Mechanisms of spray formation and combustion from a multi-hole injector with E85 and gasoline

被引:133
作者
Aleiferis, P. G. [1 ]
Serras-Pereira, J. [1 ]
van Romunde, Z. [1 ]
Caine, J.
Wirth, M. [2 ]
机构
[1] UCL, Dept Mech Engn, London WC1E 7JE, England
[2] Ford Werke GmbH, Cologne, Germany
关键词
Spray formation; Combustion; Ethanol; Gasoline; E85; DISI engines; LIQUID JETS; FUEL; BREAKUP; ATOMIZATION; NOZZLE;
D O I
10.1016/j.combustflame.2009.12.019
中图分类号
O414.1 [热力学];
学科分类号
摘要
The spray formation and combustion characteristics of gasoline and E85 (85% ethanol, 15% gasoline) have been investigated using a multi-hole injector with asymmetric nozzle-hole arrangement. Experiments were carried out in a quiescent optical chamber using high-speed shadowgraphy (9 kHz) to characterise the spray sensitivity to both injector temperature and ambient pressure in the range of 20-120 degrees C and 0.5, 1.0 bar. Spray-tip penetrations and 'umbrella' spray cone angles were calculated for all conditions. Phase Doppler Anemometry was also used to measure droplet sizes in the core of one of the spray plumes, 25 rum below the injector tip. To study the effect of fuel properties on vaporisation and mixture preparation under realistic operating conditions, a separate set of experiments was carried out in a direct-injection Spark-ignition optical engine. The engine was run at 1500 RPM under cold and fully warmed-up conditions (20 degrees C and 90 degrees C) at part load and full load (0.5 and 1.0 bar intake pressure). Floodlit laser Mie-scattering images of the sprays on two orthogonal planes Corresponding to the swirl and tumble planes of in-cylinder flow motion were acquired to study the full injection event and post-injection mixing stage. These were used to make comparisons with the static chamber sprays and to quantify the liquid-to-vapour phase evaporation process for both fuels by calculating the projected 'footprint' of the Sprays at different conditions. Analysis of the macroscopic structure and turbulent primary break-up properties of the sprays was undertaken in light of jet exit conditions described in terms of non-dimensional numbers. The effects on stoichiometric combustion were investigated by imaging the natural flame chemiluminescence through the engine's piston crown (swirl plane) and by post-processing to derive flame growth rates and trajectories of flame motion. (c) 2009 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:735 / 756
页数:22
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