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大尺寸槽型铝表面的冰剪切黏附。

Shear Adhesion of Ice on Large-Sized Grooved Aluminum Surfaces.

机构信息

Department of Mechanical Science and Engineering, Sichuan University, Chengdu 610065, China.

Yibin Institute of Industrial Technology, Sichuan University (Yibin Park), Yibin 644000, China.

出版信息

Langmuir. 2023 Jul 4;39(26):9100-9110. doi: 10.1021/acs.langmuir.3c00833. Epub 2023 Jun 22.

Abstract

Ice adhesion is important when designing aircraft anti-icing/de-icing systems. Major and minor grooves are common in the skin of aircraft. However, the effects of millimeter-scale grooves on ice adhesive strength have not been given due attention. Specimens with varying depths, widths, and numbers of grooves were fabricated by machining to investigate the ice adhesive characteristics of large-sized grooved aluminum surfaces. After the ice cube was frozen on the surface using a silicon mold, the adhesive force was measured using a self-assembled shear adhesive force setup. A correlation between groove size and apparent adhesive strength in the perpendicular loading direction was established based on the experimental results. Every 1% increase in the groove width ratio was associated with an 18.7 kPa increase in apparent adhesive strength. The increasing speed of the adhesion rapidly decayed as the groove depth increased. The increase in adhesion reached 99% of the maximum increase when the groove depth reached 0.8 times the width. The number of grooves had little effect on the adhesion when the total width of the grooves was kept constant. Stress distribution analysis was conducted using the finite element method, and the results were in accordance with the cracking phenomena in the experiments. The adhesive strength in the parallel loading direction was 30% lower than that in the perpendicular loading direction for all six chosen surfaces. This study is the first to propose a quantitative relationship between the surface textures of millimeter-sized grooves and ice adhesive strength. The loading orientation also had a substantial influence on adhesion. The results will serve as a valuable reference for future studies on ice adhesion on textured surfaces and for improving the performance of anti-icing/de-icing systems.

摘要

在设计飞机防冰/除冰系统时,冰附着很重要。飞机蒙皮上通常有大凹槽和小凹槽。然而,毫米级凹槽对冰附着强度的影响尚未得到充分关注。通过机械加工制造了具有不同深度、宽度和凹槽数量的试样,以研究大尺寸有槽铝表面的冰附着特性。使用硅模具将冰块冷冻在表面上后,使用自组装剪切附着力装置测量附着力。根据实验结果,建立了凹槽尺寸与垂直加载方向表观附着强度之间的相关性。凹槽宽度比每增加 1%,表观附着强度就会增加 18.7 kPa。随着凹槽深度的增加,附着速度迅速衰减。当凹槽深度达到宽度的 0.8 倍时,附着的增加达到最大增加的 99%。当保持凹槽总宽度不变时,凹槽数量对附着的影响很小。使用有限元法进行了应力分布分析,结果与实验中的开裂现象一致。对于所有六个选择的表面,平行加载方向的附着强度比垂直加载方向低 30%。本研究首次提出了毫米级凹槽表面纹理与冰附着强度之间的定量关系。加载方向对附着也有很大影响。研究结果将为未来关于纹理表面冰附着的研究和改进防冰/除冰系统的性能提供有价值的参考。

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