Less lethal ammunition

• US 8,065,961 B1
• Filed: 12/23/2008
• Issued: 11/29/2011
• Est. Priority Date: 09/18/2007
• Status: Active Grant

• Current Assignee: Scarr Research And Development Co. LLC
• Original Assignee: Kimball Rustin Scarr
• Inventors: Scarr, Kimball Rustin
• Primary Examiner(s): Chambers; Troy
• Application Number:
  US12/342,915
• Time in Patent Office: 1,071 Days
• Field of Search: 102/502, 102/503, 102/520, 89/17.01, 89/146
• US Class Current: 102/503
• CPC Class Codes: F42B 10/36 Ring-foil projectiles
• CPC Class Codes: F42B 10/54 Spin braking means
• CPC Class Codes: F42B 14/06 Sub-calibre projectiles having sabots; Sabots therefor
• CPC Class Codes: F42B 5/045 of telescopic type F42B5/184 takes precedence

Abstract

In one embodiment, a less lethal munition including a ring airfoil projectile. The flight trajectory of the projectile has increased accuracy resulting from the aerodynamic stabilization of the projectile. In some embodiments, the projectile is both aerodynamically stabilized and spin stabilized.

Claims

1. A method for firing a munition from a gun, comprising:

providing a projectile, a sabot, and supporting member within the barrel of the gun;

propelling the sabot with compressed gas;

guiding the propelled sabot by the supporting member and spinning the propelled sabot by said guiding;

pushing the projectile by the propelled sabot;

stopping the propelled sabot within the gun; and

firing the pushed projectile from the gun.

2. The method of claim 1 which further comprises retaining the stopped sabot by the supporting member.

3. The method of claim 2 which further comprises removing the supporting member with the retained sabot from the breech of the gun.

4. The method of claim 1 which further comprises guiding the propelled sabot by the barrel of the gun.

5. The method of claim 1 wherein the supporting member includes a rod extending from a base, and said guiding by the supporting member is by sliding contact between the sabot and the rod.

6. The method of claim 1 wherein the sabot comprises a first annular ring separable from a second annular ring, said pushing is by the first ring, and which further comprises:

separating the first ring and the second ring before said firing; and

ejecting the first ring from the muzzle of the barrel.

7. The method of claim 1 wherein said stopping is on the supporting member.

8. The method of claim 1 wherein the supporting member is cylindrical and said guiding is by the outer diameter of the supporting member.

9. The method of claim 1 wherein the projectile is a ring airfoil.

10. The method of claim 1 wherein said pushing include spinning the projectile by the propelled sabot.

11. The method of claim 1 which further comprises spinning the sabot by rifling of the barrel.

12. The method of claim 1 wherein the compressed gas is provided by an explosive charge.

13. A method for automatic feeding of a munition into a gun, comprising:

providing a munition including an elastically deformable link, a projectile, and a cylindrical body, the cylindrical body having at least portions of a circumferential ridge;

supporting the link on the body in a first state of elastic tension;

feeding the munition into the breech of the gun;

contacting the link with the breech;

pushing the munition into the barrel after said contacting;

sliding the contacted link toward the aft end of the munition by said pushing;

moving the link on the ridge portions on the body; and

stopping the movement of the munition into the barrel by contacting the breech with the ridge.

14. The method of claim 13 which further comprises supporting the link on the body in a second state of tension that is more relaxed than the first state before said moving.

15. The method of claim 14 wherein during said stopping the link is expanded to a second state of tension that is higher than the first state.

16. The method of claim 13 wherein during said stopping the link is expanded to a second state of tension that is higher than the first state.

17. The method of claim 13 wherein after said stopping at least a portion of the link remains seated on at least a portion of the ridge.

18. The method of claim 13 wherein said supporting is at a first diameter of the body and which further comprises supporting at least a portion of the link at a second diameter smaller than the first diameter before said moving.

19. The method of claim 18 wherein during said stopping the link is expanded to a second state of tension that is higher than the first state.

20. The method of claim 13 which further comprises propelling the projectile from the gun after said stopping.

21. The method of claim 13 wherein the projectile is a ring airfoil.

22. The method of claim 13 wherein said providing includes a movable sabot for propelling the projectile, and which further comprises moving the sabot toward the end of the gun barrel after said stopping.

