通用飞机结冰适航验证关键技术及工程应用
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: 335-350&&&&DOI: 10.-08
部件与分系统设计及其他
通用飞机结冰适航验证关键技术及工程应用
王洪伟, 李先哲, 宋展
哈尔滨飞机工业集团有限责任公司, 哈尔滨 150066
Key airworthiness validation technologies for icing of general aviation aircraft and their engineering application
WANG Hongwei, LI Xianzhe, SONG Zhan
Harbin Aircraft Industry Group Co., Ltd., Harbin 150066, China
摘要&民用飞机为获得在结冰环境中的运营许可,必须按照适航当局发布的有关结冰适航条款进行结冰适航验证。与大型运输类飞机相比,通用飞机自身的特点决定了其面临更加严重的结冰问题和更加苛刻的结冰适航验证要求。主要以美国FAA发布的相关结冰适航文件为基础,结合国际上最新的飞机结冰研究成果,并以某通用飞机结冰适航验证的实际工程过程为例,论述通用飞机结冰适航验证中的一些关键技术现状、要求及发展趋势。通过论述可知,当前通用飞机的结冰适航验证需要采用多种适航验证技术的有机组合才能完成,结冰问题已经成为飞机总体气动设计中不可分割的组成部分。
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Abstract:&Civil aircraft must conduct icing airworthiness validation according to relevant icing requirements published by airworthiness authority in order to obtain operation permit in icing environment.The features of general aviation aircraft result in the fact that general aviation aircraft face more severe icing problems and more strict icing airworthiness certification requirements when compared to large transport category aircraft.This paper researches relevant icing airworthiness documents published by FAA and recent international achievements on icing problems,and then discusses some key icing airworthiness validation technologies for general aviation aircraft,their state of art and development trends,based on an engineering application of icing airworthiness validation for a general aviation aircraft.This paper shows that a deliberate combination of several icing airworthiness validation technologies is necessary for general aviation aircraft's icing airworthiness certification program and the issues of icing has become a part of aircraft's aerodynamic layout technology.
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王洪伟,Tel.:3,E-mail:&&&
作者简介:& 王洪伟 男,学士,研究员级高级工程师。主要研究方向:飞机空气动力设计、飞机除防冰设计技术。Tel:3,E-mail:feijisuo@avic.李先哲 男,学士,研究员级高级工程师。主要研究方向:飞机总体设计、飞机空气动力设计。E-mail:feijisuo@avic.宋展 男,学士,研究员级高级工程师。主要研究方向:飞机总体设计、飞机空气动力设计。E-mail:
引用本文:& &&
王洪伟, 李先哲, 宋展. 通用飞机结冰适航验证关键技术及工程应用[J]. 航空学报, ): 335-350.
WANG Hongwei, LI Xianzhe, SONG Zhan. Key airworthiness validation technologies for icing of general aviation aircraft and their engineering application. Acta Aeronautica et Astronautica Sinica, ): 335-350.
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[1] GREEN S D.A study of U.S.inflight icing accidents,1978 to 2002:AIAA-[R].Reston:AIAA,2006.
[2] SMALLEY C L.Certification of Part 23 airplanes for flight in icing conditions:AC 23.1419-2D[R].Washington,D.C.:FAA,2007.
[3] CABLER S J M.Aircraft ice protection:AC 20-73A[R].Washington,D.C.:FAA,2006.
[4] MCGRATH J K.Radio technical commission for aeronautic,Inc.Document RTCA/DO-178B:AC 20-115B[R].Washington,D.C.:FAA,1993.
[5] BEARD M C.Hazards following ground deicing and groundoperations in conditions conducive to aircraft icing:AC 20-117[R].Washington,D.C.:FAA,1982.
[6] HEMPE D W.Turbojet,turboprop,and turbofan engine induction system icing and ice ingestion:AC 20-147[R].Washington,D.C.:FAA,2004.
[7] CABLER S J M.RTCA Document DO-160E,environmental conditions and test procedures for airborne equipment:AC 21-16E[R].Washington,D.C.:FAA,2005.
