航空发动机进气旋流畸变研究综述

程邦勤; 王加乐; 冯路宁

doi:10.13224/j.cnki.jasp.2020.12.001

航空发动机进气旋流畸变研究综述

doi: 10.13224/j.cnki.jasp.2020.12.001

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出版历程
- 收稿日期: 2020-05-21
- 刊出日期: 2020-12-28

Review of aero-engine inlet swirl distortion research

Aeronautics Engineering College,Air Force Engineering University,Xi’an 710038,China

摘要

摘要: 为完善和发展航空发动机进气旋流畸变研究体系,回顾了进气旋流畸变的产生与来源,概述了国内外模拟旋流畸变的方法。归纳总结了不同类型、不同结构的旋流畸变对压气机以及航空发动机性能和稳定性的影响。综合分析了当前旋流畸变研究存在的问题和困难,对旋流畸变的发展趋势进行了讨论,提出以下建议:发展可变式旋流畸变发生器;探究旋流畸变对发动机整机性能的影响机理,为有效扩稳打下基础;要利用多种途径开展旋流进气条件下的压气机/发动机扩稳研究;建立统一的旋流畸变评价指标,并纳入到综合畸变指数系统中;探索小畸变进气道的设计方法。
- 旋流畸变 /
- 压气机 /
- 稳定性 /
- 进气道/发动机匹配 /
- 旋流畸变发生器
Abstract: In order to improve and develop the research system of inlet swirl distortion of aero-engine, the generation and source of inlet swirl distortion were reviewed, and the methods of simulating swirl distortion at home and abroad were summarized. The influences of swirl distortion of different types and structures on the performance and stability of compressors and aero-engines were summarized. The existing problems and difficulties in the current study of swirl distortion were analyzed synthetically, and the development trend of swirl distortion was discussed. Following suggestions are given: a variable swirl distortion generator should be developed. It is necessary to investigate the influence mechanism of swirl distortion on engine performance to lay a foundation for extending stable working range of engine effectively. Many ways should be used to extend stable working range of compressor/engine under the condition of inlet swirl. A unified evaluation index of swirl distortion should be established and incorporated into the integrated distortion index system. The design method of small distortion inlet should be explored.
- swirl distortion /
- compressor /
- stability /
- inlet/engine matching /
- ,swirl distortion generator

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参考文献(75)

