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首页|期刊导航|南京航空航天大学学报(英文版)|过冷大水滴撞击复材表面结冰特性及防冰研究

过冷大水滴撞击复材表面结冰特性及防冰研究

李小飞 王祥昭 吉泽民 黄小彬 刘洪

南京航空航天大学学报(英文版)2025,Vol.42Issue(2):178-190,13.
南京航空航天大学学报(英文版)2025,Vol.42Issue(2):178-190,13.DOI:10.16356/j.1005-1120.2025.02.003

过冷大水滴撞击复材表面结冰特性及防冰研究

Icing Characteristics and Anti-icing Research of Supercooled Large Droplet Impact on Epoxy Composite Surfaces

李小飞 1王祥昭 2吉泽民 2黄小彬 2刘洪2

作者信息

  • 1. 上海交通大学航空航天学院,上海 200240,中国||中国航空研究院,北京 100012,中国
  • 2. 上海交通大学航空航天学院,上海 200240,中国
  • 折叠

摘要

Abstract

The icing characteristics of supercooled large droplet(SLD)impacting carbon fiber-reinforced composites(CFRCs)remain poorly understood,hindering the enhancement of ice protection capabilities and the certification of ice-accreted composite aircraft.The paper systematically investigates the effects of the supercooling degree,the surface temperature,and the impact velocity on the ice accretion behavior of SLDs impacting carbon fiber-reinforced epoxy composite surfaces.To address the ice-prone nature of CFRCs,nanoparticle-modified anti-icing coatings are developed,and the icing characteristics of SLD-impacted modified carbon fiber-reinforced epoxy composite surfaces are analyzed.Results demonstrate that surface-modified carbon fiber-reinforced epoxy composite exhibits significantly delayed ice formation.Under conditions of droplet temperature(-15℃)and surface temperature(-18℃),the icing time of hydrophobic-modified CFRCs was delayed by over 1 100 ms,representing a 5.4-fold improvement compared to the unmodified carbon fiber-reinforced epoxy composite.

关键词

飞机结冰/碳纤维增强环氧树脂复合材料/过冷大水滴/疏水改性/结冰防护

Key words

aircraft icing/carbon fiber-reinforced epoxy composites/supercooled large droplets/hydrophobic modification/icing protection

引用本文复制引用

李小飞,王祥昭,吉泽民,黄小彬,刘洪..过冷大水滴撞击复材表面结冰特性及防冰研究[J].南京航空航天大学学报(英文版),2025,42(2):178-190,13.

基金项目

This work was supported by the Na-tional Key Laboratory of Advanced Composite Materials(No.KZ42191814). (No.KZ42191814)

南京航空航天大学学报(英文版)

1005-1120

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