[8] JACKSON J E.Powerplant guide for certification of Part 23 airplanes and airships:AC 23-16A[R].Washington,D.C.:FAA,2004.
[9] SHOWERS D R.Systems and equipment guide for certification of Part 23 airplanes:AC 23-17B[R].Washington,D.C.:FAA,2004.
[10] BAKER D D.Means of compliance with title 14 CFR,Part 23,& 23.629,flutter:AC 23.629-1B[R].Washington,D.C.:FAA,2004.
[11] JACKSON J E.Equipment,systems,and installations in Part 23 airplanes:AC 23.1309-1C[R].Washington,D.C.:FAA,1999.
[12] BALLOUGH J J.Pilot guide flight in icing conditions:AC 91-74[R].Washington,D.C.:FAA,2002.
[13] HARRINGTON D R.Pilot guide large aircraft ground deicing:AC 120-58[R].Washington,D.C.:FAA,1992.
[14] DALBEY C B.Ground deicing and anti-icing program:AC 120-60B[R].Washington,D.C.:FAA,2004.
[15] WHITE W J.Ground deicing & anti-icing training & checking:AC 135-16[R].Washington,D.C.:FAA,1994.
[16] WHITE W J.Pilot guide small aircraft ground deicing(pocket):AC 135-17[R].Washington,D.C.:FAA,1994.
[17] MALONE D K.Flight test guide for certification of Part 23 airplanes:AC 23-8B[R].Washington,D.C.:FAA,2003.
[18] POTAPCZUK M G.LEWICE/E:An Euler based ice accretion code:NASA TM-105389[R].Washington,D.C.:NASA,1992.
[19] RUFF G A,BERKOWITZ B M.Users manual for the NASA Lewis ice accretion prediction code(LEWICE):NASA CR-185129[R].Washington,D.C.:NASA,1990.
[20] BRANDI M V,ESPOSITO B.Ice accretion prediction on multi-element airfoils:AIAA-[R].Reston:AIAA,1997.
[21] FORTIN G,ILINCA A,LAFORTE J L,et al.Prediction of 2D airfoil ice accretion by bisection method and by rivulets and beads modeling:AIAA-[R].Reston:AIAA,2003.
[22] FORTIN G,LAFORTE J L,BEISSWENGER A.Prediction of ice shapes on NACA0012 airfoil:AIAA-4[R].Reston:AIAA,2003.
[23] BOURGAULT Y,HABASHI W G,BEAUGENDRE H.Development of a shallow water icing model in Fensap-Ice:AIAA-[R].Reston:AIAA,1999.
[24] CROCE G,BEAUGENDRE H,HABASHI W G.CHT3D:FENSAP-ICE conjugate heat transfer computations with droplet impingement and runback effects:AIAA-[R].Reston:AIAA,2002.
[25] BEAUGENDRE H,MORENCY F,HABASHI W G.FENSAP-ICE:Roughness effects on ice shape prediction:AIAA-[R].Reston:AIAA,2003.
[26] MYERS T G.Extension to the Messinger model for aircraft icing[J].AIAA Journal,):211-218.
[27] HEINRICH A,ROSS R,ZUMWALT G,et al.Aircraft icing handbook:FAA Technical Report DOT/FAA/CT-88/8-1[R].Washington,D.C.:FAA,1991.
[28] BARTLETT C S.An analytical study of icing similitude for aircraft engine testing:DOT/FAA/CT-86/35 and AEDC-TR-86-26[R].Washington,D.C.:FAA,1986.
[29] BARTLETT C S.Icing scaling considerations for aircraft engine testing:AIAA-[R].Reston:AIAA,1988.
[30] BARTLETT C S.An empirical look at tolerances in setting icing test conditions with particular application to icing similitude:DOT/FAA/CT-87/31 and AEDC-TR-87-23[R].Washington,D.C.:FAA,1988.
[31] OLESKIM M M,GREGORIO F D,ESPOSITO B,et al.The effect of altitude on icing tunnel airfoil icing simulation:DOT/FAA/AR-96/81,Ⅱ[R].Washington,D.C.:FAA,1996.
