Volume 32 Issue 5
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Study on bleed air anti-icing system of aircraft[J]. Journal of Aerospace Power, 2017, 32(5): 1025-1034. doi: 10.13224/j.cnki.jasp.2017.05.001
Citation: Study on bleed air anti-icing system of aircraft[J]. Journal of Aerospace Power, 2017, 32(5): 1025-1034. doi: 10.13224/j.cnki.jasp.2017.05.001
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Study on bleed air anti-icing system of aircraft

doi: 10.13224/j.cnki.jasp.2017.05.001
  • Received Date: 2016-12-08
  • Publish Date: 2017-05-28
    Abstract
  • The basic structure and application background of the bleed air anti-icing system of aircraft was introduced, and its development history and present development situation at home and abroad were reviewed. The main research contents were analyzed from four key points, including the calculation of anti-icing surface droplet impingement property, the modeling of external icing/runback water of skin, the study of the internal structure parameters of bleed air anti-ice system, and multiphase coupling simulation of anti-icing system. Finally, the development trend of bleed air anti-icing system was shown via the analysis of the accurate prediction of three-dimensional accreting process of runback ice, optimization method of internal structure parameters of bleed air anti-icing system, the determination of the anti-icing systems safety boundary and margin, the parameters scaled model icing-wind tunnel experiment of anti-icing system.Key words: bleed air anti-icing; icing/runback

     

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    • References(61)
  • [1]
    Belcastro C M,Foster J V.Aircraft loss-of-control accident analysis［R］.AIAA-2010-8004，2010.
    [2]
    Bragg M B,Perkins W R,Sarter N B,et al.An interdisciplinary approach to inflight aircraft icing safety［R］.AIAA 98-0095,1998.
    [3]
    Petty K R,Floyd C D J.A statistical review of aviation airframe icing accidents in the U.S.［R］.Washington：11th Conference on Aviation,Range,and Aerospace,2004.
    [4]
    Jones S M,Reveley M S,Evans J K，et al.Subsonic aircraft safety icing study［R］.NASA/TM-2008-215107，2008.
    [5]
    Meier O，Scholz D.A handbook method for the estimation of power requirements for electrical de-icing systems［EB/OL］.［2016-12-01］.http:∥MOZART.Profschol I.de.
    [6]
    Yeoman K E.Efficiency of a bleed air powered inlet icing［R］.AIAA 94-0717，1994.
    [7]
    Papadakis M,Wong S H,Yeong H W，et al.Experimental investigation of a bleed air ice protection system［R］.SAE Technical Paper 2007-01-3313,2007.
    [8]
    裘燮纲,韩凤华.飞机防冰系统［M］.北京:航空专业教材编审组，1985:93-97.
    [9]
    韩凤华，张朝民，王跃欣.飞机机翼表面水滴撞击特性计算［J］.北京航空航天大学学报,1995,21(3):16-21. HAN Fenghua,ZHANG Chaomin,WANG Yuexin.Calculation of water-droplet impingement on an airfoil［J］.Journal of Beijing University of Aeronautics and Astronautics,1995,21(3):16-21.（in Chinese）
    [10]
    Bourgault Y,Habashi W G,Dompierre J,et al.An Eulerian approach to supercooled droplets impingement calculations［R］.AIAA 97-0176，1997.
    [11]
    杨胜华，林贵平，申晓斌.三维复杂表面水滴撞击特性计算［J］.航空动力学报，2010,25(2):284-290. YANG Shenghua,LIN Guiping,SHEN Xiaobin.Water droplet impingement prediction for three-dimensional complex surfaces［J］.Journal of Aerospace Power,2010,25(2):284-290.(in Chinese)
    [12]
    Hedde T,Guffond D.ONERA three-dimensional icing model［J］.AIAA Journal,1995,33(6):1038-1045.
    [13]
    Ruff G A,Berkowittz B M.Users manual for the NASA Lewis ice accretion prediction code (LEWICE)［R］.NASA-CR-185129,1990.
    [14]
    Ming G,Brandi V.Ice accretion prediction on multi-element airfoils［J］.Journal of Aircraft,1998,35(2):240-246.
    [15]
    Morency F,Brahimi M T,Tezok F,et al.Bleed air anti-icing system modelization in the ice prediction code:CANICE［R］.AIAA 98-0192，1998.
    [16]
    Hansman R J,Turnock S R.Investigation of surface water behavior during glaze ice accretion［J］.Journal of Aircraft,1989,26(2):140-147.
    [17]
    Al-Khalil K M.Numerical simulation of an aircraft anti-icing system incorporating a rivulet model for the runback water［D］.Toledo,US：University of Toledo,1991.
    [18]
    Hansman R J,Yamaguchi K,Berkowitz B，et al.Modeling of surface roughness effects on glaze ice accretion［J］.Journal of Thermophysics and Heat Transfer,1989,5(1):54-60.
    [19]
    Al-Khalil K M,Keith T G,De Witt K J.New conceptin runback water modeling for anti-iced aircraft surfaces［J］.Journal of Aircraft,1993,30(1):41-49.
