端壁附面层抽吸对对转压气机性能的影响 *

推进技术 ›› 2014, Vol. 35 ›› Issue (10): 1356-1362.

端壁附面层抽吸对对转压气机性能的影响 *

巫骁雄,刘　波,史　磊

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;西北工业大学动力与能源学院，陕西西安 710072

发布日期:2021-08-15
作者简介:巫骁雄(1990—)，男，硕士生，研究领域为叶轮机械气动热力学。
基金资助:
国家自然科学基金重点项目(51236006)。

Effects of Endwall Boundary Layer Suction on a

School of Power and Energy，Northwestern Polytechnical University，Xi’an 710072，China;School of Power and Energy，Northwestern Polytechnical University，Xi’an 710072，China;School of Power and Energy，Northwestern Polytechnical University，Xi’an 710072，China

Published:2021-08-15

摘要/Abstract

摘要： 以双级对转压气机为研究对象，通过在两排转子机匣处开设抽吸孔，采用数值方法研究了不同抽吸流量下端壁附面层抽吸对压气机性能的影响，为吸附式压气机优化设计提供参考。计算结果表明:在级环境下端壁附面层抽吸可以提升压气机失速裕度，但抽吸流量过大会对效率造成一定损失，当抽吸1.6%流量时失速裕度提升了3.8%，压气机性能达到最佳；失速主要由间隙泄漏涡引起并首先在第二排转子叶尖发生，抽吸削弱了泄漏涡的强度推迟失速发生；端壁附面层抽吸增大了叶尖流通能力，使转子叶尖效率和压比得到提升，并有效改善了出口导叶流场。

关键词: 对转压气机；端壁附面层抽吸；数值计算；抽吸流量；级环境

Abstract: To provide a reference for design and optimization of the aspirate compressor，the performance and detailed flow structure of a counter-rotating compressor were numerically investigated under different suction flow with endwall boundary layer suction through the two rows of suction holes in the casing over the rotor tip. The results show that in multistage environment endwall boundary layer suction can increase compressor stall margin，but the adiabatic efficiency would be adversely affected by excess suction flow. The compressor performs best under 1.6% suction rate while the stall margin increased by 3.8%. Stall is mainly induced by the leakage vortex，and occurs in the tip area of the second row of rotor at first. The suction can weaken the strength of leakage vortex and delay the stall. Since the end wall boundary layer suction increases the flow capacity，the pressure ratio and adiabatic efficiency are increased，meanwhile the flow field in outlet guide vane tip has also been improved.

Key words: Counter-rotating compressor；Endwall boundary layer suction；Numerical computation；Suction flow；Multistage environment

巫骁雄,刘　波,史　磊. 端壁附面层抽吸对对转压气机性能的影响 *[J]. 推进技术, 2014, 35(10): 1356-1362.

WU Xiao-xiong,LIU Bo,SHI Lei. Effects of Endwall Boundary Layer Suction on a[J]. Journal of Propulsion Technology, 2014, 35(10): 1356-1362.

参考文献

[1] 蔡睿贤. 有关对转涡轮基本设计与应用的进一步思考 [J]. 航空动力学报, 2001, 16(3): 193-198.
[2] 王掩刚, 贾瑞琦, 牛楠, 等. 双级对转压气机多工况数值分析研究 [J]. 西北工业大学学报, 2008, 26(5): 535-539.
[3] 刘波, 杨艳, 王掩刚, 等. 设计压比和转速变化对对转压气机性能的影响研究 [J]. 西北工业大学学报, 2007, 25(4): 576-580.
[4] 高丽敏, 李晓军, 冯旭栋, 等. 对转压气机转速比变化对稳定边界的影响[J]. 推进技术, 2012, 33(6): 881-887.(GAO Li-min, LI Xiao-jun, FENG Xu-dong, et al. Effect of Rotational Speed Ratio on Stability Boundary of Contra-Rotating Compressor [J]. Journal of Propulsion Technology, 2012, 33(6): 881-887.)
[5] Antoine G, Fran?ois B, Stéphane B, et al. Experimental and Numerical Study of a Subsonic Aspirated Cascade [R]. ASME 2012-GT-69011.
[6] Hubrich K, Bolcs A, Ott P. Boundary Layer Suction Via a Slot in a Transonic Compressor-Numerical Parameter Study and First Experiments [J]. ASME 2004-GT-53758.
[7] Kerrebrock J L, Reijnen D P, Ziminsky W S, et al. Aspirated Compressors [R].ASME 97-GT-525.
[8] Kerrebrock J L, Drela M, Merchant A A, et al. Family of Designs for Aspirated Compressors [R]. ASME 98-GT-196.
[9] Merchant A A. Design and Analysis of Axial Aspirated Compressor Stages [D].USA: Massachusetts Institute of Technology, 1999.
[10] Kirchner J. Aerodynamic Design of an Aspirated Counter-Rotating Compressor [D]. USA: Massachusetts Institute of Technology, 2002.
[11] Kerrebrock J L, Epstein A H, Merchant A A, et al. Design and Test of an Aspirated Counter-Rotating fan [J]. Journal of Turbomachinery, 2008, 130(2).
[12] 刘波, 曹志远, 魏巍, 等. 级环境下附面层抽吸对对转压气机性能的影响[J]. 航空动力学报, 2013, 28(4).
[13] Schuler B J, Kerrebrock J L, Merchant A. Experimental Investigation of an Aspirated Fan Stage[R]. ASME 2002-GT-30370.
[14] Merchant A, Kerrebrock J L, Adamczyk J J, et al. Experimental Investigation of a High Pressure Ratio Aspirated Fan Stage [J]. Transactions of the ASME Journal of Turbomachinery, 2005, 127(1): 43-51.
[15] GLIMMER V, Goller M, Swoboda M. Numerical Investigation of End Wall Boundary Layer Suction on Highly loaded Axial Compressor Blade Rows [J]. Journal of Turbomachinery, 2008, 130(1).
[16] Camp T R, Day I J. A Study of Spike and Modal Stall Phenomena in a Low-Speed Axial Compressor[J]. Journal of Turbomachinery, 1998, 120(3).(编辑:梅瑛)　　　　　　　　　　　　　*　收稿日期:2013-10-17；修订日期:2013-11-26。基金项目:国家自然科学基金重点项目(51236006)。作者简介:巫骁雄(1990—),男,硕士生,研究领域为叶轮机械气动热力学。E-mail:xxwu1990@126.com