[1]	姜健,于芳芳,赵海刚,等.进气道/发动机相容性评价体系的完善与发展［J］.科学技术与工程,2009,9(21):6474-6482. JIANG Jian,YU Fangfang,ZHAO Haigang et al.Perfection and development of engine/intake compatibility evaluate criterion［J］.Science Technology and Engineering,2009,9(21):6474-6482.(in Chinese)
[2]	侯敏杰,叶巍,彭生红.关于未来进气道/发动机相容性技术的探讨［J］.航空科学技术,2012(5):5-8. HOU Minjie,YE Wei,PENG Shenghong.Investigation on compatibility of future inlet/engine［J］.Aeronautical Science and Technology,2012(5):5-8.(in Chinese)
[3]	刘大响,叶培梁,胡骏,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.
[4]	ZHENG Ning,ZOU Zhengping,XU Liping.3-D unsteady numerical simulation of fan/compressor with inlet distortion［J］.Journal of Aerospace Power,2007,22(1):60-65.
[5]	YAO J,GORREL S E,WADIA A R.A time-accurate CFD analysis of inlet distortion induced swirl in multistage fans［R］.AIAA 2007-5059,2007.
[6]	Society of Automotive Engineers.Inlet total-pressure-distortion considerations for gas-turbine engines［R］.S16 Turbine Engine Inlet Distortion Committee,AIR1419,1983.
[7]	Society of Automotive Engineers.Gas turbine engine inlet flow distortion guidelines［R］.S16 Turbine Engine Inlet Distortion Committee ARP1420b,1978.
[8]	王如根,高坤华.航空发动机新技术［M］.北京:航空工业出版社,2003.
[9]	LUDWIG G.Tomahawk engine/inlet compatibility study for f107-wr-400/402 engines［R］.Williams International Report 5003-2025,2002.
[10]	Society of Automotive Engineers.A method for assessing inlet swirl distortion［R］.S16 Turbine Engine Inlet Flow Distortion Committee,AIR 5686,2010.
[11]	胡伟波,程邦勤,陈志敏,等.整体涡旋流畸变对压气机性能影响的研究［J］.推进技术,2015,36(9):1324-1330. HU Weibo,CHENG Bangqin,CHEN Zhimin,et al.Investi gation on effects of bulk swirl distortion on compressor performance［J］.Journal of Propulsion Technology,2015,36(9):1324-1330.(in Chinese)
[12]	胡伟波.旋流畸变对压气机性能和稳定性影响的数值模拟研究［D］.西安:空军工程大学,2015. HU Weibo.Numerical simulation of the effect of swirl distortion on compressor performance and stability［D］.Xi’an:Air Force Engineering University,2015.(in Chinese)
[13]	滕宏旭.逆风条件下地面涡气动特性及评价方式研究［D］.天津:中国民航大学,2019. TENG Hongxu.Study on aerodynamic characteristics and evaluation methods of ground vortex under headwind conditions［D］.Tianjin:Civil Aviation University of China,2019.(in Chinese)
[14]	MOTYCKA D.Ground vortex-limit to engine/reverser operation［R］.ASME Paper 75-GT-3,1975.
[15]	SIERVI F D,VIGUIER H C,GREITZER E M,et al.Mechanisms of inlet vortex formation［J］.Journal of Fluid Mechanics,1982,124:173-207.
[16]	SHIN H W,GREITZER E M,CHENG W K,et al.Circulation measurements and vortical structure in an inlet vortex flow field［J］.Journal of Fluid Mechanics,1986,162:463-487.
[17]	MOTYCKA D,WALTER W,MULLER G.Analytical and experimental study of inlet ground vortices［R］.AIAA 73-1313,1973.
[18]	杨国才.S弯进气道和发动机相容性［J］.推进技术,1995,16(6):26-29. YANG Guocai.Engine/S-shaped-inlet compatibility［J］.Journal of Propulsion Technology,1995,16(6):26-29.(in Chinese)
[19]	国防科学技术工业委员会.航空燃气涡轮发动机稳定性设计与评定指南:GJB/Z 224-2005［S］.北京:国防科学技术工业委员会,2005:4.
[20]	AULEHLA F.Intake swirl-a major disturbance parameter in engine/intake compatibility［C］∥Proceedings of 13th congress of International Council of the Aeronautical Sciences.Seattle:International Council of the Aeronautical Sciences,1982:1415-1424.
[21]	马高建,郭荣伟.无人机两侧式布局的S弯进气道设计与实验［J］.南京航空航天大学学报,2008,40(2):146-150. MA Gaojian,GUO Rongwei.Design and experiment of bilateral type s-shaped inlet of UAV［J］.Journal of Nanjing University of Aeronautics and Astronautics,2008,40(2):146-150.(in Chinese)
