Experiment on surge phenomenon of small multi-stage axial compressor
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摘要: 针对某小尺寸多级轴流压气机,在首级转子叶顶沿弦向布置Kulite动态压力传感器以及在后面级插入高频压力探针,通过动态测量试验,研究不同转速下多级轴流压气机喘振现象.结果表明:在中高转速下,该压气机深度喘振是由模态波扰动发展成旋转失速,从而引起流动堵塞,最终导致流动崩溃所造成的;在低转速下,压气机轻度的经典喘振由模态波直接引起的,在喘振周期内一直伴随有旋转失速的产生、发展和消失.Abstract: An experimental investigation on the compressor surge phenomenon was carried out in a small multi-stage axial compressor under different rotor speeds. The dynamic pressure signals of 1st rotor tip were measured by the Kulite dynamic pressure transducers and the fast response pressure probes. Results indicated that, at mid and higher rotor speed, the modal wave appears and evolves into rotating stall in the pre-surge period and, subsequently, the compressor is rapidly brought to deep surge by the huge blockage of the stall cell; However, at lower rotor speed, the classical surge is directly triggered by modal wave with the existence of rotating stall in the surge cycle.
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[1] 刘大响,叶培梁,胡俊,等.航空燃气涡轮发动机稳定性设计与评定技术[M].北京:航空工业出版社,2004. [2] Pampreen R C.Compressor surge and stall[M].Norwich:Concepts ETI Incroporated,1993. [3] Greitzer E M.Surge and rotating stall in axial flow compressors:Part 1 theoretical compression system model[J].Journal of Engineering for Power,1976,98(2):190-198. [4] Greitzer E M.Surge and rotating stall in axial flow compressors:Part 2 experimental results and comparisons with theory[J].Journal of Engineering for Power,1976,98(2):199-211. [5] Greitzer E M,Moore F K.A theory of post-stall transients in axial compression systems:Part 1 development of equations[J].Journal of Engineering for Gas Turbines and Power,1986,108(1):68-76. [6] Greitzer E M,Moore F K.A theory of post-stall transients in axial compression systems:Part 2 application[J].Journal of Engineering for Gas Turbines and Power,1986,108(2):231-239. [7] Garnier V H,Epstein A H,Greitzer E M.Rotating waves as a stall inception indication in axial compressor[J].Journal of Turbomachinery,1991,113(2):390-301. [8] Day I J.Active suppression of rotating stall and surge in axial compressors[J].Journal of Turbomachinery,1993,115(1):40-47. [9] Courtiade N.Experimental analysis of the unsteady flow and instabilities in a high-speed multistage compressor[D].Ecully:Ecole Centrale de Lyon,2012. [10] Courtiade N.Experimental study of surge precursors in a high-speed multistage compressor[R].ASME Paper GT2012-68321,2012. [11] 朱俊强,刘志伟.多叶排旋转失速起始的研究[J].航空动力学报,1993,8(1):24-28. ZHU Junqiang,LIU Zhiwei.Research of onset of rotating stall for multiple blade rows[J].Journal of Aerospace Power,1993,8(1):24-28.(in Chinese) [12] 张环,胡骏,刘大响,等.旋转总压畸变对压气机气动稳定性影响的二维不可压缩模型[J].航空动力学报,2009,24(8):1773-1784. ZHANG Huan,HU Jun,LIU Daxiang,et al.Two-dimensional incompressible model of effects of rotating inlet distortion on flow instability in compression systems[J].Journal of Aerospace Power,2009,24(8):1773-1784.(in Chinese) [13] Sun X F.Three-dimensional compressible flow stability theory of rotating stall[R].Beijing University of Aeronautics and Astronautics Technical Report BH-B4765,1996. [14] 聂超群,陈静宜,蒋浩康,等.低速轴流压气机旋转失速先兆特征的试验分析[J].工程热物理学报,1998,19(3):293-298. NIE Chaoqun,CHEN Jinyi,JIANG Haokang,et al.Experimental investigation on inception of rotating stall in a low-speed axial compressor[J].Journal of Engineering Thermophysics,1998,19(3):293-298.(in Chinese) [15] 屠宝锋,胡骏,王志强,等.低速轴流压气机旋转失速特性试验[J].航空动力学报,2009,24(1):143-149. TU Baofeng,HU Jun,WANG Zhiqiang,et al.Experimental investigation on characteristic of rotating stall in a low-speed axial compressor[J].Journal of Aerospace Power,2009,24(1):143-149.(in Chinese) [16] 单晓明,姚峥嵘,岳林,等.组合压气机旋转失速特征的小波分析[J].航空动力学报,2012,27(5):1015-1021. SHAN Xiaoming,YAO Zhengrong,YUE Lin,et al.Wavelet analysis of features of rotating stall in a combined compressor[J].Journal of Aerospace Power,2012,27(5):1015-1021.(in Chinese) [17] 马宏伟,贺象,单晓明,等.一种测量跨声速多级压气机转子出口二维流场的方法[J].推进技术,2013,34(6):754-759. MA Hongwei,HE Xiang,SHAN Xiaoming,et al.Method of measuring 2D dynamic flow-field at exits of transonic multistage compressor rotor[J].Journal of Propulsion Technology,2013,34(6):754-759.(in Chinese) [18] Day I J,Cumpsty N A.The measurement and interpretation of flow within rotating stall cells in axial compressors[J].Journal of Mechanical Engineering Sciences,1978,20(2):101-114.
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