使用CONVERGE 3.0对PFI SI发动机中氢燃料和传统燃料的性能和排放进行分析

Rashedul Islam , S.M. Asiqur Rahman , Md. Rajin Islam , Md. Rakibul Islam , Md. Rasel Ahmed , Md. Rabiul Islam Sarker
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摘要

传统燃料,如用于火花点火(SI)发动机的汽油和甲烷,越来越受到化石燃料储量有限性的限制。燃烧效率低下与发动机效率降低有关,因为不完全燃烧会增加有害污染物(包括CO2和CO)的排放,同时也会对燃油经济性产生负面影响。本研究的目的是在考虑不同等效比和运行速度的情况下,对选定的传统燃料和氢燃料的发动机性能和排放进行比较研究。为了实现这一目标,使用CONVERGE 3.0仿真软件进行了广泛的三维数值模拟,以模拟端口燃料SI引擎,SI8引擎预混SAGE模型促进了模拟。本研究评估的性能指标包括气缸压力、比热比、热效率、平均温度。在NOx、CO、CO2和HC排放的情况下,分析了排放特性。在不同发动机转速(2000、2500和3000 rpm)下,通过改变氢气当量比(0.4、0.6和0.9),获得了仿真结果。发动机设置,网格创建,边界条件,湍流,燃烧和物种运输模型被精心概述,以确保准确的模拟结果。当当量比为0.4,发动机转速为3000 rpm时,氢燃料在所有测试条件中表现出最佳的综合性能。热效率最高,达到40.94%,气缸压力和比热比最佳,平均温度较好,燃油消耗最低。此外,这种配置导致二氧化碳和碳氢化合物的零排放,同时由于燃料结构中没有碳,二氧化碳排放量显著减少。然而,由于与氢相关的高温燃烧,氮氧化物排放仍然存在,需要进一步的缓解策略。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Performance and Emission Analysis of Hydrogen and Conventional Fuels in PFI SI Engines Using CONVERGE 3.0
The availability of conventional fuels, such as gasoline and methane, which are used in spark-ignition (SI) engines, is increasingly limited by the finite nature of fossil fuel reserves. The inefficiencies in combustion are associated with reduced engine effectiveness, as incomplete combustion heightens the emissions of harmful pollutants, including CO2 and CO, while also negatively impacting fuel economy. The objective of this research is to undertake a comparative study of engine performance and emissions for a selection of conventional fuels and hydrogen, while considering varying equivalence ratios and operational speeds. To accomplish this, an extensive 3-dimensional numerical simulation was carried out using CONVERGE 3.0 simulation software to model a port-fueled SI engine, with the SI8 Engine Premix SAGE model facilitating the simulations. The performance metrics assessed in this research include cylinder pressure, specific heat ratio, heat rate, thermal efficiency, and mean temperature. The emission characteristics are analyzed in cases of NOx, CO, CO2, and HC emissions. The simulation results are obtained by varying the equivalence ratios of hydrogen (0.4, 0.6, and 0.9) at different engine speeds (2000, 2500, and 3000 rpm). The engine setup, mesh creation, boundary conditions, turbulence, combustion, and species transport models were meticulously outlined to ensure accurate simulation results. Hydrogen fuel, when operated at an equivalence ratio of 0.4 and an engine speed of 3000 rpm, showcases the best overall performance among all tested conditions. It achieves the highest thermal efficiency of 40.94%, optimal cylinder pressure and specific heat ratio, a favorable mean temperature, and the lowest fuel consumption. Additionally, this configuration results in zero emissions of CO and HC, along with a significant reduction in CO2 emissions due to the absence of carbon in the fuel structure. However, due to the high combustion temperatures associated with hydrogen, NOx emissions remained present and require further mitigation strategies.
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