INM-Leibniz Institute for New Materials, Functional Surfaces Group, Saarland University, Saarbruecken, Germany.
J R Soc Interface. 2013 Apr 3;10(83):20130171. doi: 10.1098/rsif.2013.0171. Print 2013 Jun 6.
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.
我们测试了具有 10-20μm 直径和 1-2.4 纵横比的圆柱形纤维阵列结构的聚合物表面的粘附响应。纤维具有两种不同的尖端形状,即端翼和圆形边缘。通过纤维的预载诱导机械屈曲不稳定性,可以在粘附和非粘附状态之间切换。在导致纤维屈曲的预载下,圆形边缘的纤维达到非粘附状态,而端翼纤维仅在非常高的预载下才表现出粘附损失。圆形边缘作为一个周向缺陷,阻止了平滑尖端接触的恢复,导致粘附损失。原位观察表明,在屈曲反转后,端翼展开并在现有压缩应力下重新形成接触,尽管发生了屈曲,但仍保持粘附。然而,在非常高的预载下,端翼无法重新形成接触,导致粘附损失。此外,端翼的接触适应性随纤维-探针的对准而变化,这进一步影响了粘附损失的预载。预载、尖端形状和对准对粘附的综合影响可用于在仿生纤维阵列中切换粘附。