首页> 外文会议>AIAA atmospheric and space environments conference;AIAA aviation forum >An Experimental Study on the Durability of Icephobic Slippery Liquid-Infused Porous Surfaces (SLIPS) Pertinent to Aircraft Anti-/De-Icing
【24h】

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

机译:冰冻滑湿液体注入多孔表面(SLIPS)耐用性与飞机抗/去冰的实验研究

获取原文

摘要

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.
机译:最近,已发现生物启发的表面是疏水性和/或冰冻的,其具有非常低的水和/或冰的粘附力。当生物启发的表面适用于飞机结冰缓解时,由于雾/雾形式的水滴的高速冲击,它们会遭受侵蚀。然而,关于喷雾腐蚀的涂层耐久性的知识仍然非常有限。在本研究中,与常用的超疏水表面(SHS)涂层相比,进行了实验研究以评估受水喷雾腐蚀的PTFE膜的滑湿液体注入多孔表面(滑动)的耐久性(即,市售的氢垫圈夹具涂层)。建立风力驱动的喷雾发生器,其喷雾腐蚀速度可控在45米/秒至95米/米。 SHS和SLIPS的防冰性能验证在冰林研究风洞中。比较了大约3,000个高韦伯号的各个水滴的冲击动态及SHS和SLIPS的喷雾腐蚀过程。通过测量SHS上的动态接触角和具有不同速度的水喷雾糜烂下的动态接触角度来分析润湿性的涂层寿命。累积疲劳损坏理论用于帮助预测飞行飞行飞机结冰缓解的涂层寿命。事实证明,在适度的喷雾腐蚀速度下,滑块可以比SHS更好地保持其疏水性。在本研究中还研究了SHS和SHIPS的喷雾腐蚀过程的机制。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号