Spray structure and characteristics of high-pressure gasoline injectors for direct-injection engine applications

被引:29
作者
Lee, CS [1 ]
Lee, KH
Chon, MS
Kim, DS
机构
[1] Hanyang Univ, Dept Engn Mech, Seoul 133791, South Korea
[2] Daewoo Motor Co Ltd, Ctr Tech, Inchon, South Korea
[3] Hanyang Univ, Grad Sch, Seoul 133791, South Korea
关键词
Atomization - Combustion - Diesel engines - Drop formation - Gasoline - High pressure effects - Particle size analysis - Spraying - Vaporization - Velocity measurement;
D O I
10.1615/AtomizSpr.v11.i1.30
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This article presents an experimental analysis of spray development, spray tip penetration, and the macroscopic characteristics of a high-pressure gasoline injector for direct-injected gasoline engine applications. Also, this study deals with microscopic characteristics of the fuel spray, such as mean droplet size, mean velocity, and the instantaneous velocity vector fields in the fuel spray of a high-pressure injector The spray development, spray penetration, and global spray structure H ere visualized using a shadowgraph technique. Atomization characteristics of the fuel spray such as mean droplet sizes and mean velocities were measured using the phase Doppler particle analyzer system. In addition, instantaneous velocity vector fields of the fuel spray with time after injection sere obtained from cross-correlation particle image velocimetry. The experimental results obtained provide the effect of injection pressure on the spray behaviors, spray structure, microscopic characteristics of the fuel spray, and the velocity vector fields at different moments after the start of injection. The injection pressure of the fuel is an important factor, which has an effect on the spray development processes involving the spray tip penetration, spray width, and mixing of fuel droplets and ambient air. With an increase in fuel injection pressure, the droplet size decreases, and the location of maximum droplet size appears farther downstream than in the case of low injection pressure. The results of spray visualization show that the counterrotating vortex along the outer edge of the spray surface is observed at a later stage of fuel injection, and it continues until right after the end of fuel injection. The velocity vector fields by particle image velocimetry show detailed flow vectors and spray development processes in the fuel sprays at different elapsed times after the start of injection.
引用
收藏
页码:35 / 48
页数:14
相关论文
共 14 条
[1]  
ANDO H, 1996, S43300196
[2]  
[Anonymous], 1995, SAE TECHNICAL PAPER
[3]  
Chigier N., 1996, PROGR AERONAUTICS AS, V166, P109, DOI DOI 10.2514/5.9781600866418.0109.0135
[4]  
Iwamoto Y., 1997, SAE TECHNICAL PAPER
[5]  
JEONG HY, 1998, P ILASS KOR ANN M 98, P32
[6]  
KANEKO M, 1998, 3 C ILASS AS, P135
[7]   MEASUREMENT OF LIQUID DROPLET DISINTEGRATION MECHANISMS [J].
KRZECZKOWSKI, SA .
INTERNATIONAL JOURNAL OF MULTIPHASE FLOW, 1980, 6 (03) :227-239
[8]  
KUME T, 1996, FISTA 96
[9]  
LEE C, 1997, S ATOMIZATION, P69
[10]  
Lefebvre A.H., 1989, ATOMIZATION SPRAY, P41