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    Numerical-Experimental Study and Solutions to Reduce the Dwell-Time Threshold for Fusion-Free Consecutive Injections in a Multijet Solenoid-Type CR System

    Source: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 002::page 22804
    Author:
    Andrea E. Catania
    ,
    Alessandro Ferrari
    ,
    Ezio Spessa
    DOI: 10.1115/1.2938394
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In “multijet” common rail (CR) diesel injection systems, when two consecutive injection current pulses approach each other, a merging of the two injections into a single one can occur. Such an “injection fusion” causes an undesired excessive amount of injected fuel, worsening both fuel consumption and particulate emissions. In order to avoid this phenomenon, lower limits to the dwell-time values are introduced in the control unit maps by a conservatively overestimated threshold, which reduces the flexibility of multiple-injection management. The injection fusion occurrence is mainly related to the time delay between the electrical signal to the solenoid and the nozzle opening and closure. The dwell-time fusion threshold was found to strongly decrease particularly with the nozzle closure delay. A functional dependence of the nozzle opening and closure delays on the solenoid energizing time and nominal rail pressure was experimentally assessed, and the injection temporal duration was correlated to the energizing time and rail pressure. A multijet CR injection-system mathematical model that was previously developed, including thermodynamics of liquids, fluid dynamics, mechanics of subsystems, and electromagnetism equations, was applied to better understand the cause and effect relationships for nozzle opening and closure delays. In particular, numerical results on the time histories of delivery- and control-chamber pressures, pilot- and needle-valve lifts, and mass flow rates through Z and A holes were obtained and analyzed to highlight the dependence of nozzle opening and closure delays on injector geometric features, physical variables, and valve dynamics. The nozzle closure delay was shown to strongly depend on the needle dynamics. Parametric numerical tests were carried out to identify configurations useful for minimizing the nozzle closure delay. Based on the results of these tests, a modified version of a commercial electroinjector was built, so as to achieve effectively lower nozzle closure delays and very close sequential injections without any fusion between them.
    keyword(s): Pressure , Flow (Dynamics) , Fuels , Ejectors , Nozzles , needles , Rails , Solenoids , Valves AND Equations ,
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      Numerical-Experimental Study and Solutions to Reduce the Dwell-Time Threshold for Fusion-Free Consecutive Injections in a Multijet Solenoid-Type CR System

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    https://yetl.yabesh.ir/yetl1/handle/yetl/140517
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorAndrea E. Catania
    contributor authorAlessandro Ferrari
    contributor authorEzio Spessa
    date accessioned2017-05-09T00:32:45Z
    date available2017-05-09T00:32:45Z
    date copyrightMarch, 2009
    date issued2009
    identifier issn1528-8919
    identifier otherJETPEZ-27059#022804_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/140517
    description abstractIn “multijet” common rail (CR) diesel injection systems, when two consecutive injection current pulses approach each other, a merging of the two injections into a single one can occur. Such an “injection fusion” causes an undesired excessive amount of injected fuel, worsening both fuel consumption and particulate emissions. In order to avoid this phenomenon, lower limits to the dwell-time values are introduced in the control unit maps by a conservatively overestimated threshold, which reduces the flexibility of multiple-injection management. The injection fusion occurrence is mainly related to the time delay between the electrical signal to the solenoid and the nozzle opening and closure. The dwell-time fusion threshold was found to strongly decrease particularly with the nozzle closure delay. A functional dependence of the nozzle opening and closure delays on the solenoid energizing time and nominal rail pressure was experimentally assessed, and the injection temporal duration was correlated to the energizing time and rail pressure. A multijet CR injection-system mathematical model that was previously developed, including thermodynamics of liquids, fluid dynamics, mechanics of subsystems, and electromagnetism equations, was applied to better understand the cause and effect relationships for nozzle opening and closure delays. In particular, numerical results on the time histories of delivery- and control-chamber pressures, pilot- and needle-valve lifts, and mass flow rates through Z and A holes were obtained and analyzed to highlight the dependence of nozzle opening and closure delays on injector geometric features, physical variables, and valve dynamics. The nozzle closure delay was shown to strongly depend on the needle dynamics. Parametric numerical tests were carried out to identify configurations useful for minimizing the nozzle closure delay. Based on the results of these tests, a modified version of a commercial electroinjector was built, so as to achieve effectively lower nozzle closure delays and very close sequential injections without any fusion between them.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical-Experimental Study and Solutions to Reduce the Dwell-Time Threshold for Fusion-Free Consecutive Injections in a Multijet Solenoid-Type CR System
    typeJournal Paper
    journal volume131
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2938394
    journal fristpage22804
    identifier eissn0742-4795
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsFuels
    keywordsEjectors
    keywordsNozzles
    keywordsneedles
    keywordsRails
    keywordsSolenoids
    keywordsValves AND Equations
    treeJournal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 002
    contenttypeFulltext
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