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2002
DOI: 10.5194/acpd-2-2045-2002
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Emission of ions and charged soot particles by aircraft engines

Abstract: Abstract. In this article, a model which examines the formation and evolution of chemiions in an aircraft engine is proposed. This model which includes chemiionisation, electron thermo-emission, electron attachment to soot particles and to neutral molecules, electron-ion and ion-ion recombination, ion-soot interaction, allows the determination of the ion concentration at the exit of the combustor and at the nozzle exit of the engine. It also allows the determination of the charge of the soot particles. A compa… Show more

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Cited by 19 publications
(16 citation statements)
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“…In general, the size of a soot particle in an aero gas turbine engine exhaust port is typically about 6nm and the distribution of the size is a bimodal distribution with humps in the ranges of 5~7nm and 20~30nm [54][55][56]. The sizes of carbon particles or metal abrasive and most of the abnormal particles caused by gas path component faults, such as blade rub or combustion performance degradation, are larger than 40um [14].…”
Section: The Formation Of Charged Particlesmentioning
confidence: 99%
“…In general, the size of a soot particle in an aero gas turbine engine exhaust port is typically about 6nm and the distribution of the size is a bimodal distribution with humps in the ranges of 5~7nm and 20~30nm [54][55][56]. The sizes of carbon particles or metal abrasive and most of the abnormal particles caused by gas path component faults, such as blade rub or combustion performance degradation, are larger than 40um [14].…”
Section: The Formation Of Charged Particlesmentioning
confidence: 99%
“…Studies by Arnold Sorokin show that there are two different particle diameter distributions in the engine exhaust, and the size of carbon particles is 5~7nm, and 20~30nm [12,14]. During gas path component failure (such as blade rub) or combustion performance degradation, which results in the large-size carbon particles or metal abrasion, most of these abnormal particle sizes are larger than 40μm [15].…”
Section: The Effect Factors On the Electrostatic Charge In The Aero-ementioning
confidence: 99%
“…In general, the carbon particles charge mainly through thermal ionization and electric adsorption; carbon particles can obtain a charge from the thermal emission of electrons, and can also interact with the ion produced by chemical ionization and the adsorb charge, and the charge may increase with the absorption of ions and the reaction with the various types of ions. The positive and negative ions in the aero-engine exhaust are measured in experimental studies [12][13][14], which also analyze the effect of the fuel flow and sulfur content on the quantity of the electrostatic charge. The experimental results show: (1) The concentration of negative ions increases with the increase of fuel sulfur content, and in the case of low flow in particular, the concentration of positive ions is affected less.…”
Section: The Charging Mechanism Of Carbon Particlesmentioning
confidence: 99%
“…In the process, dissociation reactions provide part of the energy required for ionisation since there are exothermic and the rest is from the flame. Exited methyl radical CH * is a known contributor to ionisation in the hydrocarbon flames e.g., in Sorokin et al [10]. CH radical reacts with oxygen atoms in the flame to produce CHO + , a primary ion in hydrocarbon flames and electrons according to the following reaction equation:…”
Section: Chemi-ionisationmentioning
confidence: 99%