IP Library Granted Patent US 7,025,001
Granted Patent B2
US 7,025,001 · App. 10/691,404 · Granted Apr 11, 2006

Super long range crash-bang round

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Quick Facts
Patent No.
US 7,025,001
App. No.
10/691,404
Granted
Apr 11, 2006
Kind
B2
Abstract

A “crash-bang” shotgun cartridge assembly has a projectile consisting of a weighty and frangible ballast on its leading edge, a flash-bang charge, and, in the rear, a delay fuse which is lit by the detonation of the propellant charge in the cartridge. The weight of the ballast insures greater stability in flight, and accuracy in targeting, thus extending the range of the crash-bang cartridge. In addition, the weighty and frangible ballast disintegrates into low mass, low energy (and therefore less-lethal) fragments when the flash charge detonates.

Claims (89)

1. A crash-bang cartridge assembly, comprising

a tubular cartridge; and

a projectile within said tubular cartridge, said projectile comprising:

a tubular projectile casing;

a delay block located at one end of the tubular projectile casing;

a delay fuse column within said delay block, said delay fuse column being at least partially filled with a delay fuse composition;

a flash charge within said projectile casing, said flash charge being ignited by said delay fuse composition; and

a weighty and frangible ballast located on a leading edge of said projectile, at an end of the tubular projectile casing opposite from the end having the delay block, wherein a weight of said ballast is sufficient to provide stability and accuracy in flight, and wherein the weighty and frangible ballast comprises a mixture of zinc powder and graphite powder;

wherein the mixture of zinc powder and graphite powder is sufficiently frangible that, after detonation of said flash charge, the mixture comprises low mass, low energy components.

2. The crash-bang cartridge assembly of claim 1 , wherein the low mass, low energy components comprising the weighty and frangible ballast after detonation are less likely to cause injury to any creature in a vicinity of said detonation.

3. The crash-bang cartridge assembly of claim 1 , wherein the delay fuse composition is consolidated.

4. The crash-bang cartridge assembly of claim 1 , wherein the weighty and frangible ballast is consolidated.

5. The crash-bang cartridge assembly of claim 4 , wherein the weighty and frangible ballast remains substantially within the end of the tubular projectile casing by means of said consolidation.

6. The crash-bang cartridge assembly of claim 1 , wherein the weighty and frangible ballast further comprises metallic particles.

7. The crash-bang cartridge assembly of claim 6 , wherein the metallic particles form a metallic powder.

8. The crash-bang cartridge assembly of claim 6 , wherein the weighty and frangible ballast is secured at the end of the tubular projectile casing by a wad.

9. The crash-bang cartridge assembly of claim 6 , wherein the tubular projectile casing comprises a cardboard tube, and wherein the end of the tubular projectile casing where the weighty and frangible ballast is located is sealed by an upper closure wad and the weighty and frangible ballast is sealed in by a lower closure wad in an inside portion of the tubular projectile casing.

10. The crash-bang cartridge assembly of claim 1 , wherein the tubular projectile casing forms a cup and the end of the tubular projectile casing where the weighty and frangible ballast is located forms a solid end of the cup, and wherein the weighty and frangible ballast is consolidated at said solid end of the cup by pressing a ram over the weighty and frangible ballast.

11. The crash-bang cartridge assembly of claim 1 , wherein the weighty and frangible ballast further comprises at least one of lead particles and tungsten particles.

12. The crash-bang cartridge assembly of claim 1 , wherein the ratio of zinc powder to graphite powder controls a degree of frangibility of the weighty and frangible ballast.

13. The crash-bang cartridge assembly of claim 1 , wherein the tubular projectile casing comprises at least one of aluminum, plastic, rubber, and cardboard.

14. The crash-bang cartridge assembly of claim 1 , wherein the projectile further comprises:

an obturator formed on an outer circumference of the tubular projectile casing.

15. The crash-bang cartridge assembly of claim 1 , wherein the projectile further comprises:

an igniter located at an end of the delay fuse composition and in proximity to the flash charge, said igniter is comprised of igniter composition, wherein said igniter is ignited by the delay fuse composition, and, in turn, ignites the flash charge.

