Characterization of Transient Plasma Ignition Flame Kernel Growth for Varying Inlet Conditions

Abstract

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 break through 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.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 2009
Accession Number
ADA514183

Entities

People

  • Neil C. Hawkes

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acquisition
  • Chemical Reaction Properties
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Combustors
  • Data Acquisition
  • Exothermic Reactions
  • Gas Turbines
  • Ignition
  • Ignition Lag
  • Ignition Systems
  • Internal Combustion Engines
  • Subsonic Combustion
  • Turbines
  • Turbojet Engines

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.
  • Rocket Propulsion.

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems