南京航空航天大学学报（英文版）2023，Vol.40Issue(z1)：96-104,9.DOI:10.16356/j.1005-1120.2023.S1.009
新型电热结构防除冰性能研究
Investigation on Anti/De-icing Performance of an Innovative Electrothermal Structure
摘要
Abstract
Innovative development of an anti-and de-icing system which can be practically used for aircraft wings is an ongoing challenge.High energy-consumption of electrothermal anti-icing/de-icing in aircraft is a tough problem up to date.In this work,we design an anti/de-icing structure based on the electric heating.The electrothermal structure is composed of the polydimethylsiloxane(PDMS)insulation coating,conductive layer,electrothermal layer and porous insulation layer from the top to the bottom.The effect of the thickness of the conductive silver paste layer and the content of the conductive liquid on the temperature of the insulation layer and the insulation layer under different power levels is investigated.The results indicate that at room temperature,when the input power is 4 W and the thickness of the silver slurry layer is 300 μm,the maximum temperature of the insulation layer can reach 134℃.Moreover,when the input power is 18 W,the top temperature can quickly reach 0℃,while the bottom temperature remains around-12.5℃at-20℃,resulting in less energy loss.Our study can provide theoretical guidance for the design of electric heating anti-icing material systems.关键词
防冰/电热结构/聚二甲基硅氧烷/传热/能量利用Key words
anti/de-icing/electrothermal structure/polydimethylsiloxane/heat transfer/energy utilization分类
航空航天引用本文复制引用
谷建臻,齐慧敏,余家欣,张亚锋,顾兴士..新型电热结构防除冰性能研究[J].南京航空航天大学学报（英文版）,2023,40(z1):96-104,9.基金项目
This work was funded by the National Natural Science Foundations of China(No.52105214),Si-chuan Science and Technology Program(No.2022NSF-SC1928),and the Key Laboratory of Icing and Anti/De-ic-ing of CARDC(Nos.IADL 20210403,IADL20210103). （No.52105214）
