation coefficient correspondingly decreases or increases with the generation or disappearance of circumferential distortion. Therefore, the cross-correlation analysis is the most effective one among these three stall warning methods. Additionally, the active control was implemented based on cross-correlation analysis in studied isolated-rotor axial compressor. Active injection can obtain 9.32% stall margin improvement under 24.75% distortion intensity condition, saving about 40% injected energy with nearly an equal stall margin improvement compared to steady injection.

Key words: Axial compressor;Inlet distortion;Stall warning;Active control;Injection

刘洋，李继超，杜娟，张宏武，聂超群. 周向畸变下轴流压气机的失速预警方法研究及应用[J]. 推进技术, 2020, 41(9): 1967-1974.

LIU yang^1,2,3,4, LI Ji-chao^1,2,3,4, DU Juan^1,2,3,4, ZHANG Hong-wu^1,2,3,4, NIE Chao-qun^1,2,3,4. Stall Warning Method Investigation and Application in an Axial-Flow Compressor with Circumferential Distortion[J]. Journal of Propulsion Technology, 2020, 41(9): 1967-1974.

参考文献

[1] Day I. Stall Inception in Axial Flow Compressors[J]. Journal of Turbomachinery, 1991， 115: 1-9.
[2] McDougall N M， Cumpsty N A， Hynes T P. Stall Inception in Axial Compressors[J]. Journal of Turbomachinery， 1990， 112(1): 116?123.
[3] Tahara N， Kurosaki M， Ohta Y， et al. Early Pre-Stall Investigation by Sensitive Stall Warning Technique[C]. Tokyo:Proceeding of the International Gas Turbine Congress， 2003.
[4] Li J C. Self-Adaptive Stability Enhancing Technology with Tip Air Injection in an Axial Flow Compressor[J]. Journal of Turbomachinery， 2017， 139(1): 1-9.
[5] Li J C， Liu Y， Du J， et al. Automatic Stability Control Using Tip Air Injection in a Multi-Stage Axial Compressor[J]. Aerospace Science and Technology， 2020， 98: 1-12.
[6] Young A， Day I， Pullan G. Stall Warning by Blade Pressure Signature Analysis[J]. Journal of Turbomachinery， 2012， 134(1): 1-10.
[7] Li F Y， Li J， Dong X， et al. Stall-Warning Approach Based on Aero-Acoustic Principle[J]. Journal of Propulsion and Power， 2016， 32(6): 1-13.
[8] Li J C， Lin F， Tong Z T， et al. The Dual Mechanisms and Implementations of Stability Enhancement with Discrete Tip Injection in Axial Flow Compressor[J]. Journal of Turbomachinery， 2015， 137(3): 1-10.
[9] Du J， Lin F， Zhang H W， et al. Numerical Investigation on the Self-Induced Unsteadiness in Tip Leakage Flow for a Transonic Fan Rotor[J]. Journal of Turbomachinery， 2010， 132(2): 1-9.
[10] Lin F， Zhang J X， Chen J Y， et al. Flow Structure of Short Length Scale Disturbance on an Axial Compressor[J]. Journal of Propulsion and Power， 2008， 24(6): 1301-1308.
[11] Tong Z， Lin F， Chen J Y， et al. The Self-Induced Unsteadiness of Tip Leakage Vortex and Its Effect on Compressor Stall Inception[C]. Montreal: ASME Turbomachinery Technical Conference， 2007.
[12] Lin F， Chen J Y， Li M L. Wavelet Analysis of Rotor-Tip Disturbances in an Axial-Flow Compressor [J]. Journal of Propulsion and Power， 2004， 20(2): 319?334.
[13] Lin F， Li M L， Chen J Y. Long-to-Short Length-Scale Transition: A Stall Inception Phenomenon in an Axial Compressor with Inlet Distortion [J]. Journal of Turbomachinery， 2006， 128(1): 130-140.
[14] Liu Y， Li J C， Du J， et al. Application of Fast Wavelet Analysis on Early Stall Warning in Axial Compressors [J]. Journal of Thermal Science， 2019， 28(5).
[15] Day I. Active Suppression of Rotating Stall and Surge in Axial Compressors[J]. Journal of Turbomachinery， 1993， 115(1): 40-47.
[16] Weigl H J， Paduano J D， Frechette L G， et al. Active Stabilization of Rotating Stall and Surge in a Transonic Single Stage Axial Compressor [C]. Orlando: International Gas Turbine & Aeroengine Congress & Exhibition， 1997.
[17] Tahara N， Nakajima T， Kurosaki M， et al. Active Stall Control with Practicable Stall Prediction System Using Auto-Correlation Coefficient [C]. Salt Lake City: AIAA Joint Propulsion Conference， 2001.
[18] 屠宝锋，胡骏，王志强，等. 进气畸变下低速轴流压气机失速起始特性试验[J]. 推进技术， 2010， 31(4): 428-437.
[19] 郭晋，胡骏，屠宝锋，等. 大涵道比风扇/增压级进气畸变数值模拟研究 [J]. 推进技术， 2019， 40(11): 2498-2504.
[20] Nie C Q， Zhang J X， Tong Z T， et al. The Response of a Low Speed Compressor on Rotating Inlet Distortion[J]. Journal of Thermal Science， 2006， 15(4): 314-318.
[21] Zhang W， Mehdi V. A Parametric Study of the Effects of Inlet Distortion on Fan Aerodynamic Stability[J]. Journal of Turbomachinery， 2019， 141（1）.
[22] Li J C， Du J， Geng S J， et al. Tip Air Injection to Extend Stall Margin of Multi-Stage Axial Flow Compressor with Inlet Radial Distortion[J]. Aerospace Science and Technology， 2020， 96:1-13.
[23] Spakovszky Z S， Weigl H J， Paduano J D， et al. Rotating Stall Control in a High-Speed Stage with Inlet Distortion， Part I: Radial Distortion[J]. Journal of Turbomachinery， 1999， 121: 510-517.
[24] Spakovszky Z S， C M van Schalkwyk ， Weigl H J， et al. Rotating Stall Control in a High-Speed Stage with Inlet Distortion， Part II: Circumferential Distortion[J]. Journal of Turbomachinery， 1999， 121: 517-524.

周向畸变下轴流压气机的失速预警方法研究及应用

Stall Warning Method Investigation and Application in an Axial-Flow Compressor with Circumferential Distortion

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 0

编辑推荐

Metrics

本文评价