Ozone Assisted Combustion—Part I: Literature Review and Kinetic Study Using Detailed n Heptane Kinetic MechanismSource: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 009::page 91507DOI: 10.1115/1.4027068Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In this first paper, the authors undertake a review of the literature in the field of ozoneassisted combustion in order to summarize literature findings. The use of a detailed nheptane combustion model including ozone kinetics helps analyze these earlier results and leads into experimentation within the authors' laboratory using a singlecylinder, directinjection compression ignition engine, briefly discussed here and in more depth in a following paper. The literature and kinetic modeling outcomes indicate that the addition of ozone leads to a decrease in ignition delay, both in comparison to no added ozone and with a decreasing equivalence ratio. This ignition delay decrease as the mixture leans is counter to the traditional increase in ignition delay with decreasing equivalence ratio. Moreover, the inclusion of ozone results in slightly higher temperatures in the cylinder due to ozone decomposition, augmented production of nitrogen oxides, and reduction in particulate matter through radial atomic oxygen chemistry. Of additional importance, acetylene levels decrease but carbon monoxide emissions are found to both increase and decrease as a function of equivalence ratio. This work illustrates that, beyond a certain level of assistance (approximately 20 ppm for the compression ratio of the authors' engine), adding more ozone has a negligible influence on combustion and emissions. This occurs because the introduction of O3 into the intake causes a temperaturelimited equilibrium set of reactions via the atomic oxygen radical produced.
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| contributor author | Depcik, Christopher | |
| contributor author | Mangus, Michael | |
| contributor author | Ragone, Colter | |
| date accessioned | 2017-05-09T01:07:52Z | |
| date available | 2017-05-09T01:07:52Z | |
| date issued | 2014 | |
| identifier issn | 1528-8919 | |
| identifier other | gtp_136_09_091507.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/154784 | |
| description abstract | In this first paper, the authors undertake a review of the literature in the field of ozoneassisted combustion in order to summarize literature findings. The use of a detailed nheptane combustion model including ozone kinetics helps analyze these earlier results and leads into experimentation within the authors' laboratory using a singlecylinder, directinjection compression ignition engine, briefly discussed here and in more depth in a following paper. The literature and kinetic modeling outcomes indicate that the addition of ozone leads to a decrease in ignition delay, both in comparison to no added ozone and with a decreasing equivalence ratio. This ignition delay decrease as the mixture leans is counter to the traditional increase in ignition delay with decreasing equivalence ratio. Moreover, the inclusion of ozone results in slightly higher temperatures in the cylinder due to ozone decomposition, augmented production of nitrogen oxides, and reduction in particulate matter through radial atomic oxygen chemistry. Of additional importance, acetylene levels decrease but carbon monoxide emissions are found to both increase and decrease as a function of equivalence ratio. This work illustrates that, beyond a certain level of assistance (approximately 20 ppm for the compression ratio of the authors' engine), adding more ozone has a negligible influence on combustion and emissions. This occurs because the introduction of O3 into the intake causes a temperaturelimited equilibrium set of reactions via the atomic oxygen radical produced. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Ozone Assisted Combustion—Part I: Literature Review and Kinetic Study Using Detailed n Heptane Kinetic Mechanism | |
| type | Journal Paper | |
| journal volume | 136 | |
| journal issue | 9 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4027068 | |
| journal fristpage | 91507 | |
| journal lastpage | 91507 | |
| identifier eissn | 0742-4795 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 009 | |
| contenttype | Fulltext |