An Experimental Study on the Durability of Icephobic Slippery Liquid-Infused Porous Surfaces (SLIPS) Pertinent to Aircraft Anti-/De-Icing

Liqun Ma, Zichen Zhang, Yang Liu, Hui Hu
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引用次数: 3

Abstract

Recently, bio-inspired surfaces have been found to be hydrophobic and/or icephobic, which has very low adhesion force for water and/or ice. When bio-inspired surfaces are applied for aircraft icing mitigation, they would suffer erosions due to high-speed impacting of the water droplets in the form of fog/mist. However, the knowledge of the coating durability regarding spray erosion is still quite limited. In the present study, an experimentally investigation was conducted to evaluate the durability of a PTFE membrane based slippery liquid infused porous surface (SLIPS) subject to water spray erosion, in comparison to that of a commonly used superhydrophobic surface (SHS) coating (i.e., a commercially-available Hydrobead® SHS coating). A wind driven spray generator was established with the spray erosion speed controllable from 45 m/s to 95 m/s. The anti-icing performance of the SHS and the SLIPS was validated in an icing research wind tunnel. Impact dynamics of individual water droplets at high Weber number about 3,000 and water spray erosion process of the SHS and the SLIPS were compared. The wettability-based coating lifetime was analyzed by measuring the dynamic contact angles on the SHS and the SLIPS under water spray erosions with different velocities. A cumulative-fatigue-damage theory was used to help predict the coating life time for in-flight aircraft icing mitigation. It turns out that the SLIPS could maintain its hydrophobicity better than the SHS under a moderate spray erosion speed. The mechanism of the spray erosion process for the SHS and the SLIPS was also examined in this study.
飞机防/除冰用疏冰湿性液体注入多孔表面耐久性实验研究
最近,人们发现仿生表面是疏水和/或疏冰的,对水和/或冰的附着力非常低。当仿生表面应用于飞机结冰减缓时,由于雾/薄雾形式的水滴的高速冲击,它们会受到侵蚀。然而,关于涂层耐久性的喷涂侵蚀的知识仍然相当有限。在本研究中,我们进行了一项实验研究,以评估基于PTFE膜的光滑液体注入多孔表面(SLIPS)在水雾侵蚀下的耐久性,并与常用的超疏水表面(SHS)涂层(即市售的Hydrobead®SHS涂层)进行了比较。建立了风力喷雾发生器,喷雾侵蚀速度在45 ~ 95 m/s范围内可控。在结冰研究风洞中验证了SHS和SLIPS的防冰性能。比较了高韦伯数(约3000)下单个水滴的冲击动力学以及SHS和slip的水雾侵蚀过程。通过测量SHS和slip在不同速度下的动态接触角,分析了润湿性涂层的寿命。利用累积疲劳损伤理论对飞机减冰涂层寿命进行预测。结果表明,在中等喷蚀速度下,滑移体的疏水性比滑移体的要好。本文还探讨了喷雾侵蚀过程对SHS和slip的影响机理。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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