    [20]
    Bourgault Y,Beaugendre H,Habashi W G.Development of a shallow-water icing model in FENSAP-ICE［J］.Journal of Aircraft,2000，37(4):640-646.
    [21]
    Fortin G,Ilinca A,Laforte J L，et al.New roughness computation method and geometric accretion model for airfoil icing［J］.Journal of Aircraft,2004,41(1):119-127.
    [22]
    Myers T G，Hammond D W.Ice and water film growth from incoming supercooled droplets［J］.International Journal of Heat and Mass Transfer,1999,42（12）:2233-2242.
    [23]
    Myers T G.Extension to the messinger model for aircraft icing［J］.AIAA Journal,2001,39(2):211-218.
    [24]
    Weigand B,Spring S.Multiple jet impingement：a review［J］.Heat Transfer Research，2011,42(2):101-142.
    [25]
    Saeed F.Numerical simulation of surface heat transfer from an array of hot-air jets［J］.Journal of Aircraft,2008,45(2):700-714.
    [26]
    彭珑，卜雪琴，林贵平，等．热气防冰腔结构参数对其热性能影响研究［J］.空气动力学学报，2014，32(6) :848- 853．PENG Long， BU Xueqin， LING Guiping,et al．Influence of the structural parameters on thermal performance of the bleed air anti-icing system［J］.Acta Aerodynamica Sinica，2014，32(6):848- 853.(in Chinese)
    [27]
    Sharif M A R,Ramirez N M.Surface roughness effects on the heat transfer due to turbulent round jet impingement on convex hemispherical surfaces［J］.Applied Thermal Engineering,2013,51（1/2）:1026-1037.
    [28]
    Wan C,Rao Y,Chen P.Numerical predictions of jet impingement heat transfer on square pin-fin roughened plates［J］.Applied Thermal Engineering,2015,80:301-309.
    [29]
    卜雪琴,陈雨晨,林贵平,等.热气防冰腔中短小销钉强化传热数值模拟［J］.北京航空航天大学学报，2013，39 (8) :1053- 1057. BU Xueqin，CHEN Yuchen，LIN Guiping,et al.Investigation of heat transfer enhancement of short pin fins in bleed air anti-icing system［J］.Journal of Beijing University of Aeronautics and Astronautics,2013,39(8):1053-1057.(in Chinese)
    [30]
    Papadakis M,Wong S H,Yeong H W，et al.Icing tunnel experiments with a bleed air anti-icing system［R］.AIAA-2008-444，2008.
    [31]
    卜雪琴,彭珑,林贵平,等.热气防冰系统内表面弦向传热性能衰减规律［J］.北京航空航天大学学报,2016,42(1):72-78. BU Xueqin,PENG Long,LIN Guiping,et al.Chordwise attenuation of heat transfer performance on inner surface of hot-air anti-icing system［J］.Journal of Beijing University of Aeronautics and Astronautics,2016,42(1):72-78.(in Chinese)
    [32]
    Wright W B.An evaluation of jet impingement heat transfer correlations for piccolo tube application［R］.AIAA-2004-0062，2004.
    [33]
    Saeed F,Morency F,Paraschivoiu I.Numerical simulation of a hot-air anti-icing system［R］.AIAA-2000-0630，2000.
    [34]
    Saeed F,Paraschivoiu I.Optimization of a hot-air anti-icing system［R］.AIAA-2003-0733，2003.
    [35]
    Pellissier M P C,Habashi W G,Pueyo A.Optimization via FENSAP-ICE of aircraft hot-air anti-icing systems［J］.Journal of Aircraft,2011,48(1):265-276.
    [36]
    Mattos B S D,Oliveira G L.Three-dimensional thermal coupled analysis of a wing slice slat with a piccolo tube［R］.AIAA-2000-3921，2000.
    [37]
    Domingos R H,Papadakis M,Zamora A O.Computational methodology for bleed air ice protection system parametric analysis［R］.AIAA-2010-7834，2010.
    [38]
    Croce G,Habashi W G,Guevremont G,et al.3D thermal analysis of an anti-icing device using FENSAP-ICE［R］.AIAA 98-0193,1998.
    [39]
    Liu H H T,Hua J.Three-dimensional integrated thermodynamic simulation for wing anti-icing system［J］.Journal of Aircraft,2004,41(6):1291-1297.
    [40]
    Hua J,Kong F,Liu H H T.Unsteady thermodynamic computational fluid dynamics simulations of aircraft wing anti-icing operation［J］.Journal of Aircraft,2007,44(4):1113-1117.
    [41]
    Miller D,Bond T,Sheldon D，et al.Validation of NASA thermal ice protection computer codes： PartⅠprogram overview［R］.AIAA 97-0049,1997.
    [42]
    Wright W B,Al-Khalil K M,Miller D.Validation of NASA thermal ice protection computer codes：PartⅡ Lewice/thermal［R］.Reno,US：Aerospace Sciences Meeting and Exhibit,1997.
