Electrodes for multi-point ignition using single or multiple transient plasma discharges

Patent metadata

Field	Value
Publication number	US-9377002-B2
Application number	US-201414185729-A
Country	US
Kind code	B2
Filing date	Feb 20, 2014
Priority date	Feb 20, 2013
Publication date	Jun 28, 2016
Grant date	Jun 28, 2016

Abstract

A device for providing ignition of a fuel-air mixture using a transient plasma discharge is provided. The device includes an anode coupled to receive a voltage; and a cathode disposed in proximity to the anode and coupled to a ground, wherein at least one of the anode and the cathode includes a protrusion that enhances an electric field formed between the anode and the cathode, the protrusion forming a sharp edge defining a plurality of points, each point forming a path of shortest distance between the anode and the cathode.

First claim

The invention claimed is:

1. A device for providing ignition of a fuel-air mixture using a transient plasma discharge, the device comprising:
an anode configured to receive a voltage;
a cathode disposed in proximity to the anode and configured to be coupled to a ground, wherein at least one of the anode and the cathode comprises a protrusion that enhances an electric field formed between the anode and the cathode, and wherein the protrusion forms a sharp edge defining a plurality of points, each point forming a path of shortest distance between the anode and the cathode; and
a pulse generator that generates a pulse having a duration of no more than a few nanoseconds and that applies this pulse across the anode and cathode so as to cause a near simultaneous transient plasma discharge between the anode and each of a plurality of the points on the cathode.

2. The device of claim 1 , wherein the anode is disposed in a longitudinal axis, the cathode is disposed around the anode, and the protrusion comprises a sharp edge formed in the anode.

3. The device of claim 2 , wherein the anode comprises a disc shape perpendicular to the longitudinal axis, the sharp edge is the perimeter of the disc, and the cathode is axi-symmetrically disposed around the anode.

4. The device of claim 3 , wherein the disc shape has a diameter matched to an inner diameter of the cathode.

5. The device of claim 2 , wherein the protrusion is one of a plurality of anode protrusions formed symmetrically around the longitudinal axis.

6. The device of claim 1 , wherein the anode is disposed in a longitudinal axis, the cathode is disposed around the anode, and the protrusion is one of a plurality of cathode protrusions formed symmetrically around the anode.

7. The device of claim 1 , wherein the anode is disposed in a longitudinal axis, the cathode extends around the anode, and the cathode includes apertures that allow a uniform plasma distribution around the anode, for ignition.

8. An internal combustion engine comprising:
a fuel injector and an air intake coupled to provide a fuel-air mixture;
a cavity configured to contain a combustion, the cavity comprising:
an internal surface fixed to the engine;
a piston;
an anode configured to receive a voltage;
a cathode disposed in proximity to the anode, the cathode configured to be coupled to a ground, wherein at least one of the anode and the cathode comprises a protrusion that enhances an electric field formed between the anode and the cathode, and wherein the protrusion forms a sharp edge defining a plurality of points, each point forming a path of shortest distance between the anode and the cathode; and
a pulse generator that generates a pulse having a duration of no more than a few nanoseconds and that applies this pulse across the anode and cathode so as to cause a near simultaneous transient plasma discharge between the anode and each of a plurality of the points on the cathode.

9. The internal combustion engine of claim 8 , wherein the cathode comprises the protrusion, the protrusion formed on a surface of the piston limiting an interior portion of the cavity.

10. The internal combustion engine of claim 8 , wherein the cathode comprises the protrusion, and the protrusion is formed on the internal surface fixed to the engine.

11. The internal combustion engine of claim 8 , wherein the cathode comprises an internal component protruding into the cavity, the internal component comprising the protrusion.

12. The internal combustion engine of claim 8 , further comprising an insulator surrounding the anode, to prevent electric breakdown at places not including the plurality of points defined by the sharp edge.

13. The internal combustion engine of claim 8 , wherein the anode is disposed in a longitudinal axis, the cathode is disposed around the anode, and the protrusion comprises a sharp edge formed in the anode.

14. The internal combustion engine of claim 13 , wherein the anode comprises a disc shape perpendicular to the longitudinal axis, the sharp edge is the perimeter of the disc, and the cathode is axi-symmetrically disposed around the anode.

15. The internal combustion engine of claim 13 , wherein the protrusion is one of a plurality of anode protrusions formed symmetrically around the longitudinal axis.

16. A method for igniting a fuel-air mixture with a transient plasma discharge, the method comprising:
forming a fuel-air mixture by combining an approximately stoichiometric amount of a fuel with air;
delivering the fuel-air mixture to a cavity having an anode and a cathode proximal to each other; and
providing a voltage pulse to the anode having a duration of no more than a few nanoseconds, wherein at least one of the anode and the cathode comprises a protrusion that enhances an electric field formed between the anode and the cathode, and the protrusion forms a sharp edge defining a plurality of points,
each point forming a path of shortest distance between the anode and the cathode,
wherein the pulse causes a near simultaneous transient plasma discharge between the anode or cathode and each of a plurality of the points.

17. The method of claim 16 , wherein providing a voltage pulse to the anode comprises providing a voltage of about 1 kV to about 100 kV to the anode.

18. The method of claim 16 , further comprising forming a transient plasma including radicals between a point in the anode and a point in the cathode, at least one of the points in the anode and the cathode being a point in the protrusion.

19. The method of claim 16 , wherein forming a fuel-air mixture with a fuel-to-air equivalence ratio slightly above one.

Assignees

• Singleton Daniel R
• Gundersen Martin A
• Sanders Jason M
• Kuthi Andras
• Univ Southern California

Inventors

• Singleton Daniel R
• Gundersen Martin A
• Sanders Jason M
• Kuthi Andras

Classifications

• H05H1/48

  using an arc (H05H1/26 takes precedence) · CPC title

• F02P23/04

  Other physical ignition means, e.g. using laser rays · CPC title

• F02P15/08

  having multiple-spark ignition, i.e. ignition occurring simultaneously at different places in one engine cylinder or in two or more separate engine cylinders · CPC title

• F02P15/04 Primary

  one of the spark electrodes being mounted on the engine working piston · CPC title

• H01T13/24

  having movable electrodes (H01T13/28 takes precedence) · CPC title