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    Performance Characteristics of a Low Heat Rejection Direct-Injection Military Diesel Engine Retrofitted With Thermal Barrier Coated Pistons

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 003::page 644
    Author:
    P. Schihl
    ,
    E. Schwarz
    ,
    W. Bryzik
    DOI: 10.1115/1.1370372
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A special two-cylinder military specific power plant was employed to evaluate the effect of thermal barrier coated pistons on overall engine performance at simulated low heat rejection-type operating conditions. This study focused on three combustion systems including a noncoated baseline ductile iron piston along with zirconia and chrome-oxide sealed zirconia coated analogs. For the test matrix encompassing ten full and half-load operating conditions, both coated piston combustion systems yielded a detrimental effect on fuel economy in comparison to the baseline combustion system at constant fueling and air consumption rates. These performance differences were attributed to a combination of combustion phasing modulations, injection timing discrepancies, and sluggish combustion associated with the zirconia coated piston configurations.
    keyword(s): Heat , Combustion , Engines , Stress , Combustion systems , Cylinders , Military systems , Pistons , Fuel efficiency , Diesel engines , Pressure , Fuels , Delays , Ignition , Performance characterization AND Temperature ,
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      Performance Characteristics of a Low Heat Rejection Direct-Injection Military Diesel Engine Retrofitted With Thermal Barrier Coated Pistons

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/125184
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorP. Schihl
    contributor authorE. Schwarz
    contributor authorW. Bryzik
    date accessioned2017-05-09T00:04:48Z
    date available2017-05-09T00:04:48Z
    date copyrightJuly, 2001
    date issued2001
    identifier issn1528-8919
    identifier otherJETPEZ-26805#644_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125184
    description abstractA special two-cylinder military specific power plant was employed to evaluate the effect of thermal barrier coated pistons on overall engine performance at simulated low heat rejection-type operating conditions. This study focused on three combustion systems including a noncoated baseline ductile iron piston along with zirconia and chrome-oxide sealed zirconia coated analogs. For the test matrix encompassing ten full and half-load operating conditions, both coated piston combustion systems yielded a detrimental effect on fuel economy in comparison to the baseline combustion system at constant fueling and air consumption rates. These performance differences were attributed to a combination of combustion phasing modulations, injection timing discrepancies, and sluggish combustion associated with the zirconia coated piston configurations.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePerformance Characteristics of a Low Heat Rejection Direct-Injection Military Diesel Engine Retrofitted With Thermal Barrier Coated Pistons
    typeJournal Paper
    journal volume123
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1370372
    journal fristpage644
    journal lastpage651
    identifier eissn0742-4795
    keywordsHeat
    keywordsCombustion
    keywordsEngines
    keywordsStress
    keywordsCombustion systems
    keywordsCylinders
    keywordsMilitary systems
    keywordsPistons
    keywordsFuel efficiency
    keywordsDiesel engines
    keywordsPressure
    keywordsFuels
    keywordsDelays
    keywordsIgnition
    keywordsPerformance characterization AND Temperature
    treeJournal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 003
    contenttypeFulltext
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