2019
DOI: 10.19206/ce-2019-413
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Analysis of the macrostructure of the fuel spray atomized with marine engine injector

Abstract: One of the main problem influencing the combustion process in the cylinder of the marine engine is an fuel spray phenomena. The parameters describing the shape of the fuel spray are named macro parameters. This article presents the research results of the macrostructure parameters of the fuel spray atomized with the marine engine injector. The research were carried out by optical visualization measurement method of Mie scattering. The diameter of nozzle injector was 0.375 mm and L/D coefficient 8.3. In these r… Show more

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Cited by 5 publications
(9 citation statements)
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“…This is caused by the aerodynamic resistance in the constant volume chamber (secondary breakup). The influence of increasing backpressure on reducing the STP was shown in Grochowalska (2019), Payri et al (2017), Wang et al (2016) and Yan et al (2016) and are confirmed by the present results. On the basis of the analysis in Figure 5 and Grochowalska (2019), it may be concluded that an increase of backpressure generally causes a reduction of STP for big nozzles.…”
Section: Resultssupporting
confidence: 90%
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“…This is caused by the aerodynamic resistance in the constant volume chamber (secondary breakup). The influence of increasing backpressure on reducing the STP was shown in Grochowalska (2019), Payri et al (2017), Wang et al (2016) and Yan et al (2016) and are confirmed by the present results. On the basis of the analysis in Figure 5 and Grochowalska (2019), it may be concluded that an increase of backpressure generally causes a reduction of STP for big nozzles.…”
Section: Resultssupporting
confidence: 90%
“…The formation of cavitation bubbles at the exit of the nozzle may cause greater dissipation and an increase in the value of the SCA (Sou et al , 2007). For Nozzles 2 and 3, there was observed a significant effect of a change in the difference between the pressures on the SCA in time (Grochowalska, 2019). This is related to the formation of large droplets in the fuel spray at the beginning and the aerodynamic resistance in the constant volume chamber.…”
Section: Resultsmentioning
confidence: 99%
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