Propellant with pattern-controlled burn rate

US11112222B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11112222-B2
Application numberUS-202016748068-A
CountryUS
Kind codeB2
Filing dateJan 21, 2020
Priority dateJan 21, 2019
Publication dateSep 7, 2021
Grant dateSep 7, 2021

How to read this patent

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

A propellant is made from a flexible sheet that in some examples is nitrocellulose. An ignitable material is deposited on one side of the flexible sheet. The ignitable material is a series of triangles having a base adjacent to one edge of the sheet, and an apex adjacent to the other side of the sheet. Some examples of the ignitable material may be thermite compositions. The flexible sheet is rolled around a nonburnable tube and placed within a firearm casing, with the triangle bases being adjacent to the back of the casing, and the triangle apexes being adjacent to the front of the casing. The nonburnable tube is disposed over the primer pocket, so that ignition products from the primer travel through the tube, igniting the propellant adjacent to the front of the casing.

First claim

Opening claim text (preview).

What is claimed is: 1. A propellant, comprising a flexible sheet defining a first surface, a first edge, and a second edge, the flexible sheet being burnable or explosive, the flexible sheet having an ignitable material deposited thereon, the imitable material being deposited in a pattern, the pattern defining at least one covered sheet portion upon which ignitable material has been deposited and at least one uncovered sheet portion upon which ignitable material is not present, the covered and uncovered sheet portions being predetermined to provide a changing ignition rate. 2. The propellant according to claim 1 , wherein the flexible sheet is made from nitrocellulose. 3. The propellant according to claim 1 , wherein the ignitable material includes a metal oxide and a reducing metal. 4. The propellant according to claim 3 , wherein the metal oxide and reducing metal are present as alternating layers. 5. The propellant according to claim 4 , wherein the metal oxide is cupric oxide, and the reducing metal is magnesium. 6. The propellant according to claim 1 : further comprising a nonbumable tube; and the flexible sheet being rolled around the nonbumable tube. 7. The propellant according to claim 1 , wherein the pattern includes at least one triangular covered sheet portion. 8. The propellant according to claim 1 , wherein the flexible sheet comprises a polymer layer. 9. The propellant according to claim 8 , wherein the flexible sheet further comprises a reactive metal layer disposed between a pair of passivation layers. 10. A propellant, comprising a flexible sheet defining a first surface, a first edge, and a second edge, the flexible sheet having an ignitable material deposited thereon, the ignitable material being deposited in a pattern, the pattern defining at least one covered sheet portion upon which ignitable material has been deposited and at least one uncovered sheet portion upon which ignitable material is not present, the covered and uncovered sheet portions being predetermined to provide a predetermined ignition rate or a predetermined pressure curve within a pressure vessel; wherein the pattern includes a series of triangular covered portions, each covered portion defining a base adjacent to the first edge, and an apex adjacent to the second edge. 11. A propellant, comprising a flexible sheet defining a first surface, a second surface, a first edge, and a second edge, the flexible sheet having an ignitable material deposited on the first surface, the ignitable material being deposited in a pattern, the pattern defining at least one covered sheet portion upon which ignitable material has been deposited and at least one uncovered sheet portion upon which ignitable material is not present, the covered and uncovered sheet portions being predetermined to provide a predetermined ignition rate or a predetermined pressure curve within a pressure vessel; and further comprising boron deposited on the second surface. 12. The propellant according to claim 11 , further comprising an adhesion layer deposited between the second surface and the boron. 13. A propellant, comprising: a flexible sheet defining a first surface, a second surface, a first edge, and a second edge, the flexible sheet having an ignitable material deposited on the first surface, the ignitable material being deposited in a pattern, the pattern defining at least one covered sheet portion upon which ignitable material has been deposited and at least one uncovered sheet portion upon which ignitable material is not present, the covered and uncovered sheet portions being predetermined to provide a predetermined ignition rate or a predetermined pressure curve within a pressure vessel; boron deposited on the second surface; and a capping layer deposited on the boron. 