Experimental and numerical investigation on aerodynamic stability of steam ingestion in a compressor
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摘要: 研究蒸汽吸入和旋流畸变对压气机气动稳定性的影响,以某两级低速轴流压气机为试验研究对象,建立压气机蒸汽吸入和旋流畸变试验台。试验结果表明:压气机吸入蒸汽引起入口总压和总温畸变,转速增加,总压畸变强度增大,总温畸变强度减小。蒸汽吸入导致总压比和稳定裕度降低,当压气机转速为600 r/min和800 r/min时,稳定裕度分别降低15%和63%。蒸汽吸入和反向整体涡旋流畸变两者共同作用下稳定裕度下降更为显著,当转速为600 r/min和800 r/min时,稳定裕度分别降低630%和1264%。对试验压气机进行蒸汽吸入数值模拟研究,结果表明:压气机转速为600 r/min和800 r/min时,稳定裕度分别降低321%和812%。Abstract: In order to investigate the effect of steam ingestion and swirl distortion on the aerodynamic stability of the compressor, a two-stage low-speed axial compressor was used as the experimental research object. The compressor test bench for steam ingestion and swirl distortion was established. The experimental results showed that steam ingestion caused the inlet total pressure and total temperature distortion. With the increase of rotating speed, the total pressure distortion intensity increased and the total temperature distortion intensity decreased. Steam ingestion caused the decrease of total pressure ratio and stability margin. When the compressor rotating speed was 600 r/min and 800 r/min, the stability margin was reduced by 15% and 63%, respectively. The stability margin decreased more significantly when the steam ingestion and the reverse bulk swirl distortion were combined. When the compressor rotating speed was 600 r/min and 800 r/min, the stability margin was reduced by 630% and 1264%. Numerical simulation investigated the effect of steam ingestion on the experimental compressor. The results showed that the stability margin decreased by 321% and 812% when the compressor rotating speed was 600 r/min and 800 r/min, respectively.
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[1] MARKS B,MELTON H,LAWRENCE T.Normalization of F/A-18E/F flight demonstrated dynamic minimum control airspeeds to reference conditions[R].AIAA-2001-0409,2001. [2] GANNON A J,HOBSON G V,PAYNE T A,et al.The effect of steam ingestion on transonic rotor stall margin[R].ASME Paper 2007-GT-28068,2007. [3] LONGLEY J P,SHIN H W,PLUMLEY R E,et al.Effects of rotating inlet distortion on multistage compressor stability[J].Journal of Turbomachinery,1996,118(2):181-188. [4] BEALE D K,CRAMER K B,KING P S.Development of improved methods for simulating aircraft inlet distortion in turbine engine ground tests[R].AIAA-2002-3045,2002. [5] SGHAIER T B,MEHDI A,PACHIDIS V,et al.A parametric numerical study of the effects of inlet swirl distortion on a transonic compressor stage[R].ASME Paper 2013-GT-94374,2013. [6] 徐浩洋,胡骏,屠宝锋.蒸汽吸入对稳定性影响中修正关联方法的研究[J].推进技术,2019,40(3):532-541. XU Haoyang,HU Jun,TU Baofeng.Numerical simulation for effects of steam ingestion on stability with improved correlation method[J].Journal of Propulsion Technology,2019,40(3):532-541.(in Chinese) [7] COLLIN R,HEDGE S.Computational fluid dynamic model of steam ingestion into a transonic compressor[D].Monterey,US:Naval Postgraduate School,2009. [8] 屠宝锋,胡骏,张凯.整体涡对跨声速单转子性能和稳定性影响[J].航空动力学报,2016,31(9):2233-2238. TU Baofeng,HU Jun,ZHANG Kai.Effect of bulk swirl on performance and stability of transonic single rotor[J].Journal of Aerospace Power,2016,31(9):2233-2238.(in Chinese) [9] PAYNE T A.Inlet flow-field measurements of a transonic compressor rotor prior to and during steam-induced rotating stall[D].Monterey,US:Naval Postgraduate School,2005. [10] ZARRO S E.Steady-state and transient measurements within a compressor rotor during steam-induced stall at transonic operational speeds[D].Monterey,US:Naval Postgraduate School,2006. [11] JOESPH J,KOESSLE R.Experimental investigation of high-pressure steam induced stall of a transonic rotor[D].Monterey,US:Naval Postgraduate School,2007. [12] TU Baofeng,ZHANG Luyao,HU Jun.The effect of high-temperature steam ingestion on aerodynamic performance and stability of a transonic rotor[J].Journal of Aerospace Engineering,2019,233(9):3351-3367. [13] 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) [14] 张环,胡骏,屠宝锋,等.旋转进气畸变对压气机气动稳定性及失速起始特性的影响[J].航空动力学报,2008,23(11):2095-2100. ZHANG Huan,HU Jun,TU Baofeng,et al.Effects of rotating inlet distortion on aerodynamic stability and stall inception of axial-flow compressor[J].Journal of Aerospace Power,2008,23(11):2095-2100.(in Chinese) [15] 刘华,屠宝锋,胡骏,等.旋流畸变对压气机失速发展过程影响的试验研究[J].推进技术,2017,38(10):2306-2313. LIU Hua,TU Baofeng,HU Jun,et al.Experimental investigation of compressor stall development induced by inlet swirl distortion[J].Journal of Propulsion Technology,2017,38(10):2306-2313.(in Chinese) [16] GANNON A J,HOBSON G V,HEDGES C R,et al.Investigation and prediction of steam-induced stall-margin reduction in two transonic rotor fans[J].Journal of Fluids Engineering,2014,36(11):101-111. [17] 孙兰昕.燃气轮机湿压缩性能与水滴运动研究[D].哈尔滨:哈尔滨工程大学,2012. SUN Lanxin.Study on wet compression performance of gast turbine and droplet motion[D].Harbin:Harbin Engineering University,2012.(in Chinese) [18] 罗铭聪.压气机湿压缩特性及水滴运动研究[D].哈尔滨:哈尔滨工程大学,2014. LUO Mingcong.Research of compressor wet compression performance and water droplet motion[D].Harbin:Harbin Engineering University,2014.(in Chinese)
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