Debris-free combustible aerial shell

• US 10,267,606 B2
• Filed: 08/24/2017
• Issued: 04/23/2019
• Est. Priority Date: 08/24/2017
• Status: Active Grant

• Current Assignee: DMD Systems, LLC
• Original Assignee: DMD Systems, LLC
• Inventors: Naud, Darren, Thomas, John David
• Primary Examiner(s): Bergin, James S
• Application Number:
  US15/685,835
• Publication Number:
  US 20190063886A1
• Time in Patent Office: 607 Days
• Field of Search: 102335, 102352, 102360, 102361
• CPC Class Codes: F42B 4/00 Fireworks, i.e. pyrotechnic devices for amusement, display, illumination or signal purposes signalling by explosives G08B; advertising by fireworks G09F13/46; signalling by pyrotechnics in railway systems B61L5/20
• CPC Class Codes: F42B 4/02 in cartridge form, i.e. shell, propellant and primer
• CPC Class Codes: F42B 4/06 Aerial display rockets rockets in general F42B15/00
• CPC Class Codes: F42B 4/24 characterised by having plural successively-ignited charges in aerial display rockets F42B4/14
• CPC Class Codes: F42B 4/30 Manufacture

Abstract

A pyrotechnic projectile including an aerial shell, the aerial shell including at least one combustible layer of material; the at least one layer surrounding and containing at least one pyrotechnic effect and a dispersive explosive charge; the at least one combustible layer including a combustible material configured to burn substantially throughout the at least one layer; and wherein the at least one combustible layer is configured to burn through a thickness at a preselected rate to thereby ignite the dispersive explosive charge.

Claims

1. A pyrotechnic projectile comprising:

an aerial shell comprising at least one combustible layer of material, the at least one combustible layer comprising an outermost combustible layer surrounding the at least one combustible layer, the outermost combustible layer configured to ignite on substantially an entire outer surface, the outermost combustible layer comprising a relatively higher combustion rate than the at least one combustible layer;

the at least one combustible layer surrounding and containing at least one pyrotechnic effect and a dispersive explosive charge;

the at least one combustible layer comprising a combustible material configured to burn substantially throughout the at least one combustible layer; and

wherein the at least one combustible layer is configured to burn through a thickness at a preselected rate to thereby ignite the dispersive explosive charge.

2. The pyrotechnic projectile of claim 1, wherein the aerial shell is configured to be launched from a launcher by combustion of a lift charge within the launcher, wherein the aerial shell comprises a shape such that outer edge portions of the shape substantially mate with inner walls of the launcher.

3. The pyrotechnic projectile of claim 2, wherein the aerial shell is configured to ignite the dispersive explosive charge at a predetermined altitude following the launch.

4. The pyrotechnic projectile of claim 2, wherein the outermost combustible layer is configured to be ignited by combustion of the lift charge to thereby subsequently ignite the at least one combustible layer.

5. The pyrotechnic projectile of claim 4, wherein the outermost combustible layer is configured to have a combustion rate of from about 5 to about 50 times greater than the at least one combustible layer.

6. The pyrotechnic projectile of claim 1, wherein the at least one combustible layer further comprises a support combustible layer adjacent to the dispersive explosive charge.

7. The pyrotechnic projectile of claim 1, wherein the aerial shell comprises one or more of ammonium nitrates, metal nitrates, perchlorates, phosphates, carbonates, aminotetrazoles, arsenites, oxalates, oxychlorides, peroxides, oxides, sulphates, fluorides, and metal powders.

8. The pyrotechnic projectile of claim 1, wherein the aerial shell comprises one more of metal fuels, magnesium, aluminum, silicon, calcium, iron, titanium, zinc, and alloys thereof.

9. The pyrotechnic projectile of claim 1, wherein the aerial shell comprises one or more of non-metal fuels, charcoal, sulfur, boron, hexamine, nitroguanidine, dextrin, camphor, red gum benzoic acid, nitrocellulose, and cellulose.

10. The pyrotechnic projectile of claim 1, wherein the aerial shell comprises one or more of Mg, Sr, Ti, Cl, metal colorants, Sr(NO)3, SrCO3, PARLON™

, Ammonium Perchlorate (AP), hexachloroethane, paroils (chlorinated short-chain hydrocarbons) and polyvinylchloride (PVC).

11. The pyrotechnic projectile of claim 1, wherein the aerial shell comprises one or more of polyvinyl nitrate, nitrocellulose, polyvinyl chloride, polyvinyl acetate, chlorofluoroethylene, and polymers and copolymers thereof.

12. The pyrotechnic projectile of claim 1, wherein the aerial shell comprises one or more of thermosetting polymers, rubber, polybutadiene, polyurethane, furans, organic resins, acrylic resins, polyester resins, epoxy resins, vinyl, PARLON™

, and vinyl ester resins.

13. The pyrotechnic projectile of claim 1, wherein the outermost combustible layer is integral with the at least one combustible layer.

14. A method of forming a pyrotechnic projectile comprising:

forming an aerial shell comprising at least one combustible layer of material, said forming comprising forming an outermost combustible layer surrounding the at least one combustible layer, the outermost combustible layer formed to ignite to thereby subsequently ignite the at least one combustible layer on substantially an entire outer surface, the outermost combustible layer comprising a relatively higher combustion rate than the at least one combustible layer;

forming the at least one combustible layer surrounding and containing at least one pyrotechnic effect and a dispersive explosive charge;

wherein the at least one combustible layer is formed to burn substantially throughout the at least one combustible layer; and

wherein the at least one combustible layer is configured to burn through a thickness at a preselected rate to thereby ignite the dispersive explosive charge.

15. The method of claim 14, wherein the aerial shell is formed to be launched from a launcher by combustion of a lift charge within the launcher to ignite the dispersive explosive charge at a predetermined altitude following the launch.

16. The method of claim 14, wherein the outermost combustible layer is formed to be ignited by combustion of the lift charge to thereby subsequently ignite the at least one combustible layer.

17. The method of claim 14, wherein the at least one combustible layer is formed by one or more of hot pressing, cold pressing, molding, 3D-printing, painting, dipping, and vapor deposition.

18. The method of claim 17, wherein the at least one combustible layer is formed in portions that may be glued together in a final shape to surround and contain the at least one pyrotechnic effect and a dispersive explosive charge.

19. The method of claim 14, wherein the aerial shell comprises one or more of ammonium nitrates, metal nitrates, perchlorates, phosphates, carbonates, aminotetrazoles, arsenites, oxalates, oxychlorides, peroxides, oxides, sulphates, fluorides, metal powders, metal fuels, magnesium, aluminum, silicon, calcium, iron, titanium, zinc, non-metal fuels, charcoal, sulfur, boron, hexamine, nitroguanidine, dextrin, camphor, red gum benzoic acid, nitrocellulose, cellulose, Sr(NO)3, SrCO3, PARLON™

, Ammonium Perchlorate (AP), hexachloroethane, paroils (chlorinated short-chain hydrocarbons) and polyvinylchloride (PVC).

20. The method of claim 14, wherein the aerial shell comprises one or more of polyvinyl nitrate, nitrocellulose, polyvinyl chloride, polyvinyl acetate, chlorofluoroethylene, rubber, polybutadiene, polyurethane, furans, organic resins, acrylic resins, polyester resins, epoxy resins, vinyl, PARLON™

, and vinyl ester resins.

21. The method of claim 14, wherein the outermost combustible layer is formed integral with the at least one combustible layer.