The relative benefit of a power turbine as a means of exhaust energy recovery (i.e., turbocompounding) being used in conjunction with altered intake valve closure timing (Miller cycle) on a medium speed diesel engine has been investigated. An assessment of the impact of these different engine architectures on the various loss mechanisms has been performed using second law analysis. The Miller and turbocompounding cycle modification as well as the combination of the two features were studied and their relative benefits are compared and discussed. Results show the corresponding decrease in effective compression ratio achieved with Miller cycle leads to lower pre-turbine exhaust availability, which decreases the potential benefit of turbocompounding.
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ASME 2010 Internal Combustion Engine Division Fall Technical Conference
September 12–15, 2010
San Antonio, Texas, USA
Conference Sponsors:
- Internal Combustion Engine Division
ISBN:
978-0-7918-4944-6
PROCEEDINGS PAPER
An Assessment of the Relative Benefits of Miller Cycle and Turbocompounding on a Medium Speed Diesel Engine Using Second Law Analysis
Thomas M. Lavertu,
Thomas M. Lavertu
GE Global Research Center, Niskayuna, NY
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Roy J. Primus,
Roy J. Primus
GE Global Research Center, Niskayuna, NY
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Omowoleola C. Akinyemi
Omowoleola C. Akinyemi
GE Global Research Center, Niskayuna, NY
Search for other works by this author on:
Thomas M. Lavertu
GE Global Research Center, Niskayuna, NY
Roy J. Primus
GE Global Research Center, Niskayuna, NY
Omowoleola C. Akinyemi
GE Global Research Center, Niskayuna, NY
Paper No:
ICEF2010-35085, pp. 65-73; 9 pages
Published Online:
January 10, 2011
Citation
Lavertu, TM, Primus, RJ, & Akinyemi, OC. "An Assessment of the Relative Benefits of Miller Cycle and Turbocompounding on a Medium Speed Diesel Engine Using Second Law Analysis." Proceedings of the ASME 2010 Internal Combustion Engine Division Fall Technical Conference. ASME 2010 Internal Combustion Engine Division Fall Technical Conference. San Antonio, Texas, USA. September 12–15, 2010. pp. 65-73. ASME. https://doi.org/10.1115/ICEF2010-35085
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