Review of Ice Crystal Icing in Aero-Engines

Journal of Propulsion Technology ›› 2018, Vol. 39 ›› Issue (12): 2641-2650.

School of Energy and Power Engineering，Beihang University，Beijing 100191,School of Energy and Power Engineering，Beihang University，Beijing 100191;Beijing Key Laboratory of Aero-Engine Structure and Strength，Beijing 100191;Collaborative Innovation Center for Advanced Aero-Engine，Beijing 100191 and School of Energy and Power Engineering，Beihang University，Beijing 100191;Beijing Key Laboratory of Aero-Engine Structure and Strength，Beijing 100191;Collaborative Innovation Center for Advanced Aero-Engine，Beijing 100191

Published:2021-08-15

航空发动机内部冰晶结冰研究综述

袁庆浩¹,樊江^1,2,3,白广忱^1,2,3

北京航空航天大学能源与动力工程学院，北京 100191,北京航空航天大学能源与动力工程学院，北京 100191; 航空发动机结构强度北京市重点试验室，北京 100191; 先进航空发动机协同创新中心，北京 100191,北京航空航天大学能源与动力工程学院，北京 100191; 航空发动机结构强度北京市重点试验室，北京 100191; 先进航空发动机协同创新中心，北京 100191

作者简介:袁庆浩，男，博士生，研究领域为航空发动机冰晶结冰、冰雹撞击、热流固耦合计算。E-mail: yuanqinghao@buaa.edu.cn 通讯作者:樊江，男，博士，副教授，研究领域为多学科优化设计、航空发动机冰吸入、热流固耦合计算。

Abstract

Abstract: In order to deeply understand the ice crystal icing(ICI) phenomenon in aero-engines， grasp the characteristics of ICI process， and establish scientific and effective ICI protection means， literature and data on ICI in recent years were investigated and summarized. The discovery and confirmed processes of ICI were reviewed. The differences between ICI and supercooled water icing， simulation tests and computational methods of ICI were emphasized. At last， several directions for the further research on the ICI problem were proposed.

Key words: Ice crystal icing；Mixed-phase；High altitude；Supercooled water droplets；Wet-bulb temperature；Review

摘要： 为深入理解航空发动机内部冰晶结冰现象，把握冰晶结冰过程的特征规律，建立科学有效的冰晶结冰防护手段，对近年来冰晶结冰文献资料进行了调研和总结。回顾了冰晶结冰现象的发现与证实的过程，重点阐述冰晶结冰与过冷水结冰的区别、冰晶结冰模拟试验及计算方法，并对冰晶结冰问题有待进一步研究的方向做了展望。

关键词: 冰晶结冰；混合相；高空；过冷水滴；湿球温度；综述

YUAN Qing-hao¹,FAN Jiang^1,2,3,BAI Guang-chen^1,2,3. Review of Ice Crystal Icing in Aero-Engines[J]. Journal of Propulsion Technology, 2018, 39(12): 2641-2650.

袁庆浩,樊江,白广忱. 航空发动机内部冰晶结冰研究综述[J]. 推进技术, 2018, 39(12): 2641-2650.

