Volume 37 Issue 1
Jan.  2022
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2022  >  37(1): 191-203
GUO Yanchao, GAO Limin, YANG Guanhua, WANG Lei. Study on the mechanism of stability improvement of the self-recirculating casing treatment in a counter-rotating compressor[J]. Journal of Aerospace Power, 2022, 37(1): 191-203. doi: 10.13224/j.cnki.jasp.20210009
Citation: GUO Yanchao, GAO Limin, YANG Guanhua, WANG Lei. Study on the mechanism of stability improvement of the self-recirculating casing treatment in a counter-rotating compressor[J]. Journal of Aerospace Power, 2022, 37(1): 191-203. doi: 10.13224/j.cnki.jasp.20210009
shu

Study on the mechanism of stability improvement of the self-recirculating casing treatment in a counter-rotating compressor

doi: 10.13224/j.cnki.jasp.20210009
  • 1.

    School of Power and Energy，Northwestern Polytechnical University，Xi'an 710129，China

  • 2.

    National Key Laboratory of Aerodynamic Design and Research，Northwestern Polytechnical University，Xi'an 710129，China

  • Received Date: 2021-01-09
  • Publish Date: 2022-01-28
    Abstract
  • In order to broaden the application range of self-recirculating casing treatment（SRCT），a counter-rotating compressor was used as the research object.The stability enhancement mechanism of SRCT and the effect of axial injection position on its stability expansion ability were studied by numerical method.The overall characteristics of the counter-rotating compressor and the change of rotor tip flow field with/without self-recirculating casing treatment were analyzed in detail.The results showed that considerable stall margin improvement can be obtained by configuring a self-recirculating casing on the rotor that stalled first，but the axial injection position had an important effect on the stability improvement effect and the aerodynamic performance of the counter-rotating compressor.The axial injection position should not be too close to the leading edge of the blade；when the injection position was 40% of the axial chord length from the leading edge of the blade，the improvement of stall margin was 7.73% and the peak efficiency loss was minimum.Self-recirculating casing treatment can delay stall by reducing blade tip load，weakening the strength of the tip secondary leakage flow and restraining the mixing of the tip leakage flow and main flow.The first stall stage of counter-rotating compressor can be changed by self-recirculating casing treatment，without change of the stall initiation type.

     

