基于容冰概念的民机结冰保护系统设计方法研究综述 -- 西北工业大学学报,2021,39(4):731-738

	论文:2021,Vol:39,Issue(4):731-738
	引用本文：
	赵宾宾, 黎先平, 李杰, 陈海昕, 艾剑良. 基于容冰概念的民机结冰保护系统设计方法研究综述[J]. 西北工业大学学报
	ZHAO Binbin, LI Xianping, LI Jie, CHEN Haixin, AI Jianliang. Research review on design method of ice protection system for civil aircraft based on ice-tolerant concept[J]. Northwestern polytechnical university

基于容冰概念的民机结冰保护系统设计方法研究综述

赵宾宾^1,2, 黎先平², 李杰¹, 陈海昕³, 艾剑良⁴

1. 西北工业大学航空学院, 陕西西安 710072;
2. 中国商飞上海飞机设计研究院, 上海 201210;
3. 清华大学航天航空学院, 北京 100084;
4. 复旦大学航空航天系, 上海 200433

摘要:

结冰是威胁民机飞行安全的重要致灾因素，也是适航审查方关注的重大安全问题。基于容冰概念开展结冰保护系统设计，最大程度降低结冰对飞机气动特性的影响，充分发挥飞行性能潜力，是当前民用飞机结冰防护研究的前沿方向。针对民机飞行安全性设计和适航认证需求，从飞机本体容冰设计和主动控制容冰设计两方面出发，对基于容冰概念的民机结冰保护系统设计方法进行分析。针对结冰损失，提炼了考虑结冰损失的机翼气动优化设计策略，形成了基于飞行控制律重构的容冰保护控制系统设计思路，将"被动结冰飞行安全"向"主动结冰安全设计"转变，能够有效提升民机在结冰气象条件下的生存力和安全性。

关键词: 飞机结冰结冰保护容冰设计飞行控制律

Research review on design method of ice protection system for civil aircraft based on ice-tolerant concept

ZHAO Binbin^1,2, LI Xianping², LI Jie¹, CHEN Haixin³, AI Jianliang⁴

1. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. Shanghai Aircraft Design and Research Institute, Shanghai 201210, China;
3. School of Aerospace Engineering, Tsinghua University, Beijing 100084, China;
4. Department of Aeronautics and Astronautics, Fudan University, Shanghai 200433, China

Abstract:

Icing is an important disaster-causing factor which threatens the flight safety of civil aircraft and a major safety issue of concern for the airworthiness. The design of icing protection system based on ice-tolerant concept can minimize the impact of icing on aerodynamic characteristics and fully utilize the potential of flight performance, which is the frontier direction of current icing protection research for civil aircraft. This paper aims at the requirements of civil aircraft flight safety design and airworthiness certification. The design method of civil aircraft icing protection system based on the concept of ice-tolerant capacity is analyzed from two aspects. One is the capacity of ice-tolerant for aircraft frame, the other one is the design of ice-tolerant with active control. The optimum design strategy of wing in aerodynamic performance considering icing loss is refined and the design idea of ice-tolerant protection control system based on flight control law reconstruction is formed. The change from passive flight safety of icing to active safety design of icing can effectively improve the survivability and safety of civil aircraft under icing weather conditions.

Key words: aircraft icing icing protection ice-tolerant design flight control law

收稿日期: 2020-12-19 修回日期:

DOI: 10.1051/jnwpu/20213940731

基金项目: 国家自然科学基金（11972304）与航空科学基金（2019ZA053005）资助

通讯作者: 李杰(1969-),西北工业大学教授,主要从事设计空气动力学及计算流体力学研究。e-mail:lijieruihao@nwpu.edu.cn Email：lijieruihao@nwpu.edu.cn

