首页> 外文会议>SAE World Congress and Exhibition >Measurements of Liquid Length, Vapor Penetration, Ignition Delay, and Flame Lift-Off Length for the Engine Combustion Network ‘Spray B’ in a 2.34 L Heavy-Duty Optical Diesel Engine
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Measurements of Liquid Length, Vapor Penetration, Ignition Delay, and Flame Lift-Off Length for the Engine Combustion Network ‘Spray B’ in a 2.34 L Heavy-Duty Optical Diesel Engine

机译:用于2.34L重型光学柴油发动机的发动机燃烧网络“喷射B”的液体长度,蒸汽渗透,点火延迟和火焰升降长度的测量

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This paper presents new measurements of liquid and liftoff lengths, vapor penetration, and ignition delay using the Engine Combustion Network (ECN) ‘Spray B’ injector in a 2.34 L skip-fired heavy-duty optical engine. The data from the Spray B injector, having three 90-micron holes, are compared with previously existing constant-volume vessel data using both the Spray B injector as well as the ECN Spray A injector, which has a single 90-micron axial hole. The new data were acquired using Mie scattering, OH* chemiluminescence imaging, schlieren imaging, and incylinder pressure measurements. This paper presents data from estimated isentropic-core top-dead-center conditions with ambient densities of 15.2 and 22.8 kg/m3, temperatures of 800, 900, and 1000 K, and for both non-reacting (0% and 7.5% O_2) and reacting (13, 15, and 21% O_2) injections of n-dodecane at fuel-rail pressures of 500, 1000, and 1500 bar. Particular attention is given to the data analysis process during transient injection, and boundary condition uncertainty. In addition to the hole of interest (#3), measurements from all three Spray B holes demonstrate that the hole-to-hole variations are small, but may indicate that the influence of internal sac flows, as well as orifice geometry, are important. In addition to the ensemble-averaged data presented here, the full dataset including cycle-to-cycle variability has also been published to an online-database available at https://ecn.sandia.gov for computer model validation. A companion paper makes a preliminary comparison of these data to Reynolds-averaged Navier Stokes solutions using Lib-ICE to simulate Spray B with a sector mesh.
机译:本文呈现的液体和剥离长度的新的测量结果,蒸汽渗透,以及使用该发动机燃烧网络(ECN)点火延迟“喷雾B”喷射器在2.34大号跳过烧成重型光学引擎。从喷雾乙喷射器中的数据,具有三个90微米的孔,与同时使用喷雾乙喷射器以及在ECN喷涂A喷射器,它有一个单一的90微米的轴向孔先前存在的恒定体积的容器中的数据进行比较。新的数据使用Mie散射,OH *的化学发光成像,纹影成像和缸内压力测量获得的。本文呈现从15.2环境密度和22.8千克/米3,在800的温度下,900,和1000 [K估计等熵芯顶部死点状态的数据,以及用于两个非反应性(0%和7.5%O_2)和反应(13,15,和21%O_2)在500,1000,和1500巴的燃料轨道压力正十二烷的注射。过渡时喷射和边界条件的不确定性时特别注意了数据分析过程。除了感兴趣的(#3)的孔中,从所有三个喷雾乙孔测量表明,该孔与孔的变化小,但可以指示内部囊的影响流动,以及孔的几何形状,是重要的。除了这里提出的整体平均数据,完整数据集,包括周期到周期的变化也被发布到计算机模型验证可用的在线数据库中https://ecn.sandia.gov。一个同伴纸使得使用LIB-ICE以模拟喷雾乙与扇区啮合这些数据雷诺兹平均Navier斯托克斯解决方案的初步比较。

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