P. Schihl et al., Performance characteristics of a low heat rejection direct-injection military diesel engine retrofitted with thermal barrier coated pistons, J ENG GAS T, 123(3), 2001, pp. 644-651
Citations number
35
Categorie Soggetti
Mechanical Engineering
Journal title
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME
A special two-cylinder. military specific power plant was employed to evalu
ate the effect of thermal barrier coated pistons on overall engine performa
nce at simulated low heat rejection-type operating conditions. This study f
ocused on three combustion systems including a noncoated baseline ductile i
i-an piston along with zirconia and chrome-oxide sealed zirconia coated ana
logs. For the test matrix encompassing ten full and half-load operating con
ditions, both coated piston combustion systems yielded a detrimental effect
on fuel economy in comparison to the baseline combustion system at constan
t fueling and air consumption rates. These performance differences were att
ributed to a combination of combustion phasing modulations, injection timin
g discrepancies, and sluggish combustion associated with the zirconia coate
d piston configurations.