首页> 外文会议>ASME Internal Combustion Engine Division technical conference >DEVELOPMENT OF A NUMERICAL MODEL FOR IGNITION PHENOMENA IN A MICRO PILOT IGNITED DUAL FUEL ENGINE WITH EXTERNAL MIXTURE FORMATION
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DEVELOPMENT OF A NUMERICAL MODEL FOR IGNITION PHENOMENA IN A MICRO PILOT IGNITED DUAL FUEL ENGINE WITH EXTERNAL MIXTURE FORMATION

机译:外部混合形成微飞行员点火双燃料发动机点火现象数值模型的建立

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In this paper, a numerical investigation of the ignition process of dual fuel engines is presented. Optical measurements revealed that a homogeneous natural gas charge ignited by a small diesel pilot comprises the combustion phenomena of compression ignition of the pilot fuel as well as premixed flame propagation. The 3-Zones Extended Coherent Flame Model (ECFM3Z) was selected, since it can treat auto-ignition, premixed flame propagation and diffusion flame aspects. Usually combustion models in multi-dimensional computational fluid dynamics (CFD) software packages are designed to handle only one reactive species representing the fuel concentration. In the context of the ECFM3Z model the concept of a multi-component fuel is applied to dual fuel operation. Since the available ignition models were not able to accurately describe the ignition characteristics of the investigated setup, a new dual fuel auto-ignition model was developed. Ignition delay times of the fuel blend are tabulated using a detailed reaction mechanism for n-heptane. Thereby, the local progress of pre-ignition reactions in the CFD simulation can be calculated. The ignition model is validated against experiments conducted with a periodically chargeable constant volume combustion chamber. The proposed model is capable to reproduce the ignition delay as well as the location of the flame kernels. The CFD simulations show the effect of temperature stratification and variations in the injection pressure on the apparent ignition delay of the micro pilot.
机译:本文对双燃料发动机的点火过程进行了数值研究。光学测量表明,由小型柴油引燃器点燃的均匀天然气装料包括引燃燃料压缩点火以及预混火焰传播的燃烧现象。选择了三区扩展相干火焰模型(ECFM3Z),因为它可以处理自燃,预混火焰传播和扩散火焰方面。通常,多维计算流体动力学(CFD)软件包中的燃烧模型被设计为仅处理代表燃料浓度的一种反应性物质。在ECFM3Z模型的上下文中,将多组分燃料的概念应用于双燃料运行。由于可用的点火模型无法准确描述所研究装置的点火特性,因此开发了新的双燃料自动点火模型。使用正庚烷的详细反应机理,将燃料混合物的点火延迟时间制成表格。由此,可以计算出CFD模拟中的点火前反应的局部进程。点火模型是通过使用可定期充电的恒容燃烧室进行的实验验证的。所提出的模型能够再现点火延迟以及火焰核的位置。 CFD仿真显示了温度分层和喷射压力变化对微型先导表观点火延迟的影响。

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