Miniature railgun engine ignitor
AssigneeBoard of Regents, The University of Texas System
InventorsRonald D. Matthews, Steven P. Nichols, William F. Weldon, Mark M. Koeroghlian, Richard W. Faidley
Life of this patent
Estimating the term…
Abstract
A plasma ignitor system capable of injecting a high energy plasma jet into a combustion chamber of an internal combustion engine or continuous combustion system. The plasma ignitor features a high energy current pulse source and a geometrically configured coaxial, dual-rail or three-rail ignitor system for deeper and more accurate injection of plasma into a combustion chamber of either large or small dimension.
Claims59
A railgun ignition device for generating and injecting a high energy plasma jet into a combustion chamber, comprising:
- a holding plug including means for mounting said railgun ignition device in a utilization apparatus;
- first and second spaced part electrodes extending along a central axis and defining a bore having a muzzle end and a plasma initiation end, said first electrode being electrically insulated from said holding plug, said bore having a width equal to a spacing between said first and second electrodes at said muzzle end and a length equal to a distance between said muzzle end and said plasma initiation end, an aspect ratio of said bore being at least 3:1;
- and
- an electrical connection between said second electrode and said holding plug, said plasma initiation end being between said electrical connection and said muzzle end.
A combustion system comprising:
- at least one combustion chamber;
- at least one railplug connected to each combustion chamber, each railplug including:
- a holding plug including means for connecting said railplug to a respective combustion chamber,
- first and second spaced part electrodes along a central axis together defining a bore having a muzzle end disposed within said respective combustion chamber, and a plasma initiation end, said first electrode being electrically insulated from said holding plug, a length of said bore being equal to a distance between said muzzle end and said plasma initiation end and a width of said bore being equal to a spacing between said first and second electrodes at said muzzle end, an aspect ratio of said bore being at least 3:1,
- an electrical connection between said second electrode and said holding plug, said plasma initiation end being between said electrical connection and said muzzle end;
- and
- a power source for supplying pulsed electrical energy to each railplug.
An internal combustion engine for rotating a crankshaft, comprising:
- at least one combustion chamber;
- at least one railplug connected to each combustion chamber, each railplug including:
- a holding plug including means for connecting said railplug to a respective combustion chamber,
- first and second spaced part electrodes, said first electrode being electrically insulated from said holding plug, said electrodes extending along an axis and defining a bore having a plasma initiation end and a muzzle end, a ratio of a length of said bore to a distance between said electrodes being at least 3:1,
- an electrical connection between said second electrode and said holding plug, said plasma initiation end being between said electrical connection and said muzzle end;
- and
- pulse generating means, timed by said crankshaft, for applying timed electrical energy pulses to said electrodes of each railplug.
A continuous combustion engine comprising:
- at least one continuous combustion chamber;
- at least one railplug connected to each continuous combustion chamber, each railplug including:
- a holding plug including means for connecting said railplug to a respective continuous combustion chamber,
- first and second spaced part electrodes, said first electrode being electrically insulated from said holding plug, said electrodes extending along an axis and defining a bore having a plasma initiation end and a muzzle end, a ratio of a length of said bore to a distance between said electrodes being at least 3:1,
- an electrical connection between said second electrode and said holding plug, said plasma initiation end being between said electrical connection and said muzzle end;
- and
- a power source for applying at least one electrical energy pulse to said electrodes of each railplug.
An ignition device for generating and injecting a high energy plasma jet into a combustion chamber, comprising:
- a holding plug including means for mounting said ignition device in a utilization apparatus;
- and
- first and second spaced apart electrodes, at least one of said electrodes extending helically around a central axis, said electrodes defining a bore having a muzzle end and a plasma initiation end, a bore width being equal to a distance between said first and second spaced apart electrodes, and a bore length being equal to a distance between said muzzle end and said plasma initiation end of said bore, an aspect ratio of said bore being at least 3:1;
- and
- an electrical connection between one of said first and second spaced apart electrodes and said holding plug, said plasma initiation end being between said electrical connection and said muzzle end.
Dependencies are inferred from the claim text.