    [43]
    A1-Khalil K M,Horvath C,Miller D R，et al.Validation of NASA thermal computer codes:Part Ⅲ the validation of ANTICE［R］.AIAA 97-0051,1997.
    [44]
    Morency F,Brahimi M T,Tezok F,et al.Anti-icing system simulation using CANICE［J］.Journal of Aircraft,1999,36(6):999-1006.
    [45]
    常士楠，袁美名，霍西恒，等.某型飞机机翼防冰系统计算分析［J］.航空动力学报,2008,23(6):1141-1145. CHANG Shinan,YUAN Meiming,HUO Xiheng,et al.Investigation of bleed air anti-icing system for an aircraft wing［J］.Journal of Aerospace Power,2008,23(6):1141-1145.(in Chinese)
    [46]
    Rodríguez A O Z.Numerical investigation of a wing bleed air ice protection system［D］.Wichita，US：Wichita State University,2009.
    [47]
    Fregeau M,Saeed F,Paraschivo I.Surface heat transfer study for ice accretion and anti-icing prediction in three dimension［R］.AIAA-2004-0063，2004.
    [48]
    Croce G,Beaugendre H,Habashi W G.CHT3D:FENSAP-ICE conjugate heat transfer computations with droplet impingement and runback effects［R］.AIAA-2002-0386,2002.
    [49]
    Lee J,Rigby D,Wright W，et al.Analysis of thermal ice protection system (tips) with piccolo tube using state-of-the-art software［R］.AIAA-2006-1011,2006.
    [50]
    卜雪琴，林贵平，郁嘉.三维内外热耦合计算热气防冰系统表面温度［J］.航空动力学报,2009,24(11):2495-2500. BU Xueqin,LIN Guiping,YU Jia.Three-dimensional conjugate heat transfer simulation for the surface temperature of wing hot-air anti-icing system［J］.Journal of Aerospace Power,2009,24(11):2495-2500.(in Chinese)
    [51]
    卜雪琴，马文涛，林贵平.二维机翼防冰表面溢流水膜破裂数值模拟［J］.航空动力学报,2015,30(2):368-375. BU Xueqin,MA Wentao,LIN Guiping.Numerical simulation of runback film breakup on two-dimensional anti-icing airfoil surface［J］.Journal of Aerospace Power,2015,30(2):368-375.(in Chinese)
    [52]
    霍西恒，王大伟，李革萍，等.某型飞机机翼防冰系统性能验证研究［J］.民用飞机设计与研究,2013（4）:13-16. HUO Xiheng,WANG Dawei,LI Geping,et al.Study on the performance verification of a certain type of aircraft wing anti icing system［J］.Civil Aircraft Design and Research,2013（4）:13-16.(in Chinese)
    [53]
    Dong W,Zhu J,Min X H.Calculation of the heat transfer and temperature on the aircraft anti-icing surface［R］.Nice,France:27th International Congress of the Aeronautical Sciences,2010.
    [54]
    王超，常士楠，杨波，等.机翼防冰过程中冰脊问题的数值分析［J］.北京航空航天大学学报,2013,39(6):776-781. WANG Chao,CHANG Shinan,YANG Bo,et al.Investigation of runback ice during aircraft anti-icing process［J］.Journal of Beijing University of Aeronautics and Astronautics,2013,39(6):776-781.(in Chinese)
    [55]
    王昆，白俊强，夏露，等.飞机热气防冰系统与冰脊预测的数值模拟［J］.航空动力学报,2014,29(11):2694-2703. WANG Kun,BAI Junqiang,XIA Lu,et al.Numerical simulation of aircraft bleed air anti-icing system and ice ridge prediction［J］.Journal of Aerospace Power,2014,29(11):2694-2703.(in Chinese)
    [56]
    Wang H,Tran P,Habashi W G，et al.Anti-icing simulation in wet air of a piccolo system using FENSAP-ICE［R］.SAE Paper 2007-01-3357，2007.
    [57]
    Gray V H,von Glahn U H.Effect of ice and frost formations on drag of NACA 65 (sub-1)1212 airfoil for various modes of thermal ice protection［R］.NACA TN-2962,1953.
    [58]
    Papadakis M,Wong S H,Yeong H W，et al.Icing tests of a wing model with a hot-air ice protection system［R］.AIAA-2010-7833，2010.
    [59]
    Papadakis M,Rodriguez A O Z,Domingos R H.Experimental and computer model results for a bleed air ice protection system［R］.SAE Technical Paper 2011-38-0034,2011.
    [60]
    Whalen E A,Broeren A P,Bragg M B.Characteristics of runback ice accretions on airfoils and their aerodynamic effects［R］.AIAA-2005-1065，2005.
    [61]
    肖春华，桂业伟，杜雁霞，等.电加热过程的冰脊形成实验研究［J］.实验流体力学,2010,24(6):52-56. XIAO Chunhua,GUI Yewei,DU Yanxia,et al.Experimental investigation on the ice ridge formation during the processes of electro-heating［J］.Journal of Experiments in Fluid Mechanics,2010,24(6):52-56.(in Chinese)
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