吸附式低反动度轴流压气机气动设计方法在多级轴流压气机中的应用

胡应交; 王松涛

doi:10.13224/j.cnki.jasp.2014.11.004

吸附式低反动度轴流压气机气动设计方法在多级轴流压气机中的应用

doi: 10.13224/j.cnki.jasp.2014.11.004

哈尔滨工业大学能源科学与工程学院发动机气体动力研究中心, 哈尔滨 150001

详细信息

作者简介:
胡应交(1985-),男,湖南隆回人,博士生,主要从事高负荷压气机气动设计技术研究.

中图分类号: V231;TK474.7
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出版历程
- 收稿日期: 2013-07-13
- 刊出日期: 2014-11-28

Application of design method of low reaction and aspiration axial compressor in multistage axial compressor

Engine Aerodynamic Research Center, School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China

摘要

摘要: 随着对吸附式低反动度轴流压气机内部流动细节的逐步深入,进一步完善了多级吸附式低反动度轴流压气机气动设计思想,完成了3级吸附式低反动度轴流压气机气动设计.三维黏性的数值计算结果表明:在第1级动叶入口叶尖切线速度为370m/s的前提下,通过只在首级静叶和末级静叶中进行附面层抽吸,实现了总压比为6.1的3级吸附式低反动度轴流压气机气动设计.附面层总抽吸流量占入口流量的11.3%.在不考虑附面层抽吸对流动效率影响的前提下,3级效率达到88.1%.
- 多级 /
- 轴流压气机 /
- 低反动度 /
- 气动设计 /
- 附面层抽吸
Abstract: With further understanding of the internal flow details in the low reaction and aspiration axial compressor stages, the design method of low reaction and aspiration axial compressor used in the three stages was further improved. A verification aerodynamic design of a low reaction and aspiration axial compressor with three stages was carried out. From these three-dimensional viscous numerical results, a compressor was attained with total pressure ratio 6.1 and efficiency 88.1%, without consideration of the influence of the bleed flow at inlet tip tangential speed 370m/s. Boundary layer suction was used only in the first and third stator. The total bleed flow was around 11.3% of the inlet.
- multistage /
- axial compressor /
- low reaction /
- aerodynamic design /
- boundary layer suction

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参考文献(21)

