| Citation: | KANG Jian-xiong, HUANG Guo-ping, ZHU Jun-qiang, WEN Dian-zhong. Inducer tip endwall bleeding effects on centrifugal compressor stability enhancement[J]. Journal of Aerospace Power, 2014, 29(11): 2561-2569. doi: 10.13224/j.cnki.jasp.2014.11.005 |
| [1] |
刘大响,叶陪梁,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] |
Greitzer E M.Review-axial compressor stall phenomena[J].ASME Journal of Fluids Engineering,1980,102(2):134-150.
|
| [3] |
Kerrcbrock J L,Reijnan C P,Ziminsky W S,et al.Aspirated compressors[R].ASME Paper GT-97-525,1997.
|
| [4] |
Chapman D C.Model 250-C30/C281 compressor development[C]//AGAED Conference Proceedings:Centrifugal Compressors,Flow Phenomenon,and Performance.Neuilly Surseine,FR:Advisory Group for Aerospace Research and Development,1980:201-206.
|
| [5] |
General Motors Corporation.Dual function compressor bleed:United States,US4248566[P].1981-02-03.
|
| [6] |
Gummer V,Goller M,Swoboda M.Numerical investigation of end wall boundary layer removal on highly loaded axial compressor blade rows[J].Journal of Turbomachinery,2008,130(1):011015.1-011015.9.
|
| [7] |
赵斌,李绍斌,周盛.引气对跨声轴流压气机性能的影响[J].北京航空航天大学学报,2011,37(1):15-20. ZHAO Bin,LI Shaobin,ZHOU Sheng.Bleeding impact on performance of transonic axial compressor[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(1):15-20.(in Chinese)
|
| [8] |
王掩刚,牛楠,赵龙波,等.端壁抽吸位置对压气机叶栅角区分离控制的影响[J].推进技术,2010,31(4):433-437. WANG Yangang,NIU Nan,ZHAO Longbo,et al.Effect on corner separation control for high load compressor cascade with different end-wall BLS position[J].Journal of Propulsion Technology,2010,31(4):433-437.(in Chinese)
|
| [9] |
周敏,李航航,唐侃平.低雷诺数下附面层组合抽吸方案对压气机特性影响的研究[J].应用力学学报,2012,29(1):27-31. ZHOU Min,LI Hanghang,TANG Kanping.Combined boundary layer suction effect on compressor characters at low Reynolds number[J].Chinese Journal of Applied Mechanics,2012,29(1):27-31.(in Chinese)
|
| [10] |
Palmer D L,Waterman W F.Design and development of an advanced two-stage centrifugal compressor[J].ASME Journal of Turbomachinery,1995,117(3):205-212.
|
| [11] |
Pratt & Whitney Canada Corp.Mixed flow and centrifugal compressor for gas turbine engine:United States,US6488469 B1[P].2002-12-03.
|
| [12] |
Dobrzynski B,Saathoff H,Kosyna G,et al.Active flow control in a single-stage axial compressor using tip injection and endwall boundary layer removal[R].ASME Paper GT2008-50214,2008.
|
| [13] |
DENG Xiangyang,Elizabeth A L,FENG Jinzhang.Time-accurate calculations of a passive shroud bleed configuration and implications for unsteady blade loading[R].ASME Paper GT2011-45777,2011.
|
| [14] |
WANG Tong,XU Wei,GU Chuangang,et al.A new type of self-adaptive casing treatment for a centrifugal compressor[R].ASME Paper GT2010-23457,2010.
|
| [15] |
戴四敏.导风轮轮罩引气对离心式压气机性能影响的数值研究[J].航空动力学报,2005,20(1):125-129. DAI Simin.Numeric simulation of inducer shroud bleeding effect on centrifugal compressor performance[J].Journal of Aerospace Power,2005,20(1):125-129.(in Chinese)
|
| [16] |
康剑雄.75kW燃气轮机离心叶轮改进设计及试验研究[D].上海:上海交通大学,2008. KANG Jianxiong.Improved design and experimental investigation for the centrifugal impeller of a 75kW gas turbine engine[D].Shanghai:Shanghai Jiaotong University,2008.(in Chinese)
|
| [17] |
石建成,邹学奇,温泉,等.离心压气机流动控制机匣新型处理方式研究[J].航空发动机,2010,36(3):1-4. SHI Jiancheng,ZOU Xueqi,WEN Quan,et al.Study on new type casing treatment method for centrifugal compressor[J].Aeroengine,2010,36(3):1-4.(in Chinese)
|
| [18] |
杨策,施新.径流式叶轮机械理论及设计[M].北京:国防工业出版社,2004.
|
| [19] |
Dunham J.Mechanical engineering science monograph[M].London:Institution of Mechanical Engineers,1965.
|
| [20] |
Schuler B J,Kerrebrock J L,Merchant A A,et al.Design,analysis,fabrication and test of an aspirated fan stage[R].ASME Paper GT2000-618,2000.
|
| [21] |
Kerrebrock J L.The prospects for aspirated compressors[R].AIAA 2000-2472,2000.
|
| [22] |
任铭林,向宏辉.有关轴流压气机效率问题的探讨[J].燃气涡轮试验与研究,2009,22(4):9-14. REN Minglin,XIANG Honghui.Exploration of efficiency in axial compressor[J].Gas Turbine Experiment and Research,2009,22(4):9-14.(in Chinese)
|