High accuracy projectile

• US 6,070,532 A
• Filed: 04/28/1998
• Issued: 06/06/2000
• Est. Priority Date: 04/28/1998
• Status: Expired due to Term

• Current Assignee: OLIN Corporation
• Original Assignee: OLIN Corporation
• Inventors: Halverson, Henry J.
• Primary Examiner(s): Tudor, Harold J.
• Application Number:
  US09/067,580
• Time in Patent Office: 770 Days
• Field of Search: 102/439, 102/501, 102/506-510, 102/517, 102/524, 102/526
• US Class Current: 102/501
• CPC Class Codes: F42B 14/02 Driving bands; Rotating bands F42B14/04 takes precedence
• CPC Class Codes: F42B 30/02 Bullets

Abstract

A projectile having improved accuracy when fired over long ranges is formed from a monolithic block of a copper alloy. Proceeding from a nose to a heel of the projectile, is a fore portion with arcuate side walls, a body portion of substantially constant cross-sectional area that minimally contacts a rifled gun barrel, a drive band having a diameter effective to seal propellant gases and an aft portion that continuously decreases in diameter terminating at the heel. A cylindrical bore extends from an opened end at the nose to a closed end proximate to a transition plane between the fore portion and the body portion.

Claims

1. A projectile to be fired from a weapon having a rifled barrel, said rifled barrel having an interior bore of a first diameter and a barrel groove surface of a second diameter greater than said first diameter, said projectile comprising:

a monolithic copper alloy of generally circular exterior latitudinal cross-section having a fore portion and an aft portion with a mid-portion disposed therebetween;

said fore portion extending from a nose thereof to a first transition plane and having arcuate sidewalls when viewed in longitudinal cross-section, that constantly increase in latitudinal exterior cross-sectional diameter from said nose to said first transition plane, a hollow cylindrical bore extending from an open end of said nose to a closed end proximate to said first transition plane;

said mid-portion having a body portion of generally constant latitudinal cross-section extending from said first transition plane to a second transition plane and a drive band portion of generally constant latitudinal cross-section extending from said second transition plane to a third transition plane, said body portion having a latitudinal diameter slightly greater than said first diameter but less than said second diameter and effective to minimally contact said rifling of said rifled barrel and said drive band having a latitudinal diameter greater than said body portion latitudinal diameter and effective to seal propellant gases behind a heel of said projectile; and

said aft portion having a latitudinal diameter that constantly decreases from said third transition plane to said heel.

2. The projectile of claim 1 wherein said body portion latitudinal diameter is from about 0.0005 inch to about 0.0025 inch greater than said interior bore first diameter.

3. The projectile of claim 2 wherein said body portion latitudinal diameter is from about 0.001 inch to about 0.002 inch greater than said interior bore first diameter.

4. The projectile of claim 2 wherein said drive band portion latitudinal diameter is from about 0.0005 inch to about 0.0025 inch greater than said barrel groove surface second diameter.

5. The projectile of claim 4 wherein said drive band portion latitudinal diameter is from about 0.001 inch to about 0.002 inch greater than said barrel groove surface second diameter.

6. The projectile of claim 4 wherein said arcuate sidewalls have a radius of curvature that is from about 1.5 to about 5 times a length of said projectile.

7. The projectile of claim 6 wherein said arcuate sidewalls have a radius of curvature that is from about 2 to about 3 times said length of said projectile.

8. The projectile of claim 6 wherein said closed end of said hollow cylindrical bore is within about 0.7 calibers of said first transition plane.

9. The projectile of claim 8 wherein said closed end of said hollow cylindrical bore is within about 0.3 calibers of said first transition plane.

10. The projectile of claim 8 wherein said monolithic copper alloy is brass.

11. The projectile of claim 10 wherein said monolithic copper alloy is selected from the group consisting of copper alloy C31400 and C31600.

12. The projectile of claim 11 being a 0.50 caliber projectile.

13. The projectile of claim 1 having a nominal caliber of 0.50 or less.

14. A projectile configured to be incorporated into a cartridge and to be fired from a weapon having a rifled barrel, said rifled barrel having barrel land surface of a land diameter and a barrel groove surface of a groove diameter, said projectile extending along a projectile length from a nose to a heel along a central longitudinal axis and consisting essentially of a monolithically formed copper alloy combination of:

a fore portion extending aft along a first length, at least thirty percent of the projectile length, from the nose to a first plane and over a majority of the first length having a continuously curving convex longitudinal profile;

a mid-portion extending aft along a second length from the first plane to a second plane and having;

a fore subportion having a third length at least equal in dimension to the land diameter, over a majority of the third length having a longitudinal profile defining a first right circular cylindrical exterior surface of a first diameter slightly larger than the land diameter and configured to cooperate with the barrel land surface to register the projectile centrally within the barrel when the cartridge is chambered in the weapon; and

an aft subportion having a fourth length, over a majority of the fourth length having a longitudinal profile defining a second right circular cylindrical exterior surface of a second diameter greater than the first diameter and greater than the groove diameter and configured to be accommodated within a case of the cartridge prior to discharge of the weapon and, upon discharge of the weapon, to engage the barrel so as to be deformed by the barrel land and groove surfaces and form a seal with the barrel effective to substantially seal combustion gasses behind the projectile during travel through the barrel; and

an aft portion extending aft along a fifth length from the second plane to the heel and over a majority of the fifth length having a rearwardly tapering longitudinal profile.

15. The projectile of claim 14 wherein the nose is truncated.

16. The projectile of claim 15 having a cavity extending rearward from the nose.

17. The projectile of claim 15 wherein the nose bounds a fore end of a central longitudinal channel extending aft along the longitudinal axis and terminating in close proximity to the first plane.

18. The projectile of claim 17 wherein the first diameter exceeds the land diameter by a first amount of about 0.0005 inch to about 0.0025 inch and the second diameter exceeds the groove diameter by a second amount from about 0.0005 inch to about 0.0025 inch.

19. The projectile of claim 18 wherein the projectile is a nominal 0.50 caliber projectile.

20. The projectile of claim 18 wherein the first diameter is from about 0.5017 inches to about 0.5020 inches and the second diameter is from about 0.5110 inches to about 0.5113 inches.

21. A projectile configured to be incorporated into a cartridge and to be fired from a weapon having a rifled barrel, said rifled barrel having barrel land surface of a land diameter and a barrel groove surface of a groove diameter, said projectile extending along a projectile length from a nose to a heel along a central longitudinal axis and comprising a monolithically formed copper alloy combination of:

a fore portion extending aft along a first length, at least thirty percent of the projectile length, from the nose to a first plane and over a majority of the first length having a continuously curving convex longitudinal profile and having a central cavity extending rearward from the nose;

a mid-portion extending aft along a second length from the first plane to a second plane and having;

a fore subportion having a third length at least equal in dimension to the land diameter, over a portion of the third length having a diameter slightly larger than the land diameter, but less than the groove diameter and configured to cooperate with the barrel land surface to register the projectile centrally within the barrel when the cartridge is chambered in the weapon; and

an aft subportion having a fourth length, over a majority of the fourth length having a diameter greater than the the groove diameter and configured to be accommodated within a case of the cartridge prior to discharge of the weapon and, upon discharge of the weapon, to engage the barrel so as to be deformed by the barrel land and groove surfaces and form a seal with the barrel effective to substantially seal combustion gasses behind the projectile during travel through the barrel; and

an aft portion extending aft along a fifth length from the second plane to the heel and over a majority of the fifth length having a rearwardly tapering longitudinal profile.