基于PHengLEI的非稳态电热除冰过程仿真

刘宗辉; 卜雪琴; 林贵平; 李伟斌

doi:10.7638/kqdlxxb-2021.0353

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基于PHengLEI的非稳态电热除冰过程仿真

研究论文 | 更新时间：2026-05-28

- 基于PHengLEI的非稳态电热除冰过程仿真
- Simulation of unsteady electrothermal deicing process based on PHengLEI
- 空气动力学学报 2023年41卷第2期页码：53-63
- 作者机构：
  
  1. 北京航空航天大学航空科学与工程学院,北京,100083
  2. 中国空气动力研究与发展中心,绵阳,621000
- 作者简介：
  
  刘宗辉（1998-），男，湖北恩施人，硕士研究生，研究方向：飞机防/除冰技术. E-mail：lzh2677@buaa.edu.cn
  卜雪琴*，副教授，研究方向：飞机和发动机结冰与防除冰技术. E-mail：buxueqin@buaa.edu.cn
- 基金信息：
  
  国家数值风洞工程（ NNW）
- DOI：10.7638/kqdlxxb-2021.0353
  中图分类号： V321.2+29;V211.3
- 纸质出版：2023
- 稿件说明：
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刘宗辉, 卜雪琴, 林贵平, 等. 基于PHengLEI的非稳态电热除冰过程仿真[J]. 空气动力学学报, 2023, 41(2): 53−63.

LIU Zonghui, BU Xueqin, LIN Guiping, et al. Simulation of unsteady electrothermal deicing process based on PHengLEI[J]. 2023, 41(2): 53-63.
刘宗辉, 卜雪琴, 林贵平, 等. 基于PHengLEI的非稳态电热除冰过程仿真[J]. 空气动力学学报, 2023, 41(2): 53−63. DOI： 10.7638/kqdlxxb-2021.0353

LIU Zonghui, BU Xueqin, LIN Guiping, et al. Simulation of unsteady electrothermal deicing process based on PHengLEI[J]. 2023, 41(2): 53-63. DOI： 10.7638/kqdlxxb-2021.0353.

摘要

为了填补国产自主可控CFD软件风雷平台的防除冰功能开发的空白，本文建立了电热除冰计算模型、计算方法和非稳态导热模型，并在国家数值风洞风雷平台（PHengLEI）基础上，集成了非稳态电热除冰计算和非稳态导热计算功能。通过与主流商业CFD软件仿真结果和实验数据的对比，验证了导热和非稳态电热除冰程序的准确性。针对某飞行工况进行了电热除冰计算，通过对表面溢流水、表面温度、结冰量的计算结果分析，发现合理布局加热片、设计加热热流密度和电热除冰控制率，可实现电热除冰系统的安全运行和能源的高效利用。

Abstract

Aircraft can encounter ice accretion on the windward surface as they fly through clouds that contain sub-cooled water droplet

which can then affect the aircraft performance and pose extremely serious threats to the flight safety. Electrothermal deicing is an important measure for aircraft icing protection. In this study

the numerical model and method for electrothermal deicing together with an unsteady heat conduction model have been established. Based on the “National Numerical Windtunnel” PHengLEI platform

the newly proposed model for unsteady electrothermal deicing is integrated. By comparing with the simulation results of widely used commercial CFD software and experimental data

the accuracy of the integrated unsteady electrothermal deicing program is verified. Simulations for electrothermal deicing under certain working conditions are carried out. Through analyses of the calculated surface overflow water

surface temperature and icing volume

it is found that a reasonable design of the heater layout

the heating heat flux and the electric heating deicing control rate

can help achieve the safe operation of the electrothermal deicing system and improve the efficient use of energy.

