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超疏水/电热协同防/除冰策略在冰风洞中的实验研究

王敬鑫 于大川 杨再利 郭镕颖 朱春玲

南京航空航天大学学报(英文版)2023,Vol.40Issue(2):193-204,12.
南京航空航天大学学报(英文版)2023,Vol.40Issue(2):193-204,12.

超疏水/电热协同防/除冰策略在冰风洞中的实验研究

Experimental Investigation of Super-hydrophobic/Electro-thermal Synergistically Anti-icing/De-icing Strategy in Ice Wind Tunnel

王敬鑫 1于大川 1杨再利 1郭镕颖 1朱春玲2

作者信息

  • 1. 南京航空航天大学航空学院,南京 210016,中国
  • 2. 南京航空航天大学航空学院,南京 210016,中国||南京航空航天大学机械结构力学及控制国家重点实验室,南京 210016,中国
  • 折叠

摘要

Abstract

The icing of unmanned aerial vehicles(UAVs)poses a serious threat to flight safety.The available energy of UAVs is inadequate,so an energy-efficient ice protection strategy is required.In this paper,an integral fiberglass composite airfoil is tested,which has super-hydrophobic coating and embedded electro-thermal film(SHS-EET).The proportional integral derivative method(PID)is used to adjust surface temperature and heating power.Experiments are conducted in an icing wind tunnel to verify the anti-icing/de-icing performance of the strategy.The results show that the super-hydrophobic coating without a heating source fails to avoid the formation of accreted ice.In addition,the ice shedding period of SHS-EET is reduced by 64.6%and the energy consumption is reduced by 72.3%.As the surface temperature is lower than 10℃,SHS-EET achieves dry anti-icing.And it reduces energy consumption by 27.5%compared with the wet anti-icing strategy of a fiberglass airfoil with underground electro-thermal film(FG-UET).The hybrid anti-icing/de-icing strategy is beneficial for the development of the icing protection system for UAVs.

关键词

超疏水涂层/电热膜/一体化结构/结冰风洞/玻璃纤维复合材料

Key words

super-hydrophobic coating/electro-thermal film/integral structure/ice wind tunnel/fiberglass composite

分类

航空航天

引用本文复制引用

王敬鑫,于大川,杨再利,郭镕颖,朱春玲..超疏水/电热协同防/除冰策略在冰风洞中的实验研究[J].南京航空航天大学学报(英文版),2023,40(2):193-204,12.

基金项目

This work was financially supported by the National Natural Science Foundation of China(Nos.11832012,12227802). (Nos.11832012,12227802)

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

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