作者简介: 赵宾宾(1985-),西北工业大学博士研究生,主要从事民机结冰研究。

相关功能

PDF(1703KB) Free

打印本文

把本文推荐给朋友

作者相关文章

赵宾宾 在本刊中的所有文章

黎先平 在本刊中的所有文章

李杰在本刊中的所有文章

陈海昕 在本刊中的所有文章

艾剑良 在本刊中的所有文章


	参考文献:
	[1] 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 LIN Guiping, PU Xueqin, SHEN Xiaobin, et al. Icing and anti icing technology for aircraft[M]. Beijing:Beijing University of Aeronautics and Astronautics Press, 2016(in Chinese) [2] 应思斌. 飞机容冰飞行控制系统设计的理论与方法研究[D]. 上海:复旦大学, 2010 YING Sibin. Study on the theory and methods of aircraft icing tolerant flight control system design[D]. Shanghai:Fudan University, 2010(in Chinese) [3] BRAGG M B, HUTCHISON T, MERRET J. Effect of ice accretion on aircraft flight dynamics[C]//38th Aerospace Sciences Meeting and Exhibit, 2000 [4] 张强. 民用飞机临界冰型确定策略浅析[J]. 民用飞机设计与研究, 2019(1):53-58 ZHANG Qiang. Determination method of critical ice shapes for large civil aircraft[J]. Civil Aircraft Design & Research, 2019(1):53-58(in Chinese) [5] BRAGG M B, BROEREN A P, BLUMENTHAL L A. Iced-airfoil aerodynamics[J]. Progress in Aerospace Sciences, 2005, 41(5):323-362 [6] STEBBINS S J, LOTH E, BROEREN A P, et al. Review of computational methods for aerodynamic analysis of iced lifting surfaces[J]. Progress in Aerospace Sciences, 2019, 111:100583 [7] GHISU T, JARRETT J P, PARKS G T. Robust design optimization of airfoils with respect to ice accretion[J]. Journal of Aircraft, 2011, 48(1):287-304 [8] JAEGGI D M, PARKS G T, KIPOUROS T, et al. The development of a multi-objective tabu search algorithm for continuous optimization problems[J]. European Journal of Operational Research, 2008, 185(3):1192-1212 [9] LI H R, ZHANG Y F, CHEN H X. Optimization of supercritical airfoil considering the ice-accretion effects[J]. AIAA Journal, 2019, 57(11):4650-4669 [10] DENG K, CHEN H. A hybrid aerodynamic optimization algorithm based on differential evolution and RBF response surface[C]//17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2016 [11] 李航航, 周敏. 飞机结冰探测技术及防除冰系统工程应用[J]. 航空工程进展, 2010(2):112-115 LI Hanghang, ZHOU Min. Engineering application of icing detection technique and anti-icing and deicing system on aircraft[J]. Advances in Aeronautical Science and Engineering, 2010(2):112-115(in Chinese) [12] 张杰, 周磊, 张洪, 等. 飞机结冰探测技术[J]. 仪器仪表学报, 2006, 27(12):1578-1586 ZHANG Jie, ZHOU Lei, ZHANG Hong, et al. Aircraft icing detection technology[J]. Chinese Journal of Scientific Instrument, 2006, 27(12):1578-1586(in Chinese) [13] MELODY J W, BAAR T, PERKINS W R, et al. Parameter identification for inflight detection and characterization of aircraft icing[J]. Control Engineering Practice, 2000, 8(9):985-1001 [14] 倪章松,刘森云,王桥, 等. 3 m×2 m结冰风洞试验技术研究进展[J]. 实验流体力学,2019,33(6):46-53 NI Zhangsong, LIU Senyun, WANG Qiao, et al. Research progress of test technologies for 3 m×2 m icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(6):46-53(in Chinese) [15] 易贤,桂业伟,朱国林. 飞机三维结冰模型及其数值求解方法[J]. 航空学报, 2010,31(11):2152-2158 YI Xian, GUI Yewei, ZHU Guolin. Numerical method of a three-dimensional ice accretion model of aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2010,31(11):2152-2158(in Chinese) [16] STEBBINS S, LOTH E, BROEREN A, et al. Aerodynamics of a common research model wing with leading-edge ice shape[J]. Journal of Aircraft, 2021(85):1-13 [17] SPALART P R, JOU W, STRELETS M et al. Comments on the feasibility of LES for wings and on a hybrid RANS/LES approach[M]. Los Angles, Greyden Press, 1997 [18] XIAO M, ZHANG Y. Improved prediction of flow around airfoil accreted with horn or ridge ice[J]. AIAA Journal, 2021(3):1-10 [19] 孔满昭,段卓毅,马玉敏. 机翼展向不同部位结冰对飞机气动力特性影响研究[J]. 实验流体力学,2016,30(2):32-37 KONG Manzhao, DUAN Zhuoyi, MA Yumin. Study on aerodynamic characteristics of ice accretion in different wing span sections[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(2):32-37(in Chinese) [20] 赵克良. 大型民机结冰计算、风洞试验及试飞验证[D]. 南京:南京航空航天大学, 2017 ZHAO Keliang. Icing calculation, wind tunnel experiment and flight test for large civil aircraft[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2017(in Chinese) [21] RATVASKY T, VAN ZANTE J. In-flight aerodynamic measurements of an iced horizontal tailplane[C]//37th Aerospace Sciences Meeting and Exhibit, 1999 [22] HOSSAIN K, SHARMA V, BRAGG M, et al. Envelope protection and control adaptation in icing encounters[C]//41st Aerospace Sciences Meeting and Exhibit, 2003 [23] 应思斌, 艾剑良. 飞机结冰包线保护对开环飞行性能影响与仿真[J]. 系统仿真学报, 2010(10):2273-2275 YING Sibin, AI Jianliang. Simulation of aircraft flight envelope protect in icing encounters effects on open loop dynamics[J]. Journal of Sytem Simulation, 2010, 22(10):2273-2275(in Chinese)

邮编:710072 电话：029-88495455 Email：xuebao@nwpu.edu.cn

本系统由北京仁和汇智信息技术有限公司设计开发技术支持：info@rhhz.net