关键词

Keywords

references

CHAUVIN R, VILLEDIEU P, TRONTIN P, et al. A robust coupling algorithm applied to thermal ice protection system unsteady modeling[C]// 6th AIAA Atmospheric and Space Environments Conference, Atlanta, GA. Reston, Virginia: AIAA, 2014. doi: 10.2514/6.2014-2061

FOSSATI M, HABASHI W G, BARUZZI G S. Simulation of supercooled large droplet impingement via reduced order technology[J]. Journal of Aircraft, 2012, 49(2): 600-610. DOI:10.2514/1.c031608

POURBAGIAN M, HABASHI W. CFD-based optimization of electro-thermal wing ice protection systems in de-icing mode[C]// 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Grapevine (Dallas/Ft. Worth Region), Texas. Reston, Virigina: AIAA, 2013. doi: 10.2514/6.2013-654

BOTURA G, FLOSDORF D, SWEET D. Concept development of low power electrothermal de-icing system[C]// 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virigina: AIAA, 2006. doi: 10.2514/6.2006-864

CHEN W J, ZHANG D L. Numerical simulation of glaze ice accretion process[J]. Journal of Aerospace Power, 2005, 20(3): 472-476. (in Chinese)

BENNANI L, VILLEDIEU P, SALAUN M. Two dimensional model of an electro-thermal ice protection system[C]// 5th AIAA Atmospheric and Space Environments Conference, San Diego, CA. Reston, Virginia: AIAA, 2013. doi: 10.2514/6.2013-2936

AI J B, DENG J H, LIU D J. Deicing structure design of helicopter rotor blade[J]. Helicopter Technique, 2005(2): 12-15. (in Chinese)

CHANG S N, LIU D J, YUAN X G. Research on protected range of the anti-icing/deicing system for helicopter rotor[J]. Journal of Aerospace Power, 2007, 22(3): 360-364. (in Chinese)

CHANG S N, HOU Y Q, YUAN X G. Influence of periodic electro-heating pulse on deicing surface temperature[J]. Journal of Aerospace Power, 2007, 22(8): 1247-1251. (in Chinese)

CHANG S N, AI S X, HUO X H, et al. Improved simulation of electrothermal de-icing system[J]. Journal of Aerospace Power, 2008, 23(10): 1753-1758. (in Chinese)

BU X Q. Numerical simulation of the hot-air anti-icing system[D]. Beijing: Beihang University 2010. (in Chinese)

XIAO C H. Study on heat transfer characteristics and effects of electrothermal aircraft deicing[D]. Mianyang: China Aerodynamics Research and Development Center, 2010 (in Chinese) .

SHEN X B, LIN G P, YU J, et al. Three-dimensional numerical simulation of ice accretion at the engine inlet[J]. Journal of Aircraft, 2013, 50(2): 635-642. DOI:10.2514/1.c031992

FU J P, ZHUANG W L, YANG B, et al. Simulation of heating control law of electro-thermal deicing of helicopter rotor blade[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(9): 1200-1207. (in Chinese)

YANG S Y, CHANG S N, GAO Y X, et al. Investigation of rotary cone electric heating anti-icing transient process[J]. Acta Aerodynamica Sinica, 2016, 34(3): 289-294, 307. (in Chinese)

MU Z D, LIN G P, SHEN X B, et al. Numerical simulation of unsteady conjugate heat transfer of electrothermal deicing process[J]. International Journal of Aerospace Engineering, 2018, 2018: 5362541. DOI:10.1155/2018/5362541

SHEN X B, WANG H F, LIN G P, et al. Unsteady simulation of aircraft electro-thermal deicing process with temperature-based method[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, 234(2): 388-400. DOI:10.1177/0954410019866066

ZHAO Z, HE L, HE X Y. Design of general CFD software PHengLEI[J]. Computer Engineering and Science, 2020, 42(2): 210-219. (in Chinese)

ZHAO Z, ZHANG L P, HE L, et al. PHengLEI: a large scale parallel CFD framework for arbitrary grids[J]. Chinese Journal of Computers, 2019, 42(11): 2368-2383. (in Chinese)

MU Z D. Study on aircraft icing and electrothermal deicing process [D]. Beijing: Beihang University 2018 (in Chinese).

MILLER D, BOND T, SHELDON D, et al. Validation of NASA thermal ice protection computer codes. I - Program overview[C]// 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. Reston, Virigina: AIAA, 1997. doi: 10.2514/6.1997-49

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