OpenFOAM 模拟开发气溶胶喷射印刷中的雾流分流器

James Q Feng
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引用次数: 0

摘要

要设计出符合气溶胶喷射®(AJ)印刷性能要求的功能装置,通过准直冲击雾状射流将油墨沉积在基材上,了解内部雾流行为非常重要。本文使用 OpenFOAM 软件包建立了一个计算流体动力学 (CFD) 模型,用于开发 AJ 印刷设备中的雾流分流器。这种雾流分流器的功能是将具有特定流速的雾流引导至沉积喷嘴,以便将油墨材料印刷到基材上,并在喷嘴移动到不希望油墨沉积的基材位置时将雾流分流。CFD 结果可以揭示雾流切换过程中的详细雾流行为,以便定量分析雾流前沿通过不同区域的时间。结果表明,这种内部气动分流器不可避免地会带来明显的导通延迟和关断延迟,由于雾滴从雾流切换室到基底所需的时间较长,因此对于雾流速率较低的精细特征印刷而言,导通延迟和关断延迟尤为明显。此外,开延时和关延时还会对印刷特征产生逐渐淡入和淡出的效果,尤其是当基底以相当快的速度移动时。这里介绍的只是将 CFD 分析应用于商用真空增压分流器性能检测的一个例子,不过由于 CFD 域几何和网格调整的便利性,已建立的计算模型还被用于指导设备设计,评估不同几何形状和尺寸的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
OpenFOAM simulations for development of a mist flow diverter in aerosol jet printing
To design functional devices meeting the performance requirements for Aerosol Jet® (AJ) printing to deposit ink on substrate by a collimated impinging mist jet, understanding the internal mist flow behaviour is important. Herewith a computational fluid dynamics (CFD) model is presented with an OpenFOAM software package, for development of a mist flow diverter in the AJ printing equipment. The function of such a mist flow diverter is to direct a mist flow with specified flow rate to the deposition nozzle for printing the ink material onto substrate and to divert the mist flow away when the nozzle moves over a substrate location where ink deposition is unwanted. The CFD results can reveal detailed mist flow behaviour during mist flow switching for quantitative analysis of mist front travelling time through different regions. It is shown that such an internal pneumatic diverter inevitably brings noticeable on-delay and off-delay, more so for finer feature printing with lower mist flow rate due to time needed for mist droplets to travel from the mist flow switching chamber to substrate. Moreover, the on-delay and off-delay also come with gradual fade-in and fade-out effects in printed features especially when the substrate is moving at a considerable speed. Presented here is but one example of CFD analysis applied to performance examination of a commercial vacuum-boost diverter, although the established computational model has also been utilized to guide equipment design with evaluations of the effects of different geometric shapes and sizes by virtue of the convenience for CFD domain geometry and mesh adjustments.
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