16. The crash-bang cartridge assembly of claim 15 , wherein an end of the tubular cartridge opposite from said end of the tubular cartridge having the primer is crimped inward to seal the projectile within the tubular cartridge.

17. The crash-bang cartridge assembly of claim 1 , further comprising:

a primer at one end of said tubular cartridge;

propellant in said tubular cartridge for launching the projectile from said tubular cartridge, said propellant being ignited by said primer; and

a pressure wad between said propellant and said projectile.

18. The crash-bang cartridge assembly of claim 17 , further comprising:

a closure wad sealing the projectile within the tubular cartridge, wherein said crimping at least assists in keeping said closure wad in place.

19. A crash-bang projectile, said crash-bang projectile fitting within a crash-bang cartridge in order to form a crash-bang cartridge assembly, comprising

a tubular projectile casing;

a flash charge within said tubular projectile casing; and

a weighty and frangible ballast located on a leading edge of said crash-bang projectile, comprising:

a mixture of zinc powder and graphite powder;

wherein a weight of said ballast is sufficient to provide stability and accuracy in flight; and

wherein the weighty and frangible ballast is sufficiently frangible that, after detonation of said flash charge, the said ballast comprises low mass, low energy components.

20. The crash-bang projectile of claim 19 , wherein the low mass, low energy components comprising the weighty and frangible ballast after detonation are less likely to cause injury to any creature in a vicinity of said detonation.

21. The crash-bang projectile of claim 19 , further comprising:

a delay fuse composition at least partially filling a delay fuse column within a delay block located at one end of the tubular projectile casing, wherein said delay fuse composition ignites the flash charge.

22. The crash-bang projectile of claim 21 , further comprising:

an igniter located at an end of the delay fuse composition and in proximity to the flash charge, said igniter is comprised of igniter composition, wherein said igniter is ignited by the delay fuse composition, and, in turn, ignites the flash charge.

23. The crash-bang projectile of claim 19 , wherein the weighty and frangible ballast is consolidated.

24. The crash-bang projectile of claim 19 , wherein the tubular projectile casing forms a cup and the end of the tubular projectile casing where the weighty and frangible ballast is located forms a solid end of the cup, and wherein the weighty and frangible ballast is consolidated at said solid end of the cup by pressing a ram over the weighty and frangible ballast.

25. The crash-bang projectile of claim 19 , wherein the weighty and frangible ballast is secured at the end of the tubular projectile casing by a wad.

26. The crash-bang projectile of claim 19 , wherein the tabular projectile casing comprises a cardboard tube, and wherein the end of the tubular projectile casing where the weighty and frangible ballast is located is sealed by an upper closure wad and the weighty and frangible ballast is sealed in by a lower closure wad in an inside portion of the tubular projectile casing.

27. The crash-bang projectile of claim 19 , wherein the ratio of zinc powder to graphite powder controls a degree of frangibility of the weighty and frangible ballast.

28. The crash-bang projectile of claim 19 , wherein the tubular projectile casing comprises at least one of aluminum, plastic, rubber, and cardboard.

29. The crash-bang projectile of claim 19 , further comprising:

an obturator formed on an outer circumference of the tubular projectile casing.

30. The crash-bang projectile of claim 19 , wherein the crash-bang cartridge within which the crash-bang projectile fits in order to form a crash-bang assembly further comprises:

a tubular cartridge;

primer at one end of said tubular cartridge;

propellant in said tubular cartridge for launching the crash-bang projectile from said tubular cartridge, said propellant being ignited by said primer; and

a pressure wad between said propellant and said projectile.

31. A method of manufacturing a crash-bang cartridge assembly, said crash-bang cartridge assembly comprising a tubular cartridge and a projectile within said tubular cartridge, said method comprising the steps of:

forming a tubular projectile casing;

placing a delay block at one end of the tabular projectile casing, wherein a delay fuse column is within said delay block, and said delay fuse column is at least partially filled with a delay fuse composition;

placing a flash charge within said projectile casing; and

placing a weighty and frangible ballast on a leading edge of said projectile, at an end of the tubular projectile casing opposite from the end having the delay block;

wherein the weighty and frangible ballast comprises a mixture of zinc powder and graphite powder;

wherein a weight of said ballast is sufficient to provide stability and accuracy in flight; and

wherein the weighty and frangible ballast is sufficiently frangible that, alter detonation of said flash charge, said ballast comprises low mass, low energy components.

