Investigation and comparison of spray characteristics of pressure-swirl atomizers for a small-sized aircraft turbine engine

dc.contributor.authorĎurdina, Lukášcs
dc.contributor.authorJedelský, Jancs
dc.contributor.authorJícha, Miroslavcs
dc.coverage.issue11cs
dc.coverage.volume78cs
dc.date.issued2014-08-08cs
dc.description.abstractThe quality of liquid fuel atomization highly affects the formation of gaseous pollutants and particulate matter emissions from combustion processes. Spray characteristics of two geometrically different pressure-swirl atom-izers for a turbojet engine in light aircraft were measured on a cold test bench. A spill-return atomizer and its intended replacement simplex atomizer were investigated using Particle Image Velocimetry (PIV) and Phase-Doppler Anemometry (PDA). Single-camera and stereoscopic PIV measurements yielded velocity distributions in the axial cross-section of the spray cone. PDA measurements provided dropsize distribution and axial velocity data. Acquired results reveal significant differences in spray characteristics of the nozzles investigated at the same fuel injection pressures. The simplex nozzle produced spray with Sauter mean diameters lower by 5–20 um depending on the regime, its spray was more stable but its shape greatly varied with fuel injection pressure. These differences are discussed in detail, their analysis indicate a potential for spray improvement provided by the novel atomizer design and elucidates the possible impact of the nozzle replacement on the combustion process.en
dc.description.abstractPříspěvek popisuje porovnání vlastností spreje dvou tlakových vířivých trysek pro malý letecký turbomotor. Sprej je zkoumán pomocí metod PIV (particle image velocimetry) a PDA (phase-Doppler anemometry) a předmětem je rychlostní pole ve spreji, rozložení kapaliny ve spreji a velikost kapek.cs
dc.formattextcs
dc.format.extent892-900cs
dc.format.mimetypeapplication/pdfcs
dc.identifier.citationInternational journal of heat and mass transfer. 2014, vol. 78, issue 11, p. 892-900.en
dc.identifier.doi10.1016/j.ijheatmasstransfer.2014.07.066cs
dc.identifier.issn0017-9310cs
dc.identifier.orcid0000-0002-1268-8434cs
dc.identifier.orcid0000-0002-1409-5165cs
dc.identifier.other108734cs
dc.identifier.researcheridA-9224-2013cs
dc.identifier.researcheridCVT-7747-2022cs
dc.identifier.scopus23090535800cs
dc.identifier.scopus6602494673cs
dc.identifier.urihttp://hdl.handle.net/11012/138393
dc.language.isoencs
dc.publisherElseviercs
dc.relation.ispartofInternational journal of heat and mass transfercs
dc.relation.urihttps://www.sciencedirect.com/science/article/pii/S0017931014006553cs
dc.rightsCreative Commons Attribution-NonCommercial-NoDerivatives 4.0 Internationalcs
dc.rights.accessopenAccesscs
dc.rights.sherpahttp://www.sherpa.ac.uk/romeo/issn/0017-9310/cs
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/cs
dc.subjectspray characteristics; pressure-swirl atomizer; particle image velocimetry; phase-Doppler anemometry; spill-return; droplet sizeen
dc.subjectPIVen
dc.subjectPDAen
dc.subjectsprej
dc.subjecttlaková vířivá tryska
dc.subjectPIV
dc.subjectPDA
dc.subjectparticle image velocimetry
dc.subjectphase-Doppler anemometry
dc.subjectvelikost kapek
dc.titleInvestigation and comparison of spray characteristics of pressure-swirl atomizers for a small-sized aircraft turbine engineen
dc.title.alternativeVýzkum a porovnání vlastností spreje tlakových vířivých trysek pro malý letecký turbomotorcs
dc.type.driverarticleen
dc.type.statusPeer-revieweden
dc.type.versionacceptedVersionen
sync.item.dbidVAV-108734en
sync.item.dbtypeVAVen
sync.item.insts2024.03.08 17:46:12en
sync.item.modts2024.03.08 17:14:00en
thesis.grantorVysoké učení technické v Brně. Fakulta strojního inženýrství. Energetický ústavcs
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