Optical study of active narrow throat pre-chamber assisted internal combustion engine at lean limit

IF 5 Q2 ENERGY & FUELS
Priybrat Sharma , Qinglong Tang , Ramgopal Sampath , Ponnya Hlaing , Manuel Echeverri Marquez , Emre Cenker , Gaetano Magnotti
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Abstract

The pre-chamber assisted ignition offers several much-needed upgrades to gas engines, ranging from improved combustion efficiency and stability to extended lean limits. The concept has received intermittent attention from researchers over the past century, and the concept's fundamental understanding remains segmented. This study investigates pre-chamber assisted combustion (PCC) in a heavy-duty gas engine fueled by methane at the lean limits. The engine is operated at two lean limits at intake pressures of 1.2 and 1.4 bar. At lower intake pressure, global excess air ratio (λglobal) is 2.4, while at higher intake pressure λglobal is 2.6. The comparison of two lean limits through experimental data and GT-Power 1D model reveals the underlying ignition and combustion. Using a combination of acetone PLIF (N-PLIF) and OH* chemiluminescence imaging allows visualization of both the reacting and non-reacting part of the pre-chamber jet. The results suggest that pressure differential across the pre-chamber and main chamber controls the reacting jet growth speed. The combustion chamber boundaries affect the main combustion through the wall jet part of the impinging pre-chamber jets as higher OH* concentrations are observable at stagnation points of the jet. In addition, the study reports the appearance of post-combustion jets and dispersed OH* pockets as the combustion dwindles. The narrow throat pre-chamber shows a spectral pressure signature reminiscent of the Helmholtz oscillator, and circumferential resonant modes dominate the main chamber combustion. Although the PCC offers great ignitibility, the main chamber mixture cannot sustain prolonged combustion at a lean limit lambda value.

主动窄喉预腔辅助内燃机在精益极限下的光学研究
预燃室辅助点火为燃气发动机提供了几项急需的升级,从提高燃烧效率和稳定性到延长稀燃极限。在过去的一个世纪里,这一概念不时受到研究人员的关注,对这一概念的基本理解仍然是分段的。本研究调查了以甲烷为燃料的重型燃气发动机在贫燃极限下的预燃室辅助燃烧(PCC)。发动机在进气压力为1.2巴和1.4巴的两个稀薄极限下运行。在进气压力较低时,整体过量空气比(λglobal)为2.4,而在进气压力较高时,λglobal为2.6。通过实验数据和GT Power 1D模型对两个贫限值的比较揭示了潜在的点火和燃烧。使用丙酮-PLIF(N-PLIF)和OH*化学发光成像的组合允许前室射流的反应和非反应部分的可视化。结果表明,预燃室和主燃室之间的压差控制着反应射流的生长速度。燃烧室边界通过撞击预燃室射流的壁射流部分影响主燃烧,因为在射流的驻点处可以观察到更高的OH*浓度。此外,该研究报告了随着燃烧的减少,燃烧后射流和分散的OH*袋的出现。窄喉预燃室显示出让人想起亥姆霍兹振荡器的光谱压力特征,周向共振模式主导了主燃烧室的燃烧。尽管PCC具有很高的可燃性,但主燃烧室混合物不能在贫极限λ值下维持长时间燃烧。
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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