A nozzle design for mitigating particle slowing in the bow shock region during micro-cold spray of 8 YSZ films

IF 3.9 3区 环境科学与生态学 Q2 ENGINEERING, CHEMICAL Journal of Aerosol Science Pub Date : 2024-03-19 DOI:10.1016/j.jaerosci.2024.106360
Stephen G. Bierschenk , Desiderio Kovar
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Abstract

During micro-cold spray deposition, also referred to as the aerosol deposition method or vacuum kinetic spraying, performed with conventional nozzles, the particle impact velocities decrease drastically with particle size for fine particles <500 nm in diameter due to slowing in the stagnation region. A new design for a nozzle that contains pressure relief channels is proposed that allows the pressure in the stagnation region downstream of the bow shock to be reduced. This reduced stagnation pressure results in less particle slowing compared to conventional nozzle geometries, particularly for smaller or less dense particles. The effects of the channel geometry on the particle impact velocity are systematically investigated by independently varying the channel parameters. Calculations show that the impact velocities for 100 and 200 nm yttria stabilized zirconia particles is increased by 111% and 31%, respectively, for a selected pressure relief channel nozzle when compared to a comparable conventional nozzle. Although impact velocities are increased, a tradeoff exists with this nozzle design in that the particle focusing in the nozzle is decreased and some of the particles may be removed from the aerosol by the channels. Experiments using a nitrogen as a carrier gas at ∼40 kPa upstream pressure show that, despite the loss of larger particles into the relief channels, the deposition efficiency is improved by 300% when depositing films from fine 8 YSZ powder with the pressure relief nozzle compared to a conventional nozzle.

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在 8 YSZ 薄膜的微冷喷雾过程中减缓弓形冲击区颗粒减速的喷嘴设计
在使用传统喷嘴进行微冷喷雾沉积(也称为气溶胶沉积法或真空动力学喷雾)时,对于直径小于 500 nm 的细颗粒,由于停滞区的速度减慢,颗粒撞击速度随颗粒大小的变化而急剧下降。我们提出了一种包含泄压通道的新型喷嘴设计,可降低弓形冲击下游停滞区的压力。与传统的喷嘴几何形状相比,停滞压力的降低可减少颗粒减速,特别是对于较小或密度较低的颗粒。通过独立改变通道参数,系统地研究了通道几何形状对颗粒撞击速度的影响。计算结果表明,与同类传统喷嘴相比,选定的泄压通道喷嘴对 100 纳米和 200 纳米钇稳定氧化锆颗粒的冲击速度分别提高了 111% 和 31%。虽然冲击速度提高了,但这种喷嘴设计存在一个折衷问题,即沉积物的横向尺寸增大,部分颗粒可能会被通道从气溶胶中去除。使用氮气作为载气,上游压力为 40 kPa 的实验表明,尽管较大的颗粒会流失到泄压通道中,但与传统喷嘴相比,使用泄压喷嘴从细 8 YSZ 粉末中沉积薄膜时,沉积效率提高了 300%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Journal of Aerosol Science
Journal of Aerosol Science 环境科学-工程:化工
CiteScore
8.80
自引率
8.90%
发文量
127
审稿时长
35 days
期刊介绍: Founded in 1970, the Journal of Aerosol Science considers itself the prime vehicle for the publication of original work as well as reviews related to fundamental and applied aerosol research, as well as aerosol instrumentation. Its content is directed at scientists working in engineering disciplines, as well as physics, chemistry, and environmental sciences. The editors welcome submissions of papers describing recent experimental, numerical, and theoretical research related to the following topics: 1. Fundamental Aerosol Science. 2. Applied Aerosol Science. 3. Instrumentation & Measurement Methods.
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