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Journal Article

Two-Dimensional In-Cylinder Soot Volume Fractions in Diesel Low Temperature Combustion Mode

2011-04-12
2011-01-1390
Soot Volume Fraction (SVF) measurements were performed in an IFP Energies nouvelles optical single cylinder Diesel engine operated in Low Temperature Combustion (LTC) conditions. The engine was equipped with a sapphire liner, a dedicated flat bowl piston and a six-hole common-rail high pressure injector. The piston design included four quartz windows allowing optical access into the bowl. The aim of this work was to study soot formation and oxidation during the LTC Diesel combustion process and to build a database providing soot formation and oxidation data under a set of engine conditions to help developing and testing Computational Fluid Dynamics (CFD) models. Two complementary optical diagnostic techniques were combined: Planar Laser Induced Incandescence (PLII) and Laser Extinction Method (LEM).
Journal Article

Study of Soot Formation and Oxidation in the Engine Combustion Network (ECN), Spray A: Effects of Ambient Temperature and Oxygen Concentration

2013-04-08
2013-01-0901
Within the Engine Combustion Network (ECN) spray combustion research frame, simultaneous line-of-sight laser extinction measurements and laser-induced incandescence (LII) imaging were performed to derive the soot volume fraction (fv). Experiments are conducted at engine-relevant high-temperature and high-pressure conditions in a constant-volume pre-combustion type vessel. The target condition, called "Spray A," uses well-defined ambient (900 K, 60 bar, 22.8 kg/m₃, 15% oxygen) and injector conditions (common rail, 1500 bar, KS1.5/86 nozzle, 0.090 mm orifice diameter, n-dodecane, 363 K). Extinction measurements are used to calibrate LII images for quantitative soot distribution measurements at cross sections intersecting the spray axis. LII images are taken after the start of injection where quasi-stationary combustion is already established.
Technical Paper

Time-Resolved Fuel Film Thickness Measurement for Direct Injection SI Engines Using Refractive Index Matching

2011-04-12
2011-01-1215
The fuel film thickness resulting from fuel spray impingement on a flat transparent window was characterized in a high pressure high temperature cell for various thermodynamic conditions, injection pressures, injection durations, fuel types and injector technologies by Refractive Index Matching technique. The ambient conditions at injection timing were similar to that of a direct injection spark ignition engine at Top Dead Center, with the distance between the injector tip and the impinging surface set to 10 mm. The spray axis was set normal to the rough transparent window surface at ambient temperatures of 453 K, 573 K and 673 K, and ambient densities of 5.0 kg/m₃, 6.0 kg/m₃ and 6.5 kg/m₃. Injection pressures of 100 and 200 bar were investigated. Three injector technologies were studied: piezo-electric, multi-holes and swirl types. Two fuels, iso-octane and model gasoline, were tested.
Technical Paper

Investigation of the Mixing Process and the Fuel Mass Concentration Fields for a Gasoline Direct-Injection Spray at ECN Spray G Conditions and Variants

2015-09-01
2015-01-1902
Within the Engine Combustion Network (ECN) research frame, the mixing process and the fuel mass concentration fields were investigated at spray G conditions and variants with optical diagnostics. Experiments were conducted in a high-temperature high-pressure constant-volume pre-combustion vessel. The target condition, called “Spray G”, which is representative of gasoline direct-injection engine conditions, uses well-defined ambient (573 K, 6 bar, 3.5 kg/m3, O2-free) and injector conditions (200 bar, eight-hole injector, 0.165 mm orifice diameter). Measurements were also conducted at 6 and 9 kg/m3 for temperatures of 700 and 800 K respectively. Two techniques were used to visualize the jet formation: p-difluorobenzene laser induced fluorescence (LIF) imaging and high-repetition-rate schlieren visualization. Images from both methods were compared in terms of jet penetration and size.
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