References

[1] Mason J G, Strapp J W, Chow P. The Ice Particle Threat to Engines in Flight[R]. AIAA 2006-206.
[2] Mason J. Engine Power Loss in Ice Crystal Conditions[J]. AERO, 2007, 4(7): 12-17.
[3] Pasztor A. Airline Regulators Grapple with Engine-Shutdown Peril[J]. Wall Street Journal, 2008, 251(81).
[4] 陈光. GEnx发动机结冰问题初探[J]. 国际航空, 2014, (2): 72-73.
[5] Grzych M L, Mason J. Weather Conditions Associated with Jet Engine Power-Loss and Damage due to Ingestion of Ice Particles: What We’ve Learned through 2009[C]. Washington, DC: 14th Conference on Aviation, Range, and Aerospace Meteorology, 2010.
[6] Mason J G, Chow P, Dan M F. Understanding Ice Crystal Accretion and Shedding Phenomenon in Jet Engines Using a Rig Test[R]. ASME GT 2010-22550.
[7] 杜雁霞, 李明, 桂业伟, 等. 飞机结冰热力学行为研究综述[J]. 航空学报, 2017, 38(2): 25-36.
[8] Zhang L, Liu Z, Zhang M. Numerical Simulation of Ice Accretion under Mixed-Phase Conditions[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2016, 230(13): 2473-2483.
[9] 刘增承. 关于发动机内部结冰的探讨[C]. 北京:全国飞行技术和飞行安全研讨会, 2000.
[10] 林贵平, 卜雪琴, 申晓斌, 等. 飞机结冰与防冰技术[M]. 北京:北京航空航天大学出版社, 2016.
[11] 丁媛媛, 蒋彦龙, 施红, 等. 国外运输类飞机最新结冰适航规章差异初步研究与分析[J]. 民用飞机设计与研究, 2016, (4): 35-39.
[12] 宣益民, 连文磊. 航空发动机整流罩新型防冰方法[J]. 科学通报, 2016, 61(25): 2843-2850.
[13] 张丽芬, 张美华, 吴丁毅, 等. 旋转帽罩结冰相似准则的研究[J]. 推进技术, 2015, 36(8): 1164-1169. (ZHANG Li-fen, ZHANG Mei-hua, WU Ding-yi, et al. Research on Icing Scaling Law for Rotating Cone[J].Journal of Propulsion Technology, 2015, 36(8): 1164-1169.)
[14] 杨军, 张靖周, 郭文, 等. 航空发动机进口支板结冰和防冰试验[J]. 航空动力学报, 2014, 29(2): 277-283.
[15] Haggerty J, Mcdonough F, Black J, et al. A System for Nowcasting Atmospheric Conditions Associated with Jet Engine Power Loss and Damage due to Ingestion of Ice Particles[R]. AIAA 2012-3234.
[16] Mason J. Current Perspectives on Jet Engine Power Loss in Ice Crystal Conditions Engine Icing[C]. Reston, VA: 2008 AIAA Atmospheric and Space Environments Conference 7th AIRA Research Implementation Forum, 2008.
[17] Knezevici D C, Fuleki D, Macleod J. Development and Commissioning of a Linear Compressor Cascade Rig for Ice Crystal Research[R]. SAE 2011-38-0079.
[18] Fuleki D M, Macleod J D. Ice Crystal Accretion Test Rig Development for a Compressor Transition Duct[R]. AIAA 2010-7529.
[19] Griffin T A, Lizanich P, Dicki D J. PSL Icing Facility Upgrade Overview[R]. AIAA 2014-2896.
[20] Struk P M, Tsao J C, Bartkus T P. Plans and Preliminary Results of Fundamental Studies of Ice Crystal Icing Physics in the NASA Propulsion Systems Laboratory[R]. AIAA 2016-3738.
[21] Zante J F V, Rosine B M. NASA Glenn Propulsion Systems Lab: 2012 Inaugural Ice Crystal Cloud Calibration[R]. AIAA 2014-2897.
[22] Struk P M, Broeren A P, Tsao J C, et al. Fundamental Ice Crystal Accretion Physics Studies[R]. SAE 2011-38-0018.
[23] Currie T, Struk P, Tsao J C, et al. Fundamental Study of Mixed-Phase Icing with Application to Ice Crystal Accretion in Aircraft Jet Engines[R]. AIAA 2012-3035.
[24] Knezevici D C, Fuleki D, Currie T C, et al. Particle Size Effects on Ice Crystal Accretion[R]. AIAA 2012-3039.
[25] Lozowski E P, Stallabrass J R, Hearty P F. The Icing of an Unheated, Nonrotating Cylinder, Part II. Icing Wind Tunnel Experiments[J]. Journal of Applied Meteorology, 1983, 22(12): 2063-2074.
