机翼热气防冰系统设计

卜雪琴; 郁嘉; 林贵平; 宋馨

机翼热气防冰系统设计

北京航空航天大学航空科学与工程学院, 北京 100191

详细信息

作者简介:
卜雪琴(1982-),女,江西萍乡人,博士生,buxueqin@ase.buaa.edu.cn.

中图分类号: V 224; V 244.1⁺5
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- 被引次数: 0
出版历程
- 收稿日期: 2009-06-29
- 网络出版日期: 2010-08-30

Investigation of the design of wing hot-air anti-icing system

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 利用热流体系统仿真分析平台Flowmaster和计算流体力学软件Fluent进行联合仿真,对机翼热气防冰系统进行了设计和性能分析.设计参数包括防冰系统笛形管热气喷口孔径、孔数及孔间距等参数.基于Flowmaster对所设计的供气管路进行供气流量分配计算.基于Fluent模拟防冰腔内流动与换热,计算了防冰腔的热效率.根据防冰热载荷及热效率结果预测每段缝翼防冰所需热气流量,引入参数供气余度来分析防冰系统热性能.所提出的热气防冰系统设计方法可为热气防冰系统的工程设计与优化提供重要的帮助.
- 热气防冰系统 /
- 设计 /
- 笛形管 /
- 热性能 /
- 供气余度
Abstract: The thermal fluid system simulation tool Flowmaster and the computational fluid dynamic tool Fluent were combined for the simulation of the wing hot-air anti-icing system (WHAIS) design and thermal performance analysis. The design parameters contained the piccolo tube diameter, the jet hole diameter and the distance between holes. Mass flow of the hot air distribution per slat supplied by system was evaluated based on Flowmaster. Thermal efficiency of the WHAIS was predicted based on Fluent. The heat required for anti-icing was determined according to the results of external heat loads and the thermal efficiency of the system. Margin of the hot-air supply was introduced to analyze the WHAIS thermal performance. The method presented can be used in the engineering design and optimization of the WHAIS.
- hot-air anti-icing system /
- design /
- piccolo tube /
- thermal performance /
- margin of air supply

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参考文献(1)

[1] Saeed F,Al-Garni A Z.Numerical simulation of surface heat transfer from an array of hot air jets .AIAA-2007-4287,2007 [2] Lee J,Rigdy D,Wright W,et al.Analysis of thermal ice protection system(TIPS) with piccolo tube using state-of-the-art software .AIAA -2006-1011,2006 [3] Silva G A L,Silvares O M,Zerbini E J G J.Numerical simulation of airfoil thermal anti-ice operation part 1:mathematical modeling[J].Journal of Aircraft,2007,44(2):627-634 [4] Tong X L,Luke E A.Eulerian simulations of icing collection efficiency using a singularity diffusion model .AIAA-2005-1246,2005 [5] 卜雪琴,林贵平.基于CFD的水收集系数及防冰表面温度预测[J].北京航空航天大学学报,2007,33(10):1182-1185 Bu Xueqin,Lin Guiping.Predictions of collection efficiency and anti-icing surface temperature[J].Journal of Beijing University of Aeronautics and Astronautics,2007,33(10):1182-1185 (in Chinese) [6] 卜雪琴,林贵平,彭又新,等.防冰热载荷计算的一种新方法[J].航空学报,2006,27(2):208-212 Bu Xueqin,Lin Guiping,Peng Youxin,et al.Method for calculation of anti-icing heat loads[J].Acta Aeronautica et Astronautica Sinica,2006,27(2):208-212 (in Chinese) [7] 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 Qiu Xiegang,Han Fenghua.Aircraft anti-icing system[M].Beijing:Compilation and Examination Group of Aero Specialized Teaching Materials,1985 (in Chinese) [8] Messinger B L.Equilibrium temperature of an unheated icing surface as a function of air speed[J].Journal of the Aeronautical Sciences,1953,20(1):29-42

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