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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.
Original language | English |
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Article number | 091014 |
Number of pages | 10 |
Journal | Journal of Engineering for Gas Turbines and Power: Transactions of the ASME |
Volume | 146 |
Issue number | 9 |
Early online date | 13 Mar 2024 |
DOIs | |
Publication status | Published - 1 Sept 2024 |
Data Availability Statement
The datasets generated and supporting the findings of this article are obtainable from the corresponding author upon reasonable request.Funding
Advanced Propulsion Center through Innovate UK on project (No. 113130; Funder ID: 10.13039/501100006041).
Funders | Funder number |
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Innovate UK | 113130 |
Keywords
- combustion
- experimental
- heat transfer
- internal combustion engines
- modeling
- piston surface temperature
ASJC Scopus subject areas
- Nuclear Energy and Engineering
- Fuel Technology
- Aerospace Engineering
- Energy Engineering and Power Technology
- Mechanical Engineering
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Dive into the research topics of 'Estimation of Piston Surface Temperature During Engine Transient Operation for Emissions Reduction'. Together they form a unique fingerprint.Projects
- 1 Finished
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DYNamic Analysis Modelling and Optimisation of GDI Engines (DYNAMO)
Akehurst, S. (PI), Brace, C. (CoI), Burke, R. (CoI), Copeland, C. (CoI), Turner, J. (CoI), Chappell, E. (Researcher), Lewis, A. (Researcher) & Pickering, S. (Researcher)
Innovate UK, Innovate UK Business Connect
1/08/17 → 31/07/21
Project: Central government, health and local authorities