[22]	谢文忠,郭荣伟.腹下无隔道大偏距S弯进气道流场特性［J］.航空学报,2008,29(6):1453-1459. XIE Wenzhong,GUO Rongwei.Flow field of ventral diverterless high offset S-shaped inlet at transonic speeds［J］.Acta Aeronautica et Astronautica Sinica,2008,29(6):1453-1459.(in Chinese)
[23]	彭成一,马家驹,尹军飞.新机试飞中的进气道旋流测量.推进技术,1994,15(4):8-13. PENG Chengyi,MA Jiaju,YIN Junfei.Measurement of inlet swirls in flight［J］.Journal of Propulsion Technology,1994,15(4):8-13.(in Chinese)
[24]	GENSSLER H P,MEYER W,FOTTNER L.Development of intake swirl generators for turbo jet engine testing［R］.DTIC Document,ADP005473,1987.
[25]	姜健,屈霁云,史建邦.进气道旋流发生器的设计与数值模拟［J］.燃气涡轮试验与研究,2008,21(1):43-46. JIANG Jian,QU Jiyun,SHI Jianbang.Design and numerical simulation of intake swirl generator［J］.Gas Turbine Experiment and Research,2008,21(1):43-46.(in Chinese)
[26]	LOTTER K W,JORG J.The effect of intake flow disturbances on APU compressor blade high cycle fatigue in the Airbus A300［R］.AIAA CAS-82-4.6,1982.
[27]	张磊.新型旋流畸变网的设计及与跨声速压气机联合仿真研究［D］.西安:空军工程大学,2018. ZHANG Lei.Design of new type of swirl distortion screen and joint simulation with a transonic compressor［D］.Xi’an:Air Force Engineering University,2018.(in Chinese)
[28]	FLITCROFT J E,DUNHAM J,ABBOTT W A.Transmission of inlet distortion through a fan［R］.DTIC Document ADP005469,1987.
[29]	GOVARDHAN M,VISWANATH K.Investigations on an axial flow fan stage subjected to circumferential inlet flow distortion and swirl［J］.Journal of Thermal Science,1997,6(4):241-250.
[30]	邓小宝,姜健,屈霁云,等.进气道旋流模拟及测量的风动试验研究［J］.燃气涡轮试验与研究,2009,22(4):51-56. DENG Xiaobao,JIANG Jian,QU Jiyun,et al.Research on simulation and measurement of inlet swirl by wind tunnel test［J］.Gas Turbine Experiment and Research,2009,22(4):51-56.(in Chinese)
[31]	叶飞,张堃元,姜健,等.进气道旋流模拟及测量的实验研究［J］.推进技术,2009,30(3):297-281. YE Fei,ZHANG Kunyuan,JIANG Jian,et al.Experimental investigation on simulation and measurement for intake swirl［J］.Journal of Propulsion Technology,2009,30(3):297-281.(in Chinese)
[32]	屠宝锋,胡骏,尹超.叶片式旋流畸变发生器数值模拟研究［J］.推进技术,2015,36(12):1817-1824. TU Baofeng,HU Jun,YIN Chao.Numerical simulation for blade type swirl distortion generator［J］.Journal of Propulsion Technology,2015,36(12):1817-1824.(in Chinese)
[33]	周游天,李军,李成龙,等.进气旋流畸变对压气机性能的影响［J］.航空动力学报,2015,30(8):1936-1943. ZHOU Youtian,LI Jun,LI Chenglong,et al.Influence on compressor characteristic of inlet swirl flow distortion［J］.Journal of Aerospace Power,2015,30(8):1936-1943.(in Chinese)
[34]	宋国兴,李军,周游天,等.轴流压气机进气旋流畸变实验与仿真研究［J］.风机技术,2017,59(5):2-12. SONG Guoxing,LI Jun,ZHOU Youtian,et al.The experi-ment and simlation of inlet swirl distortion for axial compressor［J］.Compressor,Blower and Fan Technology,2017,59(5):2-12.(in Chinese)
[35]	PAZUR W,FOTTNER L.The influence of inlet swirl distortions on the performance of a jet propulsion two-stage axial compressor［R］.ASME Paper 90-GT-147,1990.
[36]	SCHMID N R,LEINHOS D C,FOTTNER L.Steady performance measurements of a turbofan engine with inlet distortions containing co-and counter rotating swirl from an intake diffuser for hypersonic flight［J］.Journal of Turbomachinery,2001,123(2):379-385.
[37]	SHEORAN Y,BOULDIN B,KRISHNAN P M.Advancements in the design of an adaptable swirl distortion generator for testing gas turbine engines［R］.ASME Paper GT2009-59146,2009.
[38]	BOULDIN B,SHEORAN Y,DAVIS M.Inlet flow angularity descriptors proposed for use with gas turbine engines［R］.SAE Paper 2002-01-2919,2002.
