Influence of Passive Pre-Chamber Nozzle Diameter on Jet Ignition in a Constant-Volume Optical Engine under Varying Load and Dilution Conditions

IF 1.1 Q3 TRANSPORTATION SCIENCE & TECHNOLOGY
Dong Eun Lee, Tianxiao Yu, Afaque Alam, Claudia Iyer, Steven Wooldridge, Li Qiao, J. Yi
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Abstract

Despite the growing prominence of electrified vehicles, internal combustion engines remain essential in future transportation. This study delves into passive pre-chamber jet ignition, a leading-edge combustion technology, offering a comprehensive visualization of its operation under varying load and dilution conditions in light-duty GDI engines. Our primary objectives are to gain fundamental insights into passive pre-chamber jet ignition and subsequent main combustion processes and evaluate their response to different load and dilution conditions. We conducted experimental investigations using a light-duty, optical, single-cylinder engine equipped with three passive pre-chamber designs featuring varying nozzle diameters. Optical diagnostic imaging and heat release analysis provided critical insights. Findings reveal that as load decreases, fuel availability and flow conditions deteriorate, leading to delayed and suboptimal jet characteristics impacting main chamber ignition and combustion. Notably, at high and medium loads without dilution, the 1.2 mm-PC (smallest nozzle diameter) excels, exhibiting superior jet ignition and main combustion. This is attributed to earlier jet ejection, improved penetration, and intensified jets, all enabled by the smaller nozzle diameter. Conversely, under low load conditions, the 1.6 mm-PC (largest nozzle diameter) performs better due to enhanced scavenging and reduced pre-chamber residuals, resulting in more balanced pre-chamber combustion and jet characteristics. Furthermore, nozzle diameter significantly influences cycle-to-cycle variations, with smaller diameters enhancing jet ignition but intensifying variability. The impact of external residuals (dilution) on jet ignition performance varies with nozzle diameter, with the 1.6 mm-PC displaying less degradation and demonstrating earlier jet ejection and CA50 timing under higher dilution conditions. In summary, this research underscores the importance of scavenging and residual levels in pre-chamber design, influencing dilution tolerance, and extending possibilities for high-efficiency engines. It contributes essential insights into the behavior of passive pre-chamber jet ignition systems, facilitating their optimization for future internal combustion engines.
被动式预腔喷嘴直径对恒定容积光学发动机在不同负载和稀释条件下喷射点火的影响
尽管电气化汽车日益突出,但内燃机在未来的交通运输中仍然不可或缺。本研究深入探讨了被动式前腔喷射点火这一前沿燃烧技术,对其在轻型 GDI 发动机中不同负荷和稀释条件下的运行情况进行了全面的可视化分析。我们的主要目标是从根本上了解被动式前腔喷射点火和随后的主燃烧过程,并评估它们在不同负荷和稀释条件下的响应。我们使用轻型光学单缸发动机进行了实验研究,该发动机配备了三种不同喷嘴直径的被动式前腔设计。光学诊断成像和热释放分析提供了重要的见解。研究结果表明,随着负荷的降低,燃料的可用性和流动条件会恶化,从而导致喷射特性延迟和不理想,影响主气室的点火和燃烧。值得注意的是,在没有稀释的中高负荷情况下,1.2 毫米 PC(最小喷嘴直径)表现出色,喷射点火和主燃烧性能优越。这要归功于较小的喷嘴直径所带来的更早的射流喷射、更好的穿透力和更强的射流。相反,在低负荷条件下,1.6 毫米 PC(最大喷嘴直径)的性能更好,这是因为它增强了清扫能力,减少了前腔残留物,从而使前腔燃烧和喷射特性更加平衡。此外,喷嘴直径对循环间的变化也有很大影响,直径越小,喷射点火越强,但变化也越大。外部残留物(稀释)对射流点火性能的影响随喷嘴直径的不同而变化,1.6 毫米直径的喷嘴退化较小,在较高的稀释条件下,射流喷射和 CA50 时间更早。总之,这项研究强调了前腔设计中清扫和残留水平的重要性,影响了稀释容限,扩大了高效发动机的可能性。它对被动式前腔喷射点火系统的行为提出了重要见解,有助于优化未来的内燃机。
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
SAE International Journal of Engines
SAE International Journal of Engines TRANSPORTATION SCIENCE & TECHNOLOGY-
CiteScore
2.70
自引率
8.30%
发文量
38
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