Estimation of Piston Surface Temperature During Engine Transient Operation for Emissions ReductionSource: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 009::page 91014-1Author:Yang, Zhijia
,
Mason, Byron
,
Bae, Brian Wooyeol
,
Bonatesta, Fabrizio
,
Winward, Edward
,
Burke, Richard
,
Chappell, Edward
DOI: 10.1115/1.4065061Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Piston 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.
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| contributor author | Yang, Zhijia | |
| contributor author | Mason, Byron | |
| contributor author | Bae, Brian Wooyeol | |
| contributor author | Bonatesta, Fabrizio | |
| contributor author | Winward, Edward | |
| contributor author | Burke, Richard | |
| contributor author | Chappell, Edward | |
| date accessioned | 2024-12-24T18:53:11Z | |
| date available | 2024-12-24T18:53:11Z | |
| date copyright | 4/4/2024 12:00:00 AM | |
| date issued | 2024 | |
| identifier issn | 0742-4795 | |
| identifier other | gtp_146_09_091014.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4302924 | |
| description abstract | Piston 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. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Estimation of Piston Surface Temperature During Engine Transient Operation for Emissions Reduction | |
| type | Journal Paper | |
| journal volume | 146 | |
| journal issue | 9 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4065061 | |
| journal fristpage | 91014-1 | |
| journal lastpage | 91014-10 | |
| page | 10 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 009 | |
| contenttype | Fulltext |