Estimation of Piston Surface Temperature During Engine Transient Operation for Emissions Reduction

Zhijia Yang, Byron Mason, Brian Wooyeol Bae, Fabrizio Bonatesta, Richard Burke, Edward Chappell

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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 languageEnglish
Article number091014
Number of pages10
JournalJournal of Engineering for Gas Turbines and Power: Transactions of the ASME
Volume146
Issue number9
Early online date13 Mar 2024
DOIs
Publication statusPublished - 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).

FundersFunder number
Innovate UK113130

    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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