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Preload-responsive adhesion: effects of aspect ratio tip shape and alignment

机译:预紧力响应粘附:长宽比尖端形状和对齐方式的影响

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摘要

We tested the adhesive response of polymer surfaces structured with arrays of cylindrical fibrils having diameters of 10–20 µm and aspect ratios 1–2.4. Fibrils had two different tip shapes of end-flaps and round edges. A preload-induced mechanical buckling instability of the fibrils was used to switch between the states of adhesion and non-adhesion. Non-adhesion in fibrils with round edges was reached at preloads that caused fibril buckling, whereas fibrils with end-flaps showed adhesion loss only at very high preloads. The round edge acted as a circumferential flaw prohibiting smooth tip contact recovery leading to an adhesion loss. In situ observations showed that, after reversal of buckling, the end-flaps unfold and re-form contact under prevailing compressive stress, retaining adhesion in spite of buckling. At very high preloads, however, end-flaps are unable to re-form contact resulting in adhesion loss. Additionally, the end-flaps showed varying contact adaptability as a function of the fibril–probe alignment, which further affects the preload for adhesion loss. The combined influence of preload, tip shape and alignment on adhesion can be used to switch adhesion in bioinspired fibrillar arrays.
机译:我们测试了由直径为10–20 µm,纵横比为1–2.4的圆柱状原纤维阵列构成的聚合物表面的粘合响应。原纤维具有两个不同的尖端形状,包括末端襟翼和圆形边缘。预加载引起的原纤维的机械屈曲不稳定性用于在粘附状态和非粘附状态之间切换。在预载荷下会导致具有圆形边缘的原纤维发生非粘附,这会导致原纤维屈曲,而带有末端襟翼的原纤维则仅在非常高的预载荷下才会显示出粘附力下降。圆形边缘起圆周缺陷的作用,阻止平滑的尖端接触恢复,从而导致粘附力损失。原位观察表明,在屈曲发生逆转之后,在主要的压缩应力作用下,尾翼展开并重新形成接触,尽管发生了屈曲,但仍保持了附着力。但是,在非常高的预紧力下,尾翼无法重新形成接触,从而导致粘附力下降。此外,端襟翼显示出不同的接触适应性,这取决于原纤维-探针排列的函数,这进一步影响了附着力损失的预紧力。预紧力,尖端形状和对齐方式对粘连的综合影响可用于切换生物启发性原纤维阵列中的粘连。

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