Ignition behavior of marine diesel sprays. Investigation of marine diesel ignition and combustion at engine-like conditions by means of OH* chemiluminescence and soot incandescence
dc.contributor.author | Schmid, Andreas | |
dc.contributor.author | von Rotz, Beat | |
dc.contributor.author | Bombach, Rolf | |
dc.contributor.author | Weisser, German | |
dc.contributor.author | Herrmann, Kai | |
dc.contributor.author | Boulouchos, Konstantinos | |
dc.date.accessioned | 2025-07-04T08:49:36Z | |
dc.date.issued | 2012 | |
dc.description.abstract | In this contribution, an initial investigation of the ignition behavior of large two-stroke marine diesel sprays has been performed. At engine-like conditions, the OH radical was traced with an intensified high speed camera and a sophisti-cated optical setup. A series of spectroscopic measurements showed, however, that the soot incandescence strongly con-tributes to the UV signal, superimposing with or even masking the chemiluminescence of the OH radical. As the com-bustion of typical fuels used in large two-stroke engines involves the formation of non-negligible amounts of soot, the signal is almost omnipresent during the oxidation process. A differentiation between the UV-light emitted by the OH radical and the UV-light emitted by soot incandescence is only possible when both signals are measured separately. Therefore, a second high speed camera recorded the light coming from soot incandescence. In addition, it recorded the background illuminated spray plume to make an exact positioning of the OH* signal relative to the spray possible. A comparison of the two images then allowed the differentiation between the two light sources. In a first measurement series, which included a temperature variation, ignition delay, ignition location and flame lift-off have been measured. The results are in accordance with literature, as they show a dramatic decrease in ignition delay towards higher gas temperature. On the other hand the standard deviation increases towards lower gas temperatures. The ignition location and lift-off showed similar behavior: Lower gas temperature corresponds to an increase of the distance between ignition location/lift-off and nozzle orifice along with increased standard deviation. It could be shown that the applied technique works for the investigation of large marine diesel engine combustion systems. | |
dc.event | The 8th International Conference on Modeling and Diagnostics for Advanced Engine Systems (COMODIA 2012) | |
dc.event.end | 2012-07-26 | |
dc.event.start | 2012-07-23 | |
dc.identifier.doi | https://doi.org/10.1299/jmsesdm.2012.8.182 | |
dc.identifier.uri | https://irf.fhnw.ch/handle/11654/51894 | |
dc.language.iso | en | |
dc.publisher | Japan Society of Mechanical Engineers | |
dc.relation.ispartof | The Proceedings of the International symposium on diagnostics and modeling of combustion in internal combustion engines | |
dc.spatial | Fukuoka | |
dc.subject.ddc | 620 - Ingenieurwissenschaften und Maschinenbau | |
dc.subject.ddc | 660 - Technische Chemie | |
dc.subject.ddc | 530 - Physik | |
dc.title | Ignition behavior of marine diesel sprays. Investigation of marine diesel ignition and combustion at engine-like conditions by means of OH* chemiluminescence and soot incandescence | |
dc.type | 01A - Beitrag in wissenschaftlicher Zeitschrift | |
dc.volume | 8 | |
dspace.entity.type | Publication | |
fhnw.InventedHere | No | |
fhnw.ReviewType | Anonymous ex ante peer review of a complete publication | |
fhnw.affiliation.hochschule | Hochschule für Technik und Umwelt FHNW | de_CH |
fhnw.affiliation.institut | Institut für Thermo- und Fluid-Engineering | de_CH |
fhnw.openAccessCategory | Closed | |
fhnw.pagination | 182-187 | |
fhnw.publicationState | Published | |
relation.isAuthorOfPublication | a9126497-808d-4e16-a262-b487cce0f979 | |
relation.isAuthorOfPublication.latestForDiscovery | a9126497-808d-4e16-a262-b487cce0f979 |
Files
License bundle
1 - 1 of 1
Loading...
- Name:
- license.txt
- Size:
- 2.66 KB
- Format:
- Item-specific license agreed upon to submission
- Description: