首页> 外文会议>ASME Internal Combustion Engine Division technical conference >SPRAY-WALL INTERACTIONS IN A SMALL-BORE, MULTI-CYLINDER ENGINE OPERATING WITH REACTIVITY-CONTROLLED COMPRESSION IGNITION
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SPRAY-WALL INTERACTIONS IN A SMALL-BORE, MULTI-CYLINDER ENGINE OPERATING WITH REACTIVITY-CONTROLLED COMPRESSION IGNITION

机译:小孔,多缸发动机中反应性受压点火的喷壁相互作用

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Experimental work on reactivity-controlled compression ignition (RCCI) in a small-bore, multi-cylinder engine operating on premixed iso-octane and direct-injected n-heptane has shown an unexpected combustion phasing advance at early injection timings, which has not been observed in large-bore engines operating under RCCI at similar conditions. In this work, computational fluid dynamics (CFD) simulations were performed to investigate whether spray-wall interactions could be responsible for this result. Comparison of the spray penetration, fuel film mass, and in-cylinder visualization of the spray from the CFD results to the experimentally measured combustion phasing and emissions provided compelling evidence of strong fuel impingement at injection timings earlier than -90 crank angle degrees (°CA) after top dead center (aTDC), and transition from partial to full impingement between -65 and -90°CA aTDC. Based on this evidence, explanations for the combustion phasing advance at early injection timings are proposed along with potential verification experiments.
机译:在使用预混合异辛烷和直喷正庚烷的小口径多缸发动机中进行反应性控制的压缩点火(RCCI)的实验工作表明,在早期喷射正时出现了意外的燃烧定相进展,但尚未实现在类似条件下在RCCI下运行的大口径发动机中观察到。在这项工作中,进行了计算流体动力学(CFD)模拟,以调查是否喷水壁相互作用可能是造成这一结果的原因。比较CFD结果中的喷雾渗透率,燃油膜质量和喷雾在缸内的可视化效果,以及通过实验测量的燃烧定相和排放,提供了令人信服的证据,证明了在-90曲柄角度(°CA)之前的喷射正时强烈的燃油撞击)在上止点(aTDC)之后,并在-65至-90°CA aTDC之间从部分撞击过渡到完全撞击。基于这些证据,提出了在早期喷射正时提前进行燃烧定相的解释,并提出了可能的验证实验。

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