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A study of the influence of orifice diameter on a turbulent jet ignition system through combustion visualization and performance characterization in a rapid compression machine

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TLDR
In this article, the effect of the size of the nozzle orifice on the performance of a turbulent jet ignition system was investigated and it was shown that increasing the diameter of the orifice increased the Reynolds number of the discharging jet.
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This article is published in Applied Thermal Engineering.The article was published on 2015-04-25. It has received 123 citations till now. The article focuses on the topics: Jet (fluid) & Ignition system.

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Citations
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On ignition mechanisms of premixed CH4/air and H2/air using a hot turbulent jet generated by pre-chamber combustion

TL;DR: In this article, a parametric study was performed to understand the effects of pressure, temperature, equivalence ratio along with geometric factors such as orifice diameter and spark position on the ignition mechanisms and probability.
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A review of prechamber ignition systems as lean combustion technology for SI engines

TL;DR: In this paper, a literature review has been made about pre-chamber ignition systems as lean combustion technology, focusing in the several investigations regarding combustion and emissions characteristics and presenting the key advantages and challenges in pre chamber ignition technology application.
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Evaluation of the passive pre-chamber ignition concept for future high compression ratio turbocharged spark-ignition engines

TL;DR: In this paper, a 1D Wave Action Model was generated to design the pre-chamber geometry taking the fuel available at the start of prechamber combustion and the pressure difference between the main chamber and pre chamber as key parameters.
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A study of the turbulent jet flow field in a methane fueled turbulent jet ignition (TJI) system

TL;DR: In this paper, the authors analytically and computationally examined the transient jet used to ignite combustible mixtures during Turbulent Jet Ignition (TJI) in both the prechamber and the main chamber.
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A study of a turbulent jet ignition system fueled with iso-octane: Pressure trace analysis and combustion visualization

TL;DR: In this article, the effects of auxiliary fuel injection and ignition distribution due to nozzle geometry were studied in a rapid compression machine using liquid iso-octane and turbulent jet ignition.
References
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Journal ArticleDOI

A study of the combustion and emission characteristics of compressed-natural-gas direct-injection stratified combustion using a rapid-compression-machine

TL;DR: In this article, the characteristics of combustion and emissions of compressed-natural-gas (CNG) direct-injection combustion using a rapid-compression-machine which has a compression ratio of 10 and a disc-shaped combustion chamber.
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Detailed investigation of ignition by hot gas jets

TL;DR: In this article, an experimental realisation of such an ignition process, where a hot exhaust gas impinges through a narrow nozzle into a quiescent hydrogen/air mixture, possibly initiating ignition and combustion, is studied.
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Ignition behavior and surrogate modeling of JP-8 and of camelina and tallow hydrotreated renewable jet fuels at low temperatures

TL;DR: In this article, the authors investigated the autoignition characteristics of the conventional jet fuel, JP-8, and the alternative jet fuels, camelina and tallow hydrotreated renewable jet (HRJ) fuels, using a rapid compression machine and the direct test chamber charge preparation approach.
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Effect of fuel type on equivalence ratio measurements using chemiluminescence in premixed flames

TL;DR: In this article, local temporally resolved measurements of chemiluminescent intensity from OH ∗, CH ∗ and C ∗ 2 radicals were obtained in premixed counterflow flames operating with propane and prevaporised fuels (isooctane, ethanol and methanol), for different equivalence ratios and strain rates.
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