One class of advanced diesel engines operates with low heat rejection and high operating temperatures; piston-ring / liner lubrication is a major problem for these engines. This study attempts to illustrate the time-dependent thermal environment around the top piston ring and lubricant in these advanced engines. Particular emphasis will be placed on the maximum lubricant temperature. The analysis starts with a standard cycle simulation and a global finite-element analysis of the piston and liner in relative motion. A more detailed finite-element model, which considers variable oil film thickness on the liner, focuses on the top ring and lubricant and uses the groove and liner temperatures generated in the global analysis as boundary conditions. Results for different heat rejection engine configurations are presented. We observe that because of major transient effects, high lubricant temperature is experienced not only at top ring reversal but also down the liner to bottom ring reversal.
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July 1989
Research Papers
Piston Ring Thermal Transient Effects on Lubricant Temperatures in Advanced Engines
M. E. Boisclair,
M. E. Boisclair
Sloan Automotive Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139
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D. P. Hoult,
D. P. Hoult
Sloan Automotive Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139
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V. W. Wong
V. W. Wong
Sloan Automotive Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139
Search for other works by this author on:
M. E. Boisclair
Sloan Automotive Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139
D. P. Hoult
Sloan Automotive Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139
V. W. Wong
Sloan Automotive Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139
J. Eng. Gas Turbines Power. Jul 1989, 111(3): 543-552 (10 pages)
Published Online: July 1, 1989
Article history
Received:
August 1, 1988
Online:
October 15, 2009
Citation
Boisclair, M. E., Hoult, D. P., and Wong, V. W. (July 1, 1989). "Piston Ring Thermal Transient Effects on Lubricant Temperatures in Advanced Engines." ASME. J. Eng. Gas Turbines Power. July 1989; 111(3): 543–552. https://doi.org/10.1115/1.3240289
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