Jiang Jiawei, Shen Yizhou, Xu Yangjiangshan, Wang Zhen, Tao Jie, Liu Senyun, Liu Weilan, Chen Haifeng
State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing, 210016, China.
key Laboratory of Icing and Anti/De-icing, China Aerodynamics Research and Development Center, 6 Erhuan South Rd., Mianyang, 621000, PR China.
Nat Commun. 2024 Jan 26;15(1):777. doi: 10.1038/s41467-024-45078-5.
Superhydrophobic surfaces demonstrate excellent anti-icing performance under static conditions. However, they show a marked decrease in icing time under real flight conditions. Here we develop an anti-icing strategy using ubiquitous wind field to improve the anti-icing efficiency of superhydrophobic surfaces during flight. We find that the icing mass on hierarchical superhydrophobic surface with a microstructure angle of 30° is at least 40% lower than that on the conventional superhydrophobic plate, which is attributed to the combined effects of microdroplet flow upwelling induced by interfacial airflow and microdroplet ejection driven by superhydrophobic characteristic. Meanwhile, the disordered arrangement of water molecules induced by the specific 30° angle also raises the energy barriers required for nucleation, resulting in an inhibition of the nucleation process. This strategy of microdroplet movement manipulation induced by interfacial airflow is expected to break through the anti-icing limitation of conventional superhydrophobic materials in service conditions and can further reduce the risk of icing on the aircraft surface.
超疏水表面在静态条件下表现出优异的防冰性能。然而,在实际飞行条件下,它们的结冰时间显著缩短。在此,我们开发了一种利用普遍存在的风场的防冰策略,以提高飞行过程中超疏水表面的防冰效率。我们发现,微观结构角度为30°的分级超疏水表面上的结冰质量比传统超疏水板上的至少低40%,这归因于界面气流诱导的微滴流上升和超疏水特性驱动的微滴喷射的综合作用。同时,特定的30°角诱导的水分子无序排列也提高了成核所需的能垒,从而抑制了成核过程。这种由界面气流诱导的微滴运动操纵策略有望突破传统超疏水材料在使用条件下的防冰限制,并可进一步降低飞机表面结冰的风险。