[39]	DAVIS M,BEALE D,SHEORAN Y.Integrated test and evaluation techniques as applied to an inlet swirl investigation using the F109 gas turbine engine［R］.ASME Paper GT2008-50074,2008.
[40]	纪振伟,程邦勤,张磊,等.腔室型旋流畸变发生器的设计与仿真研究［J］.推进技术,2018,39(4):776-784. JI Zhenwei,CHENG Bangqin,ZHANG Lei,et al.Design and numerical simulation for chamber swirl generator［J］.Journal of Propulsion Technology,2018,39(4):776-784.(in Chinese)
[41]	KEVIN M H,WALTER F,O’BRIEN W F.The streamvane method:a new way to generate swirl distortion for jet engine research［R］.AIAA-2013-3665,2013.
[42]	NELSON M,LOWE K T,O’BRIEN W F,et al.Stereoscopic PIV measurements of swirl distortion on a full-scale turbofan engine inlet［R］.AIAA-2014-0533,2014.
[43]	张磊,程邦勤,王加乐,等.新型旋流畸变网的设计与仿真研究［J］.推进技术,2018,39(9):2110-2119. ZHANG Lei,CHENG Bangqin,WANG Jiale,et al.Design and numerical simulation of a new swirl distortion screen［J］.Journal of Propulsion Technology,2018,39(9):2110-2119.(in Chinese)
[44]	叶飞.进气道出口旋流模拟技术［D］.南京:南京航空航天大学,2007. YE Fei.Simulated technology of intake swirl［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2007.(in Chinese)
[45]	王加乐,程邦勤,冯路宁,等.叶片式旋流发生器生成旋流角的影响因素研究［J］.空军工程大学学报(自然科学版),2020,21(3):31-37. WANG Jiale,CHENG Bangqin,FENG Luning,et al.Investigation on affecting factors of swirl angle generated by stream vane swirl distortion generator［J］.Journal of Air Force Engineering University (Natural Science Edition),2020,21(3):31-37.(in Chinese)
[46]	李成龙.进气旋流畸变对压气机性能影响的实验研究［D］.西安:空军工程大学,2013. LI Chenglong.Experiment study on influence of inlet swirl distortion on compressor performance［D］.Xi’an:Air Force Engineering University,2013.(in Chinese)
[47]	HAH C,RABE D C,SULLIVAN T J.Effects of inlet distortion on the flow field in a transonic compressor rotor［J］.Journal of Turbomachinery,1998,120(3):1230-1238.
[48]	GORRELL S E,YAO J,WADIA A R.High fidelity UNRANS analysis of swirl generation and fan response to inlet distortion［R］.AIAA 2008-4985,2008.
[49]	HAH C.Large eddy simulation of transonic flow field in NASA rotor 37［R］.AIAA 2009-1061,2009.
[50]	DAVIS M,BEALE D,BOYER K.An example for integrated gas turbine engine testing and analysis using modeling and simulation［R］.ITEA ADA497076,2006.
[51]	DAVIS M,HALE A.A parametric study on the effects of inlet swirl on compression system performance and operability using numerical simulations［R］.ASME Paper GT2007-27033,2007.
[52]	NICHOLAS F,DAVIS M.Investigation of the effect of inlet swirl on compressor performance and operability using a modified parallel compressor model［R］.ASME Paper GT2011-45553,2011.
[53]	COUSIN W,DAVIS M.Evaluating complex inlet distortion with a parallel compressor model:Part 1 concepts,theory,extensions,and limitations［R］.ASME Paper GT2011-45067,2011.
[54]	SHEORAN Y,BOULDIN B,KRISHNAN P.Compressor performance and operability in swirl distortion［J］.Journal of Turbomachinery,2012,134(4):2453-2464.
[55]	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):2307-2313. 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):2307-2313.(in Chinese)
[56]	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)
[57]	屠宝锋,胡骏.旋流畸变影响低速轴流压气机数值模拟研究［J］.推进技术,2016,37(9):1650-1656. TU Baofeng,HU Jun.Numerical simulation of low speed axial compressor with swirl distortion［J］.Journal of Propulsion Technology,2016,37(9):1650-1656.(in Chinese)
[58]	屠宝锋,胡骏,张凯.对涡旋流影响压气机转子性能和稳定性的研究［J］.推进技术,2016,37(4):641-645. TU Baofeng,HU Jun,ZHANG Kai.Effects of twin swirl on per formance and stability of compressor rotor［J］.Journal of Propulsion Technology,2016,37(4):641-645.(in Chinese)