32. The method of claim 31 , further comprising the step of:

consolidating the delay fuse composition within the delay block.

33. The method of claim 31 , further comprising the step of:

consolidating the weighty and frangible ballast inside the tubular projectile casing.

34. The method of claim 33 , wherein the tubular projectile casing forms a cup and the end of the tubular projectile casing where the weighty and frangible ballast is located forms a solid end of the cup, and wherein said step of consolidating the at least one material comprising the weighty and frangible ballast comprises the step of:

consolidating the weighty and frangible ballast at said solid end of the cup by pressing a ram over the at least one material.

35. The method of claim 33 , wherein the weighty and frangible ballast remains substantially in place in the end of the tubular projectile casing by means of said consolidation.

36. The method of claim 31 , further comprising the step of:

securing the weighty and frangible ballast at the end of the tubular projectile casing with a wad.

37. The method of claim 31 , wherein the tubular projectile casing comprises a cardboard tube, the method further comprising the steps of:

sealing the end of the tubular projectile easing where the weighty and frangible ballast is located with an upper closure wad; and

sealing the weighty and frangible ballast in with a lower closure wad in an inside portion of the tubular projectile casing.

38. The method of claim 31 , further comprising the step of:

controlling a degree of frangibility of the weighty and frangible ballast by adjusting components comprising the weighty and frangible ballast.

39. The method of claim 31 , further comprising the step of:

at least one of forming and placing an obturator on an outer circumference of the tubular projectile casing.

40. The method of claim 31 , further comprising the steps of:

placing a primer at one end of said tubular cartridge;

placing propellant in said tubular cartridge; and

placing a pressure wad between said propellant and the projectile.

41. The method of claim 40 , further comprising the step of:

crimping an end of the tubular cartridge opposite from said end of the tubular cartridge having the primer inward to seal the projectile within the tubular cartridge.

42. The method of claim 41 , further comprising the step of:

placing a closure wad at the end of the tubular cartridge opposite from the primer in order to seal the projectile within the tubular cartridge, wherein said step of crimping at least assists in keeping said closure wad in place.

Assignments (7)
PATENT, TRADEMARK AND COPYRIGHT SECURITY AGREEMENT Recorded Nov 3, 2023
From: COMBINED SYSTEMS, INC.; CTS-CSI HOLDINGS, INC.
To: FIRST NATIONAL BANK OF PENNSYLVANIA
Reel/Frame 065448/0586 →
RELEASE OF SECURITY INTEREST Recorded Nov 2, 2023
From: FIDUS INVESTMENT CORPORATION
To: COMBINED SYSTEMS, INC.
Reel/Frame 065432/0324 →
SECURITY INTEREST Recorded Feb 3, 2020
From: COMBINED SYSTEMS, INC.
To: FIDUS INVESTMENT CORPORATION, AS COLLATERAL AGENT
Reel/Frame 051696/0132 →
RELEASE OF SECURITY INTEREST Recorded Jan 31, 2020
From: FIRST EAGLE PRIVATE CREDIT, LLC (FKA NEWSTAR BUSINESS CREDIT, LLC)
To: COMBINED SYSTEMS, INC.
Reel/Frame 051687/0760 →
RELEASE OF SECURITY INTEREST Recorded Jan 31, 2020
From: FIRST EAGLE PRIVATE CREDIT, LLC (FKA NEWSTAR FINANCIAL, INC.)
To: COMBINED SYSTEMS, INC.
Reel/Frame 051687/0345 →
CORRECTIVE ASSIGNMENT TO ADD PATENT NO. 7444941 PREVIOUSLY RECORDED AT REEL: 036101 FRAME: 0021. ASSIGNOR(S) HEREBY CONFIRMS THE SECURITY AGREEMENT. Recorded Aug 13, 2015
From: COMBINED SYSTEMS, INC.
To: NEWSTAR BUSINESS CREDIT, LLC
Reel/Frame 036501/0251 →
SECURITY INTEREST Recorded Jul 13, 2015
From: COMBINED SYSTEMS, INC.
To: NEWSTAR BUSINESS CREDIT, LLC
Reel/Frame 036101/0021 →