Characterization of transient plasma ignition flame kernel growth for varying inlet conditions

Approved for public release, distribution unlimited === Pulse detonation engines (PDEs) have the potential to significantly improve the efficiency of a variety of internal combustion engine designs. This efficiency improvement hinges on the ability of the engine to detonate fuel/air mixture through...

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Main Author: Hawkes, Neil C.
Other Authors: Brophy, Christopher M.
Published: Monterey, California. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/4427
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spelling ndltd-nps.edu-oai-calhoun.nps.edu-10945-44272014-12-04T04:08:42Z Characterization of transient plasma ignition flame kernel growth for varying inlet conditions Hawkes, Neil C. Brophy, Christopher M. Sinibaldi, Jose O. Naval Postgraduate School (U.S.) Approved for public release, distribution unlimited Pulse detonation engines (PDEs) have the potential to significantly improve the efficiency of a variety of internal combustion engine designs. This efficiency improvement hinges on the ability of the engine to detonate fuel/air mixture through deflagration-to-detonation transitions at 60 to 100 times a second. A major breakthrough in reducing the cycle time of a pulse detonation device is through the use of a Transient Plasma Ignition (TPI) system vice the normal Capacitive Discharge Ignition (CDI) system. The TPI system deposits an equivalent amount of energy as the CDI system but in a fraction of the time and over a larger combustor volume. The TPI also creates high quantities of OH due to the high density of energetic electrons produced by the TPI event. The combination of decreased energy deposition time, larger ignition volume, and a high density of free radicals reduces the flame kernel growth time, which in turn creates a choked flame condition more rapidly. This thesis characterized the flame kernel growth following a transient plasma ignition event for various combustor inlet configurations so as to better understand the flame patterns within the combustion chamber. High-speed images of the combustor were taken from a side profile and end view to observe the flame growth. Time from ignition event until initial flame kernel observation and from ignition event until fully developed flame were gathered from the images and plotted to find the most favorable inlet condition. 2012-03-14T17:41:51Z 2012-03-14T17:41:51Z 2009-12 Thesis http://hdl.handle.net/10945/4427 503114693 Monterey, California. Naval Postgraduate School
collection NDLTD
sources NDLTD
description Approved for public release, distribution unlimited === Pulse detonation engines (PDEs) have the potential to significantly improve the efficiency of a variety of internal combustion engine designs. This efficiency improvement hinges on the ability of the engine to detonate fuel/air mixture through deflagration-to-detonation transitions at 60 to 100 times a second. A major breakthrough in reducing the cycle time of a pulse detonation device is through the use of a Transient Plasma Ignition (TPI) system vice the normal Capacitive Discharge Ignition (CDI) system. The TPI system deposits an equivalent amount of energy as the CDI system but in a fraction of the time and over a larger combustor volume. The TPI also creates high quantities of OH due to the high density of energetic electrons produced by the TPI event. The combination of decreased energy deposition time, larger ignition volume, and a high density of free radicals reduces the flame kernel growth time, which in turn creates a choked flame condition more rapidly. This thesis characterized the flame kernel growth following a transient plasma ignition event for various combustor inlet configurations so as to better understand the flame patterns within the combustion chamber. High-speed images of the combustor were taken from a side profile and end view to observe the flame growth. Time from ignition event until initial flame kernel observation and from ignition event until fully developed flame were gathered from the images and plotted to find the most favorable inlet condition.
author2 Brophy, Christopher M.
author_facet Brophy, Christopher M.
Hawkes, Neil C.
author Hawkes, Neil C.
spellingShingle Hawkes, Neil C.
Characterization of transient plasma ignition flame kernel growth for varying inlet conditions
author_sort Hawkes, Neil C.
title Characterization of transient plasma ignition flame kernel growth for varying inlet conditions
title_short Characterization of transient plasma ignition flame kernel growth for varying inlet conditions
title_full Characterization of transient plasma ignition flame kernel growth for varying inlet conditions
title_fullStr Characterization of transient plasma ignition flame kernel growth for varying inlet conditions
title_full_unstemmed Characterization of transient plasma ignition flame kernel growth for varying inlet conditions
title_sort characterization of transient plasma ignition flame kernel growth for varying inlet conditions
publisher Monterey, California. Naval Postgraduate School
publishDate 2012
url http://hdl.handle.net/10945/4427
work_keys_str_mv AT hawkesneilc characterizationoftransientplasmaignitionflamekernelgrowthforvaryinginletconditions
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