[26] Stallabrass J R, Hearty P F. Further Icing Experiments on an Unheated Non-Rotating Cylinder[R]. LTR-LT-105.
[27] Al-khali K. Assessment of Effects of Mixed-Phase Icing Conditions on Thermal Ice Protection Systems[R]. DOT/FAA/AR-03/48.
[28] Bartkus T P, Struk P M, Tsao J C, et al. Numerical Analysis of Mixed-Phase Icing Cloud Simulations in the NASA Propulsion Systems Laboratory[R]. AIAA 2016-3739.
[29] Flegel A B, Oliver M J. Preliminary Results from a Heavily Instrumented Engine Ice Crystal Icing Test in a Ground Based Altitude Test Facility[R]. AIAA 2016-3894.
[30] Veres J P, Jorgenson P, Jones S M. Modeling of Highly Instrumented Honeywell Turbofan Engine Tested with Ice Crystal Ingestion in the NASA Propulsion System Laboratory[R]. AIAA 2016-3895.
[31] Hauk T, Roisman I, Tropea C. Investigation of the Impact Behaviour of Ice Particles[R]. AIAA 2014-3046.
[32] Hauk T. Investigation of the Impact and Melting Process of Ice Particles[D]. Darmstadt: Technische Universit?t Darmstadt, 2016.
[33] Bidwell C, Rigby D. Ice Particle Analysis of the Honeywell ALF502 Engine Booster[C]. Chicago, IL: SAE 2015 International Conference on Icing of Aircraft, Engines, and Structures, 2015.
[34] Jorgenson P C E, Veres J P, Wright W B, et al. Engine Icing Modeling and Simulation, Part I: Ice Crystal Accretion on Compression System Components and Modeling its Effects on Engine Performance[R]. SAE 2011-38-0025.
[35] Villedieu P, Trontin P, Chauvin R. Glaciated and Mixed Phase Ice Accretion Modeling Using ONERA 2D Icing Suite[R]. AIAA 2014-2199.
[36] Kintea D M. Hydrodynamics and Thermodynamics of Ice Particle Accretion[D]. Darmstadt: Technische Universit?t Darmstadt, 2016.
[37] Wright W, Jorgenson P, Veres J. Mixed Phase Modeling in GlennICE with Application to Engine Icing[R]. AIAA 2010-7674.
[38] 邢玉明, 刘海丽, 徐柳青. 飞机发动机结冰研究进展[J]. 空军工程大学学报(自然科学版), 2011, 12(6): 8-12.
[39] 董葳, 赵冬梅. 飞机结冰动力学的研究发展综述[C]. 绵阳:中国第一届近代空气动力学与气动热力学会议, 2006.
[40] Lou D, Hammond D W. Heat and Mass Transfer for Ice Particle Ingestion Inside Aero-Engine[J]. Journal of Turbomachinery, 2011, 133(3).
[41] Myers T G. An Extension to the Messinger Model for Aircraft Icing[J]. AIAA Journal, 2001, 39(2): 211-218.
[42] Tsao J C, Struk P, Oliver M. Possible Mechanisms for Turbofan Engine Ice Crystal Icing at High Altitude[R]. AIAA 2014-3044.
[43] Nilamdeen S, Habashi W G. Multiphase Approach Toward Simulating Ice Crystal Ingestion in Jet Engines[J]. Journal of Propulsion and Power, 2011, 27(5): 959-969.
[44] Kintea D M, Schremb M, Roisman I V. Numerical Investigation of Ice Particle Accretion on Heated Surfaces with Application to Aircraft Engines[R]. AIAA 2014-2820.
[45] May R D, Guo T H, Veres J P, et al. Engine Icing Modeling and Simulation, Part 2: Performance Simulation of Engine Rollback Phenomena[C]. Chicago, IL: SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing, 2011.
[46] May R D, Simon D L, Guo T H. Modeling and Detection of Ice Particle Accretion in Aircraft Engine Compression Systems[R]. AIAA 2012-4649.
[47] Kundu R. Impact of Engine Icing on Jet Engine Compressor Flow Dynamics[D]. Atlanta: Georgia Institute of Technology, 2016.　　　　　　　　　　　　　　收稿日期:2018-01-04；修订日期:2018-04-24。作者简介:袁庆浩,男,博士生,研究领域为航空发动机冰晶结冰、冰雹撞击、热流固耦合计算。E-mail: yuanqinghao@buaa.edu.cn通讯作者:樊江,男,博士,副教授,研究领域为多学科优化设计、航空发动机冰吸入、热流固耦合计算。E-mail: fanjiang@buaa.edu.cn(编辑:朱立影)