23. The method of claim 13 wherein the cylindrical body is a first cylindrical body, said providing includes a second cylindrical body for supporting the projectile, and which further comprises coupling the first body to the second body by a threaded interface before said feeding.

24. The method of claim 13 wherein the breech end of the barrel includes a chamfer and said sliding is by contact of the link with the chamfer.

25. A method for automatic feeding of non-lethal munitions into a machine gun, comprising:

providing a munition including a circumferential link for coupling to a circumferential link of another munition, a first cylindrical body, a non-lethal projectile, and a second cylindrical body for supporting the projectile,

coupling the first body to the second body by a threaded interface;

supporting the link on the first body in a state of tension;

feeding the one munition into the breech of the gun after said coupling;

contacting the link with the breech;

pushing the one munition toward the barrel after said contacting;

sliding the contacted link toward the aft end of the one munition by said pushing.

26. The method of claim 25 wherein the cylindrical body includes a circumferential ridge, and said sliding includes expanding the link by the ridge.

27. The method of claim 25 wherein the non-lethal projectile is a ring airfoil.

28. The method of claim 25 wherein the breech end of the barrel includes a chamfer and said contacting is of the link with the chamfer.

29. The munition of claim 25 wherein said providing includes a sabot having an outer diameter greater than about 35 mm and less than about 43 mm, the sabot being adapted and configured to push the projectile.

30. The munition of claim 25 wherein the first cylindrical body includes a primer.

31. A method for firing a munition from a gun, comprising:

providing a projectile, a sabot, and supporting member within the barrel of the gun;

propelling the sabot with compressed gas;

guiding the propelled sabot by the supporting member;

pushing the projectile by the propelled sabot;

stopping the propelled sabot within the gun;

firing the pushed projectile from the gun;

retaining the stopped sabot by the supporting member; and

removing the supporting member with the retained sabot from the breech of the gun.

32. The method of claim 31 wherein the projectile is a ring airfoil.

33. A method for firing a munition from a gun, comprising:

providing a projectile, a sabot, and supporting member within the barrel of the gun, the supporting member including a rod extending from a base;

propelling the sabot with compressed gas;

guiding the propelled sabot by the supporting member by sliding contact between the sabot and the rod;

pushing the projectile by the propelled sabot;

stopping the propelled sabot within the gun; and

firing the pushed projectile from the gun.

34. The method of claim 33 which further comprises retaining the stopped sabot by the supporting member.

35. The method of claim 33 which further comprises removing the stopped sabot from the breech of the gun.

36. A method for firing a munition from a gun, comprising:

providing a projectile, a sabot including a first annular ring separable from a second annular ring, and a supporting member within the barrel of the gun;

propelling the sabot with compressed gas;

guiding the propelled sabot by the supporting member;

pushing the projectile by the first ring of the propelled sabot;

stopping the propelled sabot within the gun;

firing the pushed projectile from the gun;

separating the first ring and the second ring before said firing; and

ejecting the first ring from the muzzle of the barrel.

37. The method of claim 36 wherein the projectile is a ring airfoil.

38. A method for firing a munition from a gun, comprising:

providing a ring airfoil projectile, a sabot, and supporting member within the barrel of the gun;

propelling the sabot with compressed gas;

guiding the propelled sabot by the supporting member;

pushing the projectile by the propelled sabot;

stopping the propelled sabot within the gun; and

firing the pushed projectile from the gun.

39. The method of claim 38 which further comprises retaining the stopped sabot by the supporting member.

40. The method of claim 38 which further comprises removing the sabot from the breech of the gun.

41. The method of claim 38 wherein the supporting member includes a rod extending from a base, and said guiding by the supporting member is by sliding contact between the sabot and the rod.

42. The method of claim 38 wherein said stopping is on the supporting member.

43. The method of claim 38 wherein said pushing include spinning the projectile by the propelled sabot.

44. The method of claim 38 which further comprises spinning the sabot by rifling of the barrel.

45. The method of claim 38 wherein the compressed gas is provided by an explosive charge.

46. A method for firing a munition from a gun, comprising:

providing a projectile, a sabot, and supporting member within the barrel of the gun;

propelling the sabot with compressed gas;

guiding the propelled sabot by the supporting member;

pushing the projectile by the propelled sabot;

spinning the sabot by rifling of the barrel;

stopping the propelled sabot within the gun; and

firing the pushed projectile from the gun.

47. The method of claim 46 wherein the compressed gas is provided by an explosive charge.