IP Library › Granted Patent US 10,259,756
Granted Patent B2
US 10,259,756 · App. 15/057,510 · Granted Apr 16, 2019

Solid propellant with integral electrodes, and method

Inventors: Jeremy C. Danforth (Tucson, AZ); Matt H. Summers (Marana, AZ); David G. Garrett (Tucson, AZ)
Assignee: Raytheon Company
C06B21/0075B05B7/22F02C3/28F02K9/08F02K9/28F02K9/94F02K9/95F05D2230/31
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Quick Facts
Patent No.
US 10,259,756
App. No.
15/057,510
Granted
Apr 16, 2019
Kind
B2
Abstract

A device may include an electrically-operated propellant or energetic gas-generating material, additively manufactured together with electrodes for producing a reaction in the material. The device may also include a casing that is additively manufactured with the other components. The additive manufacturing may be accomplished by extruding or otherwise depositing raw materials for the different components where desired. The electrodes may be made of a conductive polymer material, for example using an electrically-conductive fill in a polymer.

Claims (20)

1. A method of making a gas-producing device, the method comprising:

in a single additive manufacturing process:

forming electrodes; and

forming electrically-controlled solid propellant material in contact with and operatively coupled to the electrodes.

2. The method of claim 1 , wherein the single additive manufacturing process further includes forming a casing around the electrodes and the electrically-controlled solid propellant material.

3. The method of claim 1 , further comprising inserting the electrodes and the electrically-controlled solid propellant material into a pre-formed casing.

4. The method of claim 1 , wherein the forming the electrically-controlled solid propellant material includes forming the electrically-controlled solid propellant materials between adjacent pairs of electrodes.

5. The method of claim 1 ,

wherein the forming the electrodes includes forming multiple adjacent pairs of electrodes; and

wherein the forming the electrically-controlled solid propellant material includes forming the electrically-controlled solid propellant materials between the adjacent pairs of electrodes.

6. The method of claim 1 , wherein the forming the electrodes includes forming multiple plate electrodes with the electrically-controlled solid propellant material between adjacent of the plate electrodes.

7. The method of claim 6 , wherein the plate electrodes are parallel to one another.

8. The method of claim 1 , wherein the forming the electrodes includes forming multiple annular electrodes with the electrically-controlled solid propellant material between adjacent of the annular electrodes.

9. The method of claim 1 ,

wherein the forming the electrodes includes extruding electrically-conductive material; and

wherein the forming the electrically-controlled solid propellant material includes extruding the electrically-controlled solid propellant material.

10. The method of claim 9 , wherein the electrically-conductive material is an electrically-conductive polymer material.

11. The method of claim 10 , wherein the electrically-conductive polymer material includes a conductive material fill, such as conductive fibers and/or conductive powder.

12. The method of claim 10 , wherein the extruding of the electrically-conductive material and the extruding the electrically-controlled solid propellant material includes extruding from separate respective nozzles.

13. The method of claim 1 , wherein the additive manufacturing includes building up the device layer by layer, placing the electrically-controlled solid propellant material and electrically-conductive electrode material for one layer before moving on to a next layer.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 1, 2016
From: DANFORTH, JEREMY C.; SUMMERS, MATT H.; GARRETT, DAVID G.
To: RAYTHEON COMPANY
Reel/Frame 037863/0264 →
Continuity (1)
Related Publication 20170253536A1 · Sep 7, 2017
Cited By (1)
US 12,631,156