1,161 research outputs found

    Heat and mass transfer effects in the nozzle of a fuel injector from the start of needle lift to after the end of injection in the presence of fuel dribble and air entrainment

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    The design of fuel injectors is key to achieving high-efficiency engine combustion with low tailpipe emissions. The small dimensions of injector nozzle holes make the manufacturing of real-size optical injectors aimed at fundamental understanding of in-nozzle processes at design stage very challenging, especially for operation under realistic in-cylinder thermodynamic conditions. Therefore, faithful numerical predictions based on complete multiphase flow simulations upstream and downstream of the nozzle exit of a real injector geometry are highly sought after. In this paper, numerical studies of a Diesel injector nozzle with moving needle were performed using transient Reynolds Averaged Navier-Stokes (RANS) modelling with compressibility of all phases accounted for. A Volume of Fluid (VOF) method was employed, coupled to cavitation and evaporation submodels, along with a complete set of pressure and temperature dependent thermophysical fuel properties. The aim was to understand the flow inside the nozzle both during injection and after the end of injection, including fuel dribble and air backfilling effects. A range of fuel injection and air chamber pressures and temperatures were simulated, namely 400 and 900 bar upstream and 1, 35 and 60 bar downstream. Fuel, air and wall temperatures were varied in the range 300 K to 550 K. The results showed that the flow during injection carried hysteresis effects. After the end of injection, the state of the nozzle varied from being filled with a large amount of liquid to being filled mostly with air. Some form of immediate fuel dribble existed in all test cases, whilst late liquid fuel mass expulsion was also predicted under certain conditions. The latter prediction highlighted sensitivity to the models enabled. The use of a transient pressure outlet based on an engine's expansion stroke pressure trace affected the process of late fuel expulsion by pulling fuel out of the nozzle in multiphase form faster. These processes are of particular importance as they can contribute directly to unburned hydrocarbon emissions and/or the formation of deposits inside the holes. Starting a second injection from the resulting state of the nozzle at the end of the original injection resulted in a deformed liquid jet tip without the classic mushroom shape and a temporarily lower liquid jet penetration

    Time-resolved fuel injector flow characterisation based on 3D laser Doppler vibrometry

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    In order to enable investigations of the fuel flow inside unmodified injectors, we have developed a new experimental approach to measure time-resolved vibration spectra of diesel nozzles using a three dimensional laser vibrometer. The technique we propose is based on the triangulation of the vibrometer and fuel pressure transducer signals, and enables the quantitative characterisation of quasi-cyclic internal flows without requiring modifications to the injector, the working fluid, or limiting the fuel injection pressure. The vibrometer, which uses the Doppler effect to measure the velocity of a vibrating object, was used to scan injector nozzle tips during the injection event. The data were processed using a discrete Fourier transform to provide time-resolved spectra for valve-closed-orifice, minisac and microsac nozzle geometries, and injection pressures ranging from 60 to 160MPa, hence offering unprecedented insight into cyclic cavitation and internal mechanical dynamic processes. A peak was consistently found in the spectrograms between 6 and 7.5kHz for all nozzles and injection pressures. Further evidence of a similar spectral peak was obtained from the fuel pressure transducer and a needle lift sensor mounted into the injector body. Evidence of propagation of the nozzle oscillations to the liquid sprays was obtained by recording high-speed videos of the near-nozzle diesel jet, and computing the fast Fourier transform for a number of pixel locations at the interface of the jets. This 6-7.5kHz frequency peak is proposed to be the natural frequency for the injector's main internal fuel line. Other spectral peaks were found between 35 and 45kHz for certain nozzle geometries, suggesting that these particular frequencies may be linked to nozzle dependent cavitation phenomena.Comment: 12 pages, 10 figure
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