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dc.contributor.authorYang, Zhijia
dc.contributor.authorMason, Byron
dc.contributor.authorBae, Brian Wooyeol
dc.contributor.authorBonatesta, Fabrizio
dc.contributor.authorWinward, Edward
dc.contributor.authorBurke, Richard
dc.contributor.authorChappell, Edward
dc.date.accessioned2024-12-24T18:53:11Z
dc.date.available2024-12-24T18:53:11Z
dc.date.copyright4/4/2024 12:00:00 AM
dc.date.issued2024
dc.identifier.issn0742-4795
dc.identifier.othergtp_146_09_091014.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302924
dc.description.abstractPiston surface temperature is an important factor in the reduction of harmful emissions in modern gasoline direct injection (GDI) engines. In transient operation, the piston surface temperature can change rapidly, increasing the risk of fuel puddling. The prediction of the piston surface temperature can provide the means to significantly improve multiple-pulse fuel injection control strategies through the avoidance of fuel puddling. It could also be used to intelligently control the piston cooling jet (PCJ), which is common in modern engines. Considerable research has been undertaken to identify generalized engine heat transfer correlations and to predict piston and cylinder wall surface temperatures during operation. Most of these correlations require in-cylinder combustion pressure as an input, as well as the identification of numerous model parameters. These requirements render such an approach impractical. In this study, the authors have developed a thermodynamic model of piston surface temperature based on the global energy balance (GEB) methodology, which includes the effect of PCJ activation. The advantages are a simple structure and no requirement for in-cylinder pressure data, and only limited experimental tests are needed for model parameter identification. Moreover, the proposed model works well during engine transient operation, with maximum average error of 6.68% during rapid transients. A detailed identification procedure is given. This and the model performance have been demonstrated using experimental piston crown surface temperature data from a prototype 1-liter 3-cylinder turbocharged GDI engine, operated in both engine steady-state and transient conditions with an oil jet used for piston cooling turned both on and off.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleEstimation of Piston Surface Temperature During Engine Transient Operation for Emissions Reduction
dc.typeJournal Paper
dc.journal.volume146
dc.journal.issue9
dc.journal.titleJournal of Engineering for Gas Turbines and Power
dc.identifier.doi10.1115/1.4065061
dc.journal.fristpage91014-1
dc.journal.lastpage91014-10
dc.page10
dc.treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 009
dc.contenttypeFulltext


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