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The Impact of Fuel Mass, Injection Pressure, Ambient Temperature, and Swirl Ratio on the Mixture Preparation of a Pilot Injection

机译:燃料质量,注射压力,环境温度和旋流比对燃料喷射的混合物的影响

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Fuel tracer-based planar laser-induced fluorescence is used to investigate the vaporization and mixing behavior of pilot injections for variations in pilot mass of 1-4 mg, and for two injection pressures, two near-TDC ambient temperatures, and two swirl ratios. The fluorescent tracer employed, 1-methylnaphthalene, permits a mixture of the diesel primary reference fuels, n-hexadecane and heptamethylnonane, to be used as the base fuel. With a near-TDC injection timing of -15°C A, pilot injection fuel is found to penetrate to the bowl rim wall for even the smallest injection quantity, where it rapidly forms fuel-lean mixture. With increased pilot mass, there is greater penetration and fuel-rich mixtures persist well beyond the expected pilot ignition delay period. Significant jet-to-jet variations in fuel distribution due to differences in the individual jet trajectories (included angle) are also observed. Increased injection pressure significantly increased the mixing rate, leading to leaner mixture distributions, and with lower ambient temperature modestly richer mixtures are found near the heads of the jets. Discrete droplets near the injector were unexpectedly found to be more common at the higher ambient temperature. Lastly, increased swirl displaces the fuel to locations lower in the bowl, while generating a greater amount of over-lean mixture in the upper-central region of the combustion chamber.
机译:基于示踪燃料平面激光诱导的荧光被用于研究引燃喷射为在1-4毫克的导频质量变异的汽化和混合行为,以及用于两个喷射压力,两个近TDC环境温度下,和两个涡流比。所采用的荧光示踪剂,1-甲基萘,允许柴油主要参考燃料的混合物,正十六烷和七甲基壬烷,用作基础燃料。用-15℃A的近TDC喷射正时,引燃喷射的燃料被发现渗透到碗边缘壁,即使是最小喷射量,在那里它迅速形成贫燃料混合物。随着试点增加质量,存在较大的渗透和富燃料混合物持续远远超出预期的试点着火延迟期。显著由于在各个射流轨迹(夹角)的差异喷射到喷射变化燃料分配还观察到。增加喷射压力显著提高混合速率,导致稀混合分布,并具有较低的环境温度下温和更丰富的混合物中发现的射流的头部附近。喷射器附近的离散液滴意外地发现在较高环境温度下更常见。最后,增加涡流位移的燃料位置在碗降低,而在所述燃烧室的上中央区域产生的过稀混合物的用量更大。

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