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Modeling the Pilot Injection and the Ignition Process of a Dual Fuel Injector with Experimental Data from a Combustion Chamber Using Detailed Reaction Kinetics

机译:使用详细的反应动力学从燃烧室实验数据模拟双燃料喷射器的点火过程和点火过程

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The introduction of the so called Emission Controlled Areas within the IMO Tier III legislation forces manufacturers of maritime propulsion systems to adherence to stringent emission thresholds. Dual fuel combustion, which is characterized by the injection of a small amount of fuel oil to ignite a premixed natural gas air mixture, constitutes an option to meet this target. At high diesel substitution rates and very short pilot injection events, the injector is operated in the ballistic regime. This influences spray penetration, mixture formation and ignition behavior. In the present work, a seven-hole dual fuel injector was measured in a combustion chamber to provide data for the generation of a CFD model using the commercial code AVL FIRE. The liquid and the vapor phase of the fuel spray were quantified by Mie-scattering and Schlieren-imaging technique for different chamber conditions. Based on the measured spray characteristics, a methodology was developed to imprint a velocity profile to the initial droplets in the CFD model, to depict the spray penetration for small injection durations. To characterize the ignition process and the flame propagation, measurements of the OH* emission and the natural luminosity of the flame were carried out. A detailed reaction mechanism, which is able to predict both diesel and dual fuel combustion, was integrated in the CFD model. The ignition delay was fitted to the experimental data by adapting the reaction mechanism for different chamber temperatures. The influence of the presence of natural gas on the ignition behavior was validated using data from a rapid compression machine. Even for low temperatures and high pressures, similar to the start of injection under engine operating conditions, a good correlation could be achieved. The developed knowledge will be transferred to an engine model to investigate the limits of dual fuel combustion processes.
机译:在IMO Tier III立法中引入所谓的排放控制区域迫使海上推进系统的制造商遵守严格的排放阈值。双燃料燃烧,其特征在于注入少量燃料油以点燃预混合的天然气空气混合物,构成满足该靶标的选项。在高柴油替换速率和非常短的先导事件中,喷射器在弹道方案中运行。这影响喷雾渗透,混合物形成和点火行为。在本作工作中,在燃烧室中测量七孔双燃料喷射器,以提供使用商业代码AVL Fire来产生CFD模型的数据。通过Mie散射和Schlieren成像技术进行燃料喷雾的液体和气相,用于不同的室内条件。基于测量的喷射特性,开发了一种方法,以将速度曲线印在CFD模型中的初始液滴,描绘用于小注射持续时间的喷雾渗透。为了表征点火过程和火焰传播,进行OH *发射的测量和火焰的自然发光度。一种详细的反应机构,能够预测柴油和双燃料燃烧,在CFD模型中集成在CFD模型中。通过调整不同室温的反应机制,将点火延迟装配到实验数据。使用来自快速压缩机的数据验证了天然气对点火行为的影响。即使对于低温和高压力,类似于发动机操作条件下的注射的开始,也可以实现良好的相关性。开发知识将转移到发动机模型,以研究双燃料燃烧过程的限制。

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