IP Library Granted Patent US 7,930,976
Granted Patent B2
US 7,930,976 · App. 11/832,845 · Granted Apr 26, 2011

Slow burning, gasless heating elements

Assignee: Ensign-Bickford Aerospace & Defense Company
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Quick Facts
Patent No.
US 7,930,976
App. No.
11/832,845
Granted
Apr 26, 2011
Kind
B2
Abstract

A structure includes a substrate of a first material and a second material coating at least a portion of the substrate, where the second material is different from the first material, where the first and second materials, upon being thermally energized, react with each other in an exothermic and self-sustaining alloying reaction that propagates from a first location within the structure along a travel path to a second location within the structure at a rate that depends upon one or more characteristics of the first and second materials.

Claims (7)

1. An initiation system, comprising: an initiator device; and a structure that includes a substrate comprised of a first material, wherein said substrate is in the form of a mesh or a foam; and a second material coating at least a portion of the substrate, where the second material is different from the first material; wherein the first and second materials, upon being thermally energized by the initiator device, react with each other in an exothermic and self-sustaining alloying reaction that propagates from a first location within the structure along a travel path to a second location within the structure and at a rate that depends upon one or more characteristics of the substrate and the coating.

2. The system of claim 1 , where the first material comprises aluminum and the second material comprises nickel.

3. The system of claim 1 , where the first and/or second materials are from the group that comprises aluminum, boron, carbon, silicon, zirconium, iron, copper, beryllium, tungsten, hafnium, antimony, magnesium, molybdenum, zinc, tin, nickel, palladium, phosphorus, sulfur, tantalum, manganese, cobalt, chromium, or vanadium.

4. The system of claim 1 , further comprising a second substrate that is an insulating material.

5. The system of claim 1 , where the first and/or second materials further comprise a material from the group that comprises glycidyl azide polymer, polyoxetanes, or polyglycidyl nitrate.

6. The system of claim 1 , where the first and/or second materials further comprise a material from the group that comprises hydroxy teiminated polybutadiene, hydroxy terminated polyether, carboxy terminated polybutadiene, polyether, polycaprolactone, or polyvinyl chloride.

7. An initiation system, comprising: an initiator device; and a structure that includes a substrate comprised of a first material arranged in a non-uniform and varying distribution of mass of the first material along a length of the substrate in a propagation direction; and a second material coating at least a portion of the substrate, where the second material is different from the first material; wherein the first and second materials, upon being thermally energized by the initiator device, react with each other in an exothermic and self-sustaining alloying reaction that propagates from a first location within the structure along a travel path to a second location within the structure at a rate that depends upon one or more characteristics of the substrate, where a physical configuration of the substrate includes one or more different directions of the first material at one or more points along the travel path.

Assignments (2)
CONFIRMATORY LICENSE Recorded Aug 4, 2016
From: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
To: THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY
Reel/Frame 039571/0575 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 21, 2007
From: KELLETT, RICHARD M.; MALLERY, CARL F., JR.; KORCSMAROS, ROBERT B.
To: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
Reel/Frame 019724/0018 →
Continuity (1)
Related Publication 20090031911A1 · Feb 5, 2009