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受火箭启发的管状催化微射流,其壁面具有格栅结构,作为导向尾翼。

Rocket-inspired tubular catalytic microjets with grating-structured walls as guiding empennages.

机构信息

Department of Materials Science, State Key Lab of ASIC and System, Fudan University, Shanghai 200433, P. R. China.

出版信息

Nanoscale. 2017 Dec 7;9(47):18590-18596. doi: 10.1039/c7nr07006c.

Abstract

Controllable locomotion in the micro-/nanoscale is challenging and attracts increasing research interest. Tubular microjets self-propelled by microbubbles are intensively investigated due to their high energy conversion efficiency, but the imperfection of the tubular geometry makes it harder to realize linear motion. Inspired by the macro rocket, we designed a tubular microjet with a grating-structured wall which mimics the guiding empennage of the macro rocket, and we found that the fluid can be effectively guided by the grooves. Both theoretical simulation and experimental work have been carried out, and the obtained results demonstrate that the stability margin of the grating-structured microjet can be enhanced. Compared with microjets with smooth walls, the structured microjets show an enhanced ability of moving linearly. In 10% HO, only 20% of the smooth microjets demonstrate linear trajectories, while 80% of the grating-structured microjets keep moving straight. The grating-structured microjet can maintain linear motion under external disturbance. We further propose to increase the stability by introducing a helical grating structure.

摘要

在微观/纳米尺度上进行可控运动具有挑战性,引起了越来越多的研究兴趣。由于微气泡自推进管状微射流具有较高的能量转换效率,因此受到了广泛的研究,但管状结构的不完美使得实现直线运动更加困难。受宏观火箭的启发,我们设计了一种带有光栅结构壁的管状微射流,该结构壁模仿了宏观火箭的制导尾翼,我们发现流体可以通过凹槽被有效地引导。我们进行了理论模拟和实验工作,结果表明,光栅结构微射流的稳定性裕度可以得到增强。与光滑壁微射流相比,结构化微射流具有更强的直线运动能力。在 10%HO 中,只有 20%的光滑微射流呈现直线轨迹,而 80%的光栅结构微射流保持直线运动。光栅结构微射流可以在外部干扰下保持直线运动。我们进一步提出通过引入螺旋光栅结构来提高稳定性。

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