[59]	纪振伟,程邦勤,张磊,等.整体涡旋流畸变下转子的流场分析［C］∥第3届中国航空科学技术大会论文集.北京:中国航空学会,2017:297-302.
[60]	程邦勤,纪振伟,胡伟波,等.对涡旋流畸变对单级跨声速压气机性能影响的数值研究［J］.推进技术,2017,38(8):1777-1786. CHENG Bangqin,JI Zhenwei,HU Weibo,et al.Effects of paired swirl distortion on single stage transonic compressor performance using numerical simulation［J］.Journal of Propulsion Technology,2017,38(8):1777-1786.(in Chinese)
[61]	张磊,程邦勤,纪振伟.整体涡旋流畸变下的压气机失速机理分析［J］.空军工程大学学报(自然科学版),2018,19(1):20-25. ZHANG Lei,CHENG Bangqin,JI Zhenwei.An instability mechanism analysis with compressor under condition of bulk swirl distortion［J］.Journal of Air Force Engineering University (Natural Science Edition),2018,19(1):20-25.(in Chinese)
[62]	DAVID B,KEVIN C,PETER K.Development of improved method for simulating aircraft inlet distortion in turbine engine ground tests［R］.AIAA-2002-3045,2002.
[63]	GOUTINES M,JOUBERT H.Compatibility entred air-moteur:impact des mthodes thoriques et exprimentales［R］.AGARD N87-24464,1975.
[64]	GARNIER E,LEPLAT M,MONNIER J C.Flow control by pulsed jet in a highly bended S-duct［R］.AIAA-2012-3250,2012.
[65]	WENDT B J,REICHERT B A.Vortex ingestion in a diffusing S-duct inlet［J］.Journal of Aircraft,1996,33(1):149-154.
[66]	ANNBTAWI A J,BLACKWELDER R F,LISSAMAN P B S.An experimental study of vortex generators in boundary layer ingesting diffusers with a centerline offset［R］.AIAA 99-211035,1999.
[67]	田晓平,潘鹏飞,田琳.某Ｓ型进气道流动分离数值模拟［J］.工程与试验,2015,55(3):15-17. TIAN Xiaoping,PAN Pengfei,TIAN Lin.Numerical simulation of flow separation of a S-duct inlet［J］.Engineering and Test,2015,55(3):15-17.(in Chinese)
[68]	张晓飞,姜健,符小刚.Ｓ弯进气道旋流畸变数值模拟及特性分析［J］.燃气涡轮试验与研究,2012,25(3):21-26. ZHANG Xiaofei,JIANG Jian,FU Xiaogang.Numerical simulation and characteristic analysis of swirl distortion in S-duct inlet［J］.Gas Turbine Experiment and Research,2012,25(3):21-26.(in Chinese)
[69]	徐诸霖,达兴亚,范召林.基于五孔探针的大Ｓ弯进气道旋流畸变评估［J］.航空学报,2017,38(12):1-7. XU Zhulin,DA Xingya,FAN Zhaolin.Assessment of swirl distortion of serpentine inlet based on five-hole probe［J］.Acta Aeronautica et Astronautica Sinica,2017,38(12):1-7.(in Chinese)
[70]	刘雷,陈浮,宋彦萍,等.大量附面层吸入Ｓ弯进气道内吹气控制［J］.航空动力学报,2015,30(10):2499-2506. LIU Lei,CHEN Fu,SONG Yanping,et al.Blowing control in S-shaped inlet with significant boundary layer ingestion［J］.Journal of Aerospace Power,2015,30(10):2499-2506.(in Chinese)
[71]	刘雷,陈浮,宋彦萍,等.Ｓ弯进气道内附面层抽吸控制对风扇级性能的影响［J］.航空动力学报,2016,31(7):1677-1684. LIU Lei,CHEN Fu,SONG Yanping,et al.Suction control of boundary layer in S-shaped air intake and its influence on fan-stage performance［J］.Journal of Aerospace Power,2016,31(7):1677-1684.(in Chinese)
[72]	刘雷,宋彦萍,陈焕龙,等.半埋入式S弯进气道设计及其优化［J］.推进技术,2014,35(10):1304-1309. LIU Lei,SONG Yanping,CHEN Huanlong,et al.Design and optimization of half flush-mounted S-shaped inlet［J］.Journal of Propulsion Technology,2014,35(10):1304-1309.(in Chinese)
[73]	刘雷,宋彦萍,陈焕龙,等.S弯进气道优化对其内流场及性能影响研究［J］.工程热物理学报,2015,36(1):50-54. LIU Lei,SONG Yanping,CHEN Huanlong,et al.Investigation on effect of S-shaped inlet optimization to internal flow characteristic and aerodynamic performance［J］.Journal of Engineering Thermophysics,2015,36(1):50-54.(in Chinese)
[74]	田晓平,潘鹏飞,田琳.利用涡流发生器抑制S弯进气道旋流畸变的数值模拟研究［J］.航空科学技术,2015,26(4):16-23. TIAN Xiaoping,PAN Pengfei,TIAN Lin.Research and simulation of flow control in S-duct inlet with vortex generators［J］.Aeronautical Science and Technology,2015,26(4):16-23.(in Chinese)
[75]	田晓平,潘鹏飞,李密.S形进气道流动控制数值模拟研究［J］.航空科学技术,2017,28(5):42-46.