14. A firearm cartridge, comprising: a casing, the casing having a side wall, an interior portion within the side wall, an open front end, a back end, a primer pocket defined within the back end, and a flash hole defined between the primer pocket and the interior portion; a propellant, comprising a flexible sheet defining a first surface, a first edge, and a second edge, the flexible sheet having an ignitable material deposited thereon, the ignitable material being deposited in a pattern, the pattern defining at least one covered sheet portion upon which ignitable material has been deposited and at least one uncovered sheet portion upon which ignitable material is not present, the covered and uncovered sheet portions being predetermined to provide a predetermined ignition rate or a predetermined pressure curve within a pressure vessel; a nonburnable tube defining a pair of ends and a passageway therebetween; the flexible sheet being rolled around the nonburnable tube; the propellant being disposed within the interior portion of the casing, the first edge of the flexible sheet being adjacent to the back end of the casing, the second edge of the flexible sheet being adjacent to the front end of the casing, one end of the nonburnable tube being disposed over the flash hole, with the flash hole being in communication with the passageway. 15. The firearm cartridge according to claim 14 , wherein the flexible sheet is made from nitrocellulose. 16. The firearm cartridge according to claim 14 , wherein the ignitable material includes a metal oxide and a reducing metal. 17. The firearm cartridge according to claim 16 , wherein the metal oxide and reducing metal are present as alternating layers. 18. The firearm cartridge according to claim 17 , wherein the metal oxide is cupric oxide, and the reducing metal is magnesium. 19. The firearm cartridge according to claim 14 , wherein the pattern includes at least one triangular covered sheet portion. 20. A firearm cartridge comprising: a casing, the casing having a side wall, an interior portion within the side wall, an open front end, a back end, a primer pocket defined within the back end, and a flash hole defined between the primer pocket and the interior portion; a propellant, comprising a flexible sheet defining a first surface, a first edge, and a second edge, the flexible sheet having an ignitable material deposited thereon, the ignitable material being deposited in a pattern, the pattern defining at least one covered sheet portion upon which ignitable material has been deposited and at least one uncovered sheet portion upon which ignitable material is not present, the covered and uncovered sheet portions being predetermined to provide a predetermined ignition rate or a predetermined pressure curve within a pressure vessel, wherein the pattern includes a series of triangular covered portions, each covered portion defining a base adjacent to the first edge, and an apex adjacent to the second edge; a nonbumable tube defining a pair of ends and a passageway therebetween; the flexible sheet being rolled around the nonburnable tube; and the propellant being disposed within the interior portion of the casing, the first edge of the flexible sheet being adjacent to the back end of the casing, the second edge of the flexible sheet being adjacent to the front end of the casing, one end of the nonburnable tube being disposed over the flash hole, with the flash hole being in communication with the passageway. 21. A firearm cartridge, comprising: a casing, the casing having a side wall, an interior portion within the side wall, an open front end, a back end, a primer pocket defined within the back end, and a flash hole defined between the

Assignees

Inventors

Classifications

  • characterised by the particular configuration of the transmission channels from the priming energy source to the charge to be ignited, e.g. multiple channels, nozzles, diaphragms or filters · CPC title

  • F42B5/16Primary

    characterised by composition or physical dimensions or form of propellant charge, {with or without projectile,} or powder (chemical composition C06B; {F42B5/24 takes precedence}) · CPC title

  • having contiguous layers or zones · CPC title

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What does patent US11112222B2 cover?
A propellant is made from a flexible sheet that in some examples is nitrocellulose. An ignitable material is deposited on one side of the flexible sheet. The ignitable material is a series of triangles having a base adjacent to one edge of the sheet, and an apex adjacent to the other side of the sheet. Some examples of the ignitable material may be thermite compositions. The flexible sheet is r…
Who is the assignee on this patent?
Spectre Mat Sciences Inc, Univ Of Central Florida Research Foundation, Univ Central Florida Res Found Inc
What technology area does this patent fall under?
Primary CPC classification F42B5/16. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Sep 07 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).