SAE Technical Paper Series 2015
DOI: 10.4271/2015-01-1903
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Characterisation of Spray Development from Spark-Eroded and Laser-Drilled Multi-Hole Injectors in an Optical DISI Engine and in a Quiescent Injection Chamber

Abstract: This paper addresses the need for fundamental understanding of the mechanisms of fuel spray formation and mixture preparation in direct injection spark ignition (DISI) engines. Fuel injection systems for DISI engines undergo rapid developments in their design and performance, therefore, their spray breakup mechanisms in the physical conditions encountered in DISI engines over a range of operating conditions and injection strategies require continuous attention. In this context, there are sparse data in the lit… Show more

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Cited by 5 publications
(9 citation statements)
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“…The spark-ignition engine injector and conditions under study here relate to 0.2 mm nozzle dimeter and 150 bar injection pressure, leading to typical nozzle Reynolds numbers of about 30,000 and 50,000 at 293 K, 1 bar (Aleiferis and van Romunde, 2013), depending on fuel type. The r/D ratio was estimated at ~0.05-0.1 from the electron microscope images of Butcher et al (2013Butcher et al ( , 2015. This value is situated within the range suggested of 0.01-0.08 being equivalent to sharp and rounded injector radii, respectively.…”
Section: Cavitation Modelmentioning
confidence: 69%
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“…The spark-ignition engine injector and conditions under study here relate to 0.2 mm nozzle dimeter and 150 bar injection pressure, leading to typical nozzle Reynolds numbers of about 30,000 and 50,000 at 293 K, 1 bar (Aleiferis and van Romunde, 2013), depending on fuel type. The r/D ratio was estimated at ~0.05-0.1 from the electron microscope images of Butcher et al (2013Butcher et al ( , 2015. This value is situated within the range suggested of 0.01-0.08 being equivalent to sharp and rounded injector radii, respectively.…”
Section: Cavitation Modelmentioning
confidence: 69%
“…Flash boiling of gasoline fuel sprays in direct-injection engine applications can have a positive effect on air-fuel mixing, due to the increased evaporation rate and smaller droplet sizes (van Romunde and Behringer et al, 2014). However, depending on exact plume orientation and injector nozzle type, flashing and spray collapse may lead to decreased liner wall wetting but increased piston wall wetting due to increased axial momentum of the spray (Butcher et al, 2015).…”
Section: Introduction 11 Backgroundmentioning
confidence: 99%
“…The length to diameter ratio for each part of the hole (inner, outer) was of the order unity. The nozzle holes have been characterised by silicon castings and microscopy in great detail and the interested reader is guided to references [29,30] for further information. The injector used was the production version of a prototype injector of very similar geometry and nozzle hole orientation that has been tested with many different fuels over a wide range of fuel temperatures from 20 °C to 180 °C and air pressures from 0.3 bar to 5 bar in constant volume injection chambers [31][32][33] and in an optical engine [34][35][36][37][38].…”
Section: Injectormentioning
confidence: 99%
“…The injector used was the production version of a prototype injector of very similar geometry and nozzle hole orientation that has been tested with many different fuels over a wide range of fuel temperatures from 20 °C to 180 °C and air pressures from 0.3 bar to 5 bar in constant volume injection chambers [31][32][33] and in an optical engine [34][35][36][37][38]. Fuel pressure was maintained at 150 bar and the injector flow rate at this pressure can be found in [29,30], with modelled sprays at the respective flow rate found in [39][40][41]. Studies of the injector/driver delays have been presented in [32], whilst a range of further details on injector delays and injector flow rate variations for the same generation of hardware can be found in [42].…”
Section: Injectormentioning
confidence: 99%
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