Dynamic Model and Simulation of Compressor Rotating Stall and Surge

Journal of Propulsion Technology ›› 2016, Vol. 37 ›› Issue (5): 960-965.

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Dynamic Model and Simulation of Compressor Rotating Stall and Surge

School of Power and Energy，Northwestern Polytechnical University，Xi’an 710072，China,School of Power and Energy，Northwestern Polytechnical University，Xi’an 710072，China,China Aviation Media Group，Beijing 100012，China and School of Power and Energy，Northwestern Polytechnical University，Xi’an 710072，China

Published:2021-08-15

压气机失速与喘振动态模型与仿真

苏三买¹,孙占恒¹,吕烨²,刘俊杰¹

西北工业大学动力与能源学院，陕西西安 710072,西北工业大学动力与能源学院，陕西西安 710072,中航出版传媒有限责任公司，北京 100012,西北工业大学动力与能源学院，陕西西安 710072

作者简介:苏三买，男，博士，副教授，研究领域为航空发动机建模与仿真。
基金资助:
航空科学基金(2013ZB53019)。

Abstract

Abstract: It is essential to develop compressor dynamic model representing transient behavior of rotating stall and surge for aeroengine active stability control. Based on Moore-Greitzer incompressible compressor model which failed in reflecting the rotation characteristics of stall cell around compressor circumference，a multidimensional state space distributed model with flow，pressure rise and loss variables was established through spatial discretization in circumferential points，in which，the compressor local flow，pressure rise，rotators and stators dynamic and static loss were reconstructed by Spatial Fourier Modes. It is proved by theoretical analysis and numerical simulation that the distributed model is available not only for calculating characteristics of compressor under stable，stall and surge conditions，but also capturing transient behavior about flow and pressure changes around compressor circumference.

Key words: Compressor；Rotating stall and surge；Distributed model；Dynamic simulation

摘要： 建立失速与喘振动态数学模型是压气机主动稳定控制的基础。针对Moore-Greitzer不可压缩压气机模型无法描述失速时失速团沿压气机周向旋转特性的不足，以该模型为基础，在压气机周向环面位置进行模型空间离散化，采用空间傅里叶模态重构压气机局部流量、压升、转子与静子的动静态损失，建立了以流量、压升及损失为状态变量的多维状态空间方程形式分布式压气机模型。理论分析及仿真表明，所建模型既可实现稳态、失速、喘振工况下的压气机外部特性计算，也可模拟失速与喘振状态下压气机内部沿周向的流量及压力变化，实现失速与喘振动态特性仿真。

关键词: 压气机；失速与喘振；分布式模型；动态仿真

SU San-mai¹,SUN Zhan-heng¹,LV Ye²,LIU Jun-jie¹. Dynamic Model and Simulation of Compressor Rotating Stall and Surge[J]. Journal of Propulsion Technology, 2016, 37(5): 960-965.

苏三买,孙占恒,吕烨,刘俊杰. 压气机失速与喘振动态模型与仿真[J]. 推进技术, 2016, 37(5): 960-965.

References

[1] 楚武利, 刘前智, 胡春波. 航空叶片机原理[M]. 西安:西北工业大学出版社, 2009.
[2] Epstein A H, FfowcsWilliams J E, Greitzer E M. Active Suppression of Aerodynamic Instabilities in Turbomachines[J]. Journal of Propulsion and Power, 1989, 5(2): 204-211.
[3] Frank Willems, Bram de Jager. Active Compressor Surge Control Using a One-Sided Controlled Bleed/Recycle Valve[C]. Florida: Proceedings of the 37th IEEE Conference on Decision & Control, 1998.
[4] 苏三买, 吕烨, 黄顺炳. 航空发动机主动稳定控制方法分析[J]. 航空工程进展, 2014, 5(1): 7-11.
[5] 吕烨. 航空发动机主动稳定控制建模方法研究[D]. 西安:西北工业大学, 2014.
[6] Shunbing Huang, Sanmai Su. Key Technology Analysis for Active Compressor Stabilization Control of Aero-Engine[C]. Jilin: 2011 International Conference on Mechatronic Science, Electric Engineering and Computer, 2011.
[7] 王鹏. 某型涡扇发动机气动稳定性模拟[D]. 西安:西北工业大学, 2006.
[8] 蒋康涛. 低速轴流压气机旋转失速的数值模拟研究[D]. 北京:中国科学院研究生院, 2004.
[9] 胡江峰, 竺晓程, 羌晓青, 等. 基于节流阀模型跨声速轴流压气机失速特性研究[J]. 推进技术, 2013, 34(6): 741-746. (HU Jiang-feng, ZHU Xiao-cheng, Qiang Xiao-qing, et al. Investigation on Stall Behavior in a Transonic Axial Compressor Based on Throttle Model[J]. Journal of Propulsion Technology, 2013, 34(6):741-746.)
[10] 屠宝锋, 胡骏. 旋转总压畸变对压气机稳定性影响的三维非定常模型[J]. 航空动力学报, 2011, 26(2):255-261.
[11] Greitzer E M. Surge and Rotating Stall in Axial Flow Compressors, Part I: Theoretical Compression System Model[J]. Journal of Engineering for Power, 1976, 98(2): 190-198.
[12] Moore F K, Greitzer E M. A Theory of Post-Stall Transients in a Axial Compressor Systems: Part I: Development of Equations[J]. Journal of Engineering for Gas Turbines and Power, 1986, 108(1): 68-76.
[13] Jun Hu, Leonhard Fottner. A New Simplified Model of Post Stall Transients in Axial Compression Systems[J]. Journal of Thermal Science, 1999, 8(3): 176-189.
[14] 黄伟, 黄向华. 基于二阶滑模的压气机喘振主动控制[J]. 中国机械工程, 2013, 24(21): 2852-2855.
[15] 于兰兰, 胡俊, 屠宝锋, 等. 轴流压缩系统中主动抑制旋转失速的数值模拟[J]. 航空动力学报, 2010, 25(1): 92-101.
[16] 王健, 李应红, 张东方, 等. 基于分岔理论的轴流式压气机旋转失速主动控制技术[J]. 航空动力学报, 2007, 22(7): 1179-1183.
[17] Behnken R L. Nonlinear Control and Modeling of Rotating Stall in an Axial Flow Compressor[D]. California: California Institute of Technology Pasadena, 1996.
[18] Mansoux C A, Gysling D L, Setiawan J D, et al. Distributed Nonlinear Modeling and Stability Analysis of Axial Compressor Stall and Surge[C]. USA: InProc. American Control Conference, 1994: 2305-2316.
[19] Paduano J D. Active Control of Rotating Stall in Axial Compressors[D]. Cambridge: Massachusetts Institute of Technology, 1992. 　　　　　　　　　　　　　*　收稿日期:2014-11-22；修订日期:2015-02-05。基金项目:航空科学基金(2013ZB53019)。作者简介:苏三买,男,博士,副教授,研究领域为航空发动机建模与仿真。E-mail: microeng@nwpu.edu.cn(编辑:史亚红)

Dynamic Model and Simulation of Compressor Rotating Stall and Surge

压气机失速与喘振动态模型与仿真

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