Low collateral damage kinetic energy projectile

• US 9,329,008 B1
• Filed: 07/28/2014
• Issued: 05/03/2016
• Est. Priority Date: 08/08/2013
• Status: Active Grant

• Current Assignee: United States Secretary of the Army
• Original Assignee: The United States Of America As Represented By The Secretary Of The Army
• Inventors: Hassan, Ahmed, Vella, Anthony, Gilbert, Steven, Chen, Yin
• Primary Examiner(s): Chambers, Troy
• Assistant Examiner(s): Cochran, Bridget
• Application Number:
  US14/444,301
• Time in Patent Office: 645 Days
• Field of Search: 102/506, 102/517, 102/439, 102/498, 102/519, 102/529
• US Class Current: 1/1
• CPC Class Codes: F42B 10/48 Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retardingF42B10/34 takes precedence
• CPC Class Codes: F42B 12/02 characterised by the warhead or the intended effect
• CPC Class Codes: F42B 12/06 with hard or heavy core; Kinetic energy penetrators F42B12/16, F42B12/74 take precedence
• CPC Class Codes: F42B 12/74 of the core or solid body
• CPC Class Codes: F42B 14/06 Sub-calibre projectiles having sabots; Sabots therefor

Abstract

A low collateral damage, kinetic energy penetrator has multiple segments that are mechanically locked together by centrifugal force generated by penetrator spin. When the penetrator spin decreases below a minimum value, the segments separate and fall to the ground with non-lethal kinetic energy.

Claims

1. A kinetic energy penetrator having a central longitudinal axis, the penetrator comprising:

a nose segment having an aft portion;

a generally annular middle segment disposed aft of the nose segment;

a base segment disposed aft of the middle segment and having a forward portion;

a compression spring disposed in the middle segment, the compression spring biasing the nose segment and the base segment away from the middle segment;

a pair of torque transfer projections formed on each of the aft portion of the nose segment and the forward portion of the base segment, the projections in each pair being spaced 180 degrees apart;

slots formed in an inner surface of the middle segment for receiving the pairs of torque transfer projections whereby the pairs of torque transfer projections transfer torque from the base segment to the middle segment and the nose segment;

a pair of ball openings formed in each of the aft portion of the nose segment and the forward portion of the base segment, the ball openings in each pair being offset 90 degrees from respective torque transfer projections;

a pair of balls disposed in each of the two pairs of ball openings, each ball being translatable in its ball opening; and

forward and aft ball detents formed in the inner surface of the middle segment for receiving the pairs of balls;

wherein a first angular velocity of the penetrator causes the two pairs of balls to engage the forward and aft ball detents and mechanically lock the nose segment and the base segment to the middle segment.

2. The penetrator of claim 1, wherein a second angular velocity less than the first angular velocity causes the two pairs of balls to disengage the forward and aft ball detents thereby enabling the compression spring to separate the nose segment and the base segment from the middle segment.

3. The penetrator of claim 2, wherein each pair of torque transfer projections are opposing ends of a pin that is disposed in a through bore formed in each of the aft portion of the nose segment and the forward portion of the base segment.

4. The penetrator of claim 3, wherein each ball is constrained from translating completely out of its respective ball opening.

5. The penetrator of claim 4, wherein each ball opening is staked to constrain translation of its respective ball.

6. The penetrator of claim 4, wherein the forward and the aft ball detents are grooves formed in the inner surface of the middle segment.

7. The penetrator of claim 6, wherein the nose segment, middle segment and base segment comprise tungsten.

8. The penetrator of claim 4, further comprising a discarding sabot disposed around the penetrator.

14. A method, comprising:

providing the penetrator of claim 1;

spinning the penetrator up to at least the first angular velocity; and

translating the two pairs of balls into engagement with the forward and aft ball detents to thereby mechanically lock the nose segment and the base segment to the middle segment.

15. The method of claim 14, further comprising decelerating the angular velocity of the penetrator to less than the first angular velocity and then, translating the two pairs of balls out of engagement with the forward and aft ball detents to thereby unlock the nose segment and the base segment from the middle segment.

16. The method of claim 15, further comprising forcing the nose segment and the base segment away from the middle segment using the compression spring.

17. The method of claim 16, further comprising decreasing the kinetic energy of each of the nose segment, middle segment and base segment to less than about 75 joules.

9. A kinetic energy penetrator having a central longitudinal axis, the penetrator comprising:

a nose segment having an aft portion;

a generally annular middle segment disposed aft of the nose segment;

a base segment disposed aft of the middle segment and having a forward portion;

a compression spring disposed in the middle segment, the compression spring biasing the nose segment and the base segment away from the middle segment;

a pair of torque transfer projections formed on each of the aft portion of the nose segment and the forward portion of the base segment wherein each pair of torque transfer projections are opposing ends of a pin that is disposed in a through bore formed in each of the aft portion of the nose segment and the forward portion of the base segment;

slots formed in an inner surface of the middle segment for receiving the pairs of torque transfer projections whereby the pairs of torque transfer projections transfer torque from the base segment to the middle segment and the nose segment;

a pair of ball openings formed on each of the aft portion of the nose segment and the forward portion of the base segment;

a pair of balls disposed in each of the two pairs of ball openings, each ball being translatable in its respective ball opening and constrained from translating completely out of its respective ball opening; and

forward and aft ball detents formed in the inner surface of the middle segment for receiving the pairs of balls, the ball detents comprising grooves.

10. The penetrator of claim 9, wherein a first angular velocity of the penetrator causes the two pairs of balls to engage the forward and aft ball detents and mechanically lock the nose segment and the base segment to the middle segment.

11. The penetrator of claim 10, wherein a second angular velocity less than the first angular velocity causes the two pairs of balls to disengage the forward and aft ball detents thereby enabling the compression spring to separate the nose segment and the base segment from the middle segment.

12. The penetrator of claim 9, wherein each ball opening is staked to constrain translation of its respective ball.

13. The penetrator of claim 9, further comprising a discarding sabot disposed around the penetrator.