[32] ANDERSON D N.Manual of scaling methods:NASA/CR-[R].Washington,D.C.:NASA,2004.
[33] SAEED F,SELIG M S,BRAGG M B.A hybrid airfoil design method to simulate full-scale ice accretion throughout a given C(l)-range:AIAA-[R].Reston:AIAA,1997.
[34] BROEREN A P,BRAGG M B.Effect of residual and intercycle ice accretions on airfoil performance:DOT/FAA/AR-02/68[R].Washington,D.C.:FAA,2002.
[35] PELLICANO P.Residual and inter-cycle ice for lower-speed aircraft with pneumatic boots:AIAA-[R].Reston:AIAA,2007.
[36] PELLICANO P.Supercooled large drop(SLD) icing and certification of Part 23 airplanes[C]//FAA 2009 Small Airplane Directorate Program Managers Meeting,2009.
[37] JONES A R,LEWIS W.Recommended values of meteorological factors to be considered in the design of aircraft ice-prevention equipment:NACA-TN-1855[R].Washington,D.C.:NACA,1949.
[38] HACKER P T,DORSCH R G.A summary of meteorological conditions associated with aircraft icing and a proposed method of selecting design criterions for ice-protection equipment:NACA-TN-2569[R].Washington,D.C.:NACA,1951.
[39] LEWIS W,BERGRUN N R.A probability analysis of the meteorological factors conductive to aircraft icing in the United States:NACA-TN-2738[R].Washington,D.C.:NACA,1952.
[40] BOWDEN D T,GENSEMER A E,SKEEN C A.Engineering summary of airframe icing technical data:FAA Technical Report ADS-4[R].Washington,D.C.:FAA,1964.
[41] GRAY V H.Correlations among ice measurements,impingement rates,icing conditions,and drag coefficients for unswept NACA 65A004 airfoil:NACA-TN-4151[R].Washington,D.C.:NACA,1958.
[42] 张杰,周磊,张洪,等.飞机结冰探测技术[J].仪器仪表学报,):.ZHANG J,ZHOU L,ZHANG H,et al.Aircraft icing detection technology[J].Chinese Journal of Scientific Instrument,):(in Chinese).
[43] LEE S,BRAGG M B.Effects of simulated-spanwise-ice shapes on airfoils:Experimental investigation:AIAA-[R].Reston:AIAA,1999.
[44] LEE S,KIM H S,BRAGG M B.Investigation of factors that influence iced-airfoil aerodynamics:AIAA-[R].Reston:AIAA,2000.
王兴, 晏晓瑜. [J]. 航空学报, ): 529.
闫文辉, 薛然然. [J]. 航空学报, ): 515.
王建锋, 卜忱, 谭浩. [J]. 航空学报, ): 521.
胡剑平, 任国哲, 易军, 刘振侠, 吕亚国, 赵静宇. [J]. 航空学报, ): 013.
祝培源, 宋立明, 李军, 丰镇平. [J]. 航空学报, ): 942.
陈云永, 万科, 杨小贺, 丁建国. [J]. 航空学报, ): 951.
张征宇, 王显圣, 黄叙辉, 周润, 茆骥. [J]. 航空学报, ): 989.
朱呈祥, 陈荣钱, 尤延铖. [J]. 航空学报, ): 764.
雷桂林, 郑梅, 董威, 周志翔, 董奇. [J]. 航空学报, ): 066.
林家泉, 李弯弯. [J]. 航空学报, ): 089.
丁明松, 江涛, 董维中, 高铁锁, 刘庆宗. [J]. 航空学报, ): 030.
王显圣, 杨党国, 刘俊, 施傲, 周方奇, 吕彬彬. [J]. 航空学报, ): 873.
代晓晴, 张翔, 李森, 郑建弘. [J]. 航空学报, ): 076.
李鑫郡, 张靖周, 谭晓茗. [J]. 航空学报, ): 982.
姜裕标, 王万波, 常智强, 黄勇. [J]. 航空学报, ): 751.
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