[1]	Grosvenor A D,Brown P M,Lawlor S P.Design methodology and predicted performance for a supersonic compressor stage[R].ASME Paper GT2006-90409,2006.
[2]	Lawlor S P,Hinkey J B,Mackin S G,et al.Supersonic compression stage design & test results[R].ASME IMECE 2004-59914,2004.
[3]	肖翔.对转冲压压气机冲压叶轮内部流动分析[D].北京:中国科学院,2007. XIAO Xiang.The aerodynamic design and analysis of counter-rotating compressor's shock-in impeller[D].Beijing:Chinese Academy of Sciences,2007.(in Chinese)
[4]	Merchant A,Kerrebrock J L,Adamczyk J J,et al.Experimental investigation of a high pressure ratio aspirated fan stage[J].Journal of Turbomachinery,2005,127(1):43-45.
[5]	Merchant A,Epstein A H,Kerrebrock J L.Compressors with aspirated flow control and counter-rotation[R].AIAA-2004-2514,2004.
[6]	Schuler B J,Kerrebrock J L,Merchant A.Experimental investigation of an aspirated fan stage[J].Journal of Turbomachinery,2005,127(2):340-348.
[7]	Kerrebrock J L,Drela M,Merchant A A.A family of designs for aspirated compressors[R].ASME Paper 98-GT-196,1998.
[8]	Merchant A.Aerodynamic design and analysis of a high pressure ratio aspirated compressor stage[R].ASME Paper GT-2000-619,2000.
[9]	Kerrebrock J L,Epstein A H,Merchant A A,et al.Design and test of an aspirated counter-rotating fan[R].ASME Paper GT2006-90582,2006.
[10]	张华良.采用叶片弯/掠及附面层抽吸控制扩压叶栅内涡结构的研究[D].哈尔滨:哈尔滨工业大学,2007. ZHANG Hualiang.Investigation on application of dihedral/swept blade and boundary layer suction to control vortex configurations in compressor cascades[D].Harbin:Harbin Institute of Technology,2007.(in Chinese)
[11]	王松涛,羌晓青.低反动度附面层抽吸式压气机及其内部流动控制[J].工程热物理学报,2009,30(1):35-40. WANG Songtao,QIANG Xiaoqing.Study of low reaction boundary layer suction axial compressor and its internal flow control[J].Journal of Engineering Thermophysics,2009,30(1):35-40.(in Chinese)
[12]	QIANG Xiaoqing,WANG Songtao.Aerodynamic design and analysis of a low-reaction axial compressor stage[J].Chinese Journal of Aeronautics,2008,21(1):1-7.
[13]	宋彦萍,陈浮,赵桂杰,等.附面层吸除对大转角压气机叶栅气动性能影响的数值研究[J].航空动力学报,2005,20(4):561-566. SONG Yanping,CHEN Fu,ZHAO Guijie,et al.Numerical investigation of boundary layer suction in compressor cascade with large turning angels[J].Journal of Aerospace Power,2005,20(4):561-566.(in Chinese)
[14]	陈浮,宋彦萍,赵桂杰,等.附面层吸除对压气机叶栅稠度特性影响[J].工程热物理学报,2005,26(2):211-215. CHEN Fu,SONG Yanping,ZHAO Guijie,et al.Effects of boundary layer suction on the performance of compressor cascade with different solidities[J].Journal of Engineering Thermopysics,2005,26(2):211-215.(in Chinese)
[15]	羌晓青.低反动度附面层抽吸式压气机流动控制及设计方法研究[D].哈尔滨:哈尔滨工业大学,2009. QIANG Xiaoqing.Study of flow control and design methods in low-reaction boundary layer suction compressors[D].Harbin:Harbin Institute of Technology,2009.(in Chinese)
[16]	王松涛,胡应交.低反动度高负荷超声速轴流压气机气动设计方法[J].航空动力学报,2013,28(6):1322-1332. WANG Songtao,HU Yingjiao.Aerodynamic design method of high loaded supersonic axial-compressor with low reaction[J].Journal of Aerospace Power,2013,28(6):1322-1332.(in Chinese)
[17]	胡应交,王松涛,王仲奇.基于动叶出口轴向速度提升的吸附式低反动度超、跨声速轴流压气机气动设计原理及其验证[J].推进技术,2013,34(9):1179-1187. HU Yingjiao,WANG Songtao,WANG Zhongqi.Analysis and verification of aerodynamic design principle of the low-reaction and aspirated supersonic or transonic compressors[J].Journal of Propulsion Technology,2013,34(9):1179-1187.(in Chinese)
[18]	胡应交,王松涛.基于动叶出口轴向速度提升的亚声速吸附式低反动度轴流压气机气动设计原理及其验证[J].航空动力学报,2014,29(3):708-718. HU Yingjiao,WANG Songtao.Aerodynamic design principle and verification for subsonic axial-flow compressor with low reaction based on enhanced axial velocity at rotor outlet[J].Journal of Aerospace Power,2014,29(3):708-718.(in Chinese)
[19]	胡应交,王松涛.一种对转压气机气动设计方法及其验证[J].航空动力学报,2014,29(5):1135-1144. HU Yingjiao,WANG Songtao.An aerodynamic design method and verification for counter-rotating compressor[J].Journal of Aerospace Power,2014,29(5):1135-1144.(in Chinese)
[20]	WANG Songtao,QIANG Xiaoqing,LIN Weichun,et al.A study of parameter selection principle and internal flow mechanism in a multi-stage low-reaction axial flow compressor[R].ASME Paper GT2008-50554,2008.
[21]	王松涛,胡应交,王仲奇.吸附式低反动度轴流压气机气动设计原理分析[J].航空动力学报,2014,29(2):350-362. WANG Songtao,HU Yingjiao,WANG Zhongqi.Aerodynamic design principle of aspirated and low-reaction axial-compressors[J].Journal of Aerospace Power,2014,29(2):350-362.(in Chinese)