    • FullText(HTML)
  • loading
    • References(39)
  • [1]
    YANG X H，SHAN P.Design of two counter-rotating fan types and CFD investigation of their aerodynamic characteristics[R].ASME Paper GT2011-45426,2011.
    [2]
    WANG J，RAVELET F，BAKIR F.Experimental comparison between a counter-rotating axial-flow fan and a conventional rotor-stator stage[C]∥Proceedings of the 10th European Turbomachinery Conference.Lappeenranta，Finland:Euroturbo European Turbomachinery Society,2013:00795006.1-00795006.10.
    [3]
    MISTRY C，PRADEEP A.Effect of variation in axial spacing and rotor speed combinations on the performance of a high aspect ratio counter-rotating axial fan stage[J].Proceedings of the Institution of Mechanical Engineers:Part A Journal of Power and Energy，2013，227（2）:138-146.
    [4]
    GAO L M，LI X J，XIE J，et al.The effect of speed ratio on the first rotating stall stage in counter-rotating compressor[R].ASME Paper GT2012-68802，2012.
    [5]
    高丽敏，李瑞宇，李晓军，等.轴向间隙对对转压气机失速性能的影响[J].推进技术，2015，36（12）:1802-1808.
    [6]
    高丽敏，苗芳，李晓军，等.对转压气机转速比对最先失速级的影响[J].应用力学学报，2013，30（6）:845-848,951.
    [7]
    PUNDHIR D S，SHARMA P B，CHAUDHARY K K.Effect of casing treatment on aerodynamic performance of a counterrotating axial compressor stage[J].Proceedings of the Institution of Mechanical Engineers:Part A Journal of Power and Energy，1990，204（1）:47-55.
    [8]
    PUNDHIR D S.A study of some factors affecting the effectiveness of casing treatment in counter-rotating axial compressor stage[J].Indian Journal of Engineering and Materials Sciences，1994，1（4）:199-207.
    [9]
    MAO X，LIU B，TANG T，et al.The impact of ca-sing groove location on the flow instability in a counter-rotating axial flow compressor[J].Aerospace Science and Technology，2018，76:250-259.
    [10]
    MAO X，LIU B，ZHAO H.Numerical analysis of the circumferential grooves casing treatment in a counter-rotating axial flow compressor[J].Applied Thermal Engineering，2018，130:29-39.
    [11]
    HEINRICH M，KHALEGHI H，FRIEBE C.Numerical investigation of circumferential groove casing treatment on a low speed counter-rotating fan[R].ASME Paper GT2019-91705，2019.
    [12]
    CROOK A J，GREITZER E M，TAN C S，et al.Numerical simulation of compressor endwall and casing treatment flow phenomena[J].Journal of Turbomachinery，1993，115（3）:501-512.
    [13]
    HOUGHTON T，DAY I.Enhancing the stability of subsonic compressors using casing grooves[J].Journal of Turbomachinery，2010，133（2）:021007.1-021007.11.
    [14]
    LIM B J，PARK T C，KWON S.Stall inception and warning in a single-stage transonic axial compressor with axial skewed slot casing treatment[J].Journal of Mechanical Science and Technology，2014，28（9）:3569-3581.
    [15]
    ALONE D B，KUMAR S S，THIMMAIAH S，et al.Experimental investigation on the effect of porosity of bend skewed casing treatment on a single stage transonic axial flow compressor[R].ASME Paper GT2014-26102，2014.
    [16]
    DAY I J.Stall，surge，and 75 years of research[J].Journal of Turbomachinery，2016，138（1）:011001.1-011001.16.
    [17]
    GREITZER E M，NIKKANEN J P，HADDAD D E，et al.A fundamental criterion for the application of rotor casing treatment[J].Journal of Fluids Engineering，1979，101（2）:237-243.
    [18]
    GUINET C，BETTRICH V，GüMMER V.Parametric study of the bleed position in a tip blowing casing treatment[R].AIAA 2014-3441，2014.
    [19]
    HATHAWAY M D.Passive endwall treatments for enhancing stability[R].NASA/TM-2007-214409，2007.
    [20]
    STREIT J A，HEINICHEN F，KAU H P.Axial-slot casing treatments improve the efficiency of axial flow compressors:aerodynamic effects of a rotor redesign[R].ASME Paper GT2013-94975，2013.
    [21]
    SUDER K L，HATHAWAY M D.Compressor stability enhancement using discrete tip injection[J].Journal of Turbomachinery，2001，123（1）:14-23.
    [22]
    KHALEGHI H.Stall inception and control in a transonic fan:Part B stall control by discrete endwall injection[J].Aerospace Science and Technology，2015，41:151-157.
    [23]
    LI J.Self-adaptive stability-enhancing technology with tip air injection in an axial flow compressor[J].Journal of Turbomachinery，2017，139（1）:011008.1-011008.9.
    [24]
    KHALEGHI H，BOROOMAND M，TEIXEIRA J A，et al.A numerical study of the effects of injection velocity on stability improvement in high-speed compressors[J].Proceedings of the Institution of Mechanical Engineers:Part A Journal of Power and Energy，2008，222（2）:189-198.
    [25]
    KHALEGHI H，TEIXEIRA J A，TOUSI A M，et al.Parametric study of injection angle effects on stability enhancement of transonic axial compressors[J].Journal of Propulsion and Power，2008，24（5）:1100-1107.
    [26]
    KHALEGHI H.Parametric study of injector radial penetration on stalling characteristics of a transonic fan[J].Aerospace Science and Technology，2017，66:112-118.
    [27]
    HATHAWAY M D.Self-recirculating casing treatment concept for enhanced compressor performance[R].ASME Paper GT2002-30368，2002.
    [28]
    WANG W，CHU W，ZHANG H.Mechanism study of performance enhancement in a subsonic axial flow compressor with recirculating casing treatment[J].Proceedings of the Institution of Mechanical Engineers:Part G Journal of Aerospace Engineering，2018，232（4）:680-693.
    [29]
    LI J，DU J，NAN X，et al.Coupling stability-enhancing mechanism with compact self-recirculating injection in an axial flow compressor[J].Proceedings of the Institution of Mechanical Engineers:Part A Journal of Power and Energy，2016，230（7）:696-708.
    [30]
    LI J，DU J，LI Z，et al.Stability enhancement with self-recirculating injection in axial flow compressor[J].Journal of Turbomachinery，2018，140（7）:071001,1-071001.13.
    [31]
    WEICHERT S A，HALL C.Tip clearance flows in axial compressors:stall inception and stability enhancement[D].London:University of Cambridge，2011.
    [32]
    WEICHERT S，DAY I，FREEMAN C.Self-regulating casing treatment for axial compressor stability enhancement[R].ASME Paper GT2011-46042，2011.
    [33]
    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）:393-401.
    [34]
    VO H D，TAN C S，GREITZER E M.Criteria for spike initiated rotating stall[J].Journal of Turbomachinery，2008，130（1）:011023.1-011023.9.
    [35]
    ZHONG Y，CHU W，ZHANG H.Numerical investigation on the effect of bleed port with self-recirculating casing treatment on the stability of a 1.5-stage transonic compressor[R].ASME Paper GT2019-90543，2019.
    [36]
    MOORE R D，REID L.Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78，respectively，and with design pressure ratio of 1.82[R].NASA TP-1338，1978.
    [37]
    PULLAN G，YOUNG A M，DAY I J， et al.Origins and structure of spike-type rotating stall[J].Journal of Turbomachinery，2015，137（5）:051007.1-051007.11.
    [38]
    杜娟，王偲臣，李继超，等.轴流压气机叶顶泄漏流与突尖先兆失稳机理的研究进展[J].推进技术，2017，38（10）:2208-2217.
    [39]
    KHALID S A，KHALSA A S，WAITZ I A，et al.Endwall blockage in axial compressors[J].Journal of Turbomachinery，1999，121（3）:499-509.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF(2721.0KB)
    XML

    Article Metrics

    Article views (562) PDF downloads(113) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return