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基于热力耦合和融冰相变的电热除冰仿真研究

陈明萱 靳海川 马奎元 宫晗 任仪航 林贵平

航天器环境工程2026,Vol.43Issue(2):111-124,14.
航天器环境工程2026,Vol.43Issue(2):111-124,14.DOI:10.12126/see.2025111

基于热力耦合和融冰相变的电热除冰仿真研究

Numerical simulation of electrothermal de-icing based on thermo-mechanical coupling and ice melting phase change

陈明萱 1靳海川 1马奎元 2宫晗 1任仪航 1林贵平3

作者信息

  • 1. 北京航空航天大学 航空科学与工程学院,北京 100191
  • 2. 北京航空航天大学 国际创新研究院,杭州 310000
  • 3. 北京航空航天大学 航空科学与工程学院,北京 100191||北京航空航天大学 国际创新研究院,杭州 310000
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摘要

Abstract

To accurately simulate the aircraft electrothermal de-icing process,the coupling and synergistic effects among multiple physical fields must be considered.In this study,a multi-step icing numerical model and a multiphysics-coupled de-icing model were established,in which the dynamic interactions among the flow field,temperature field,stress field,and ice melting phase change were fully considered.The stress distribution characteristics at the ice-skin interface and within the two-dimensional accreted ice under chordwise local heating conditions during the de-icing process were analyzed,and the critical local heating range was determined based on multiphysics-coupled simulations.Furthermore,the mechanical responses of the ice under different flight velocities,altitudes,and liquid water contents were investigated.The results show that thermo-mechanical coupling induces significant stress responses in the ice,and the melting phase change further promotes stress evolution.A critical local heating range(with a heating coverage of 90%-95%)is identified.Under this condition,the shear stress exceeds the shear strength over more than 90%of the ice-skin interface,while the minimum principal stress exceeds the compressive strength over more than 99%of the ice near the ice-skin interface.These findings provide numerical support for analyzing the mechanical behavior of ice during aircraft electrothermal de-icing processes.

关键词

飞机除冰/电热除冰/热-力耦合/融冰相变/多物理场耦合/仿真研究

Key words

aircraft de-icing/electrothermal de-icing/thermo-mechanical coupling/ice melting phase change/multiphysics coupling/numerical simulation

分类

航空航天

引用本文复制引用

陈明萱,靳海川,马奎元,宫晗,任仪航,林贵平..基于热力耦合和融冰相变的电热除冰仿真研究[J].航天器环境工程,2026,43(2):111-124,14.

航天器环境工程

1673-1379

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