Investigation of fuel temperature and injection timing effects on ammonia direct injection in an optical engine

IF 5 Q2 ENERGY & FUELS
Valentin Scharl , Karl Oskar Pires Bjørgen , David Robert Emberson , Terese Løvås
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Abstract

This work investigates the effects of fuel temperature and injection timing on ammonia direct injection in an optical engine using a multi-hole injector. Flash-boiling may occur over various engine-relevant conditions due to ammonia’s high vapor pressure. This phenomenon impacts spray characteristics and, in severe cases, facilitates cavitation inside the nozzle. Both fuel temperature and injection timing (i.e., ambient conditions during injection) impact the intensity of flash-boiling during fuel injection. Therefore, this work varies fuel temperature (from 320K to 388K) and injection timing (from 60CADaTDC (crank angle degrees after top dead center) to 6CADaTDC) to assess their impact on injection mass flux, discharge coefficients, and macroscopic spray characteristics using an ammonia injection pressure of 200bar. For this purpose, the injection mass is measured by analyzing exhaust gas compositions during engine operation with ammonia injections but without combustion. In addition, diffuse background illumination (DBI) images capture the liquid phase of the fuel spray to characterize spray behavior. The findings reveal that increasing fuel temperature decreases ammonia’s injection mass by up to 12.8% but has little impact on discharge coefficients for late injection timings and high in-cylinder pressures. However, discharge coefficients decrease by up to 17.4% (from 0.58 to 0.48) for early injection timings if fuel temperatures are high. The individual sprays of the 6-hole GDI injector may collapse into a uniform spray at high-density conditions without flash-boiling or under strongly flash-boiling conditions. The findings clarify the impact of ammonia’s high vapor pressure on injection mass and prove the relevance of different spray collapse mechanisms in ammonia direct injection engines.
研究燃料温度和喷射正时对光学发动机中氨直接喷射的影响
这项研究探讨了在使用多孔喷射器的光学发动机中,燃料温度和喷射正时对氨直接喷射的影响。由于氨的蒸汽压较高,在各种发动机相关条件下都可能出现闪沸现象。这种现象会影响喷雾特性,严重时还会导致喷嘴内部气蚀。燃料温度和喷射时间(即喷射过程中的环境条件)都会影响燃料喷射过程中的闪沸强度。因此,本研究改变了燃料温度(从 320K 到 388K)和喷射时间(从 -60CADaTDC(顶死中心后的曲柄角度)到 -6CADaTDC),以评估它们对喷射质量通量、放电系数和氨喷射压力为 200bar 的宏观喷雾特性的影响。为此,在有氨喷射但没有燃烧的发动机运行期间,通过分析废气成分来测量喷射质量。此外,漫反射背景照明(DBI)图像捕捉了燃料喷雾的液相,以确定喷雾行为的特征。研究结果表明,在喷射时间较晚和缸内压力较高的情况下,提高燃料温度会使氨的喷射质量降低达 12.8%,但对排出系数的影响很小。然而,如果燃料温度较高,在较早喷射时间段,排放系数最多会降低 17.4%(从 0.58 降至 0.48)。在高密度条件下,6 孔 GDI 喷射器的单个喷雾可能会在没有闪沸或强烈闪沸的条件下溃散成均匀的喷雾。研究结果阐明了氨的高蒸汽压对喷射质量的影响,并证明了氨直喷发动机中不同喷雾溃缩机制的相关性。
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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CiteScore
4.20
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