IP Library Granted Patent US 11,609,073
Granted Patent B2
US 11,609,073 · App. 17/127,505 · Granted Mar 21, 2023

Munitions and methods for operating same

Inventors: Sean Kevin Treadway (Mooresville, NC); Erik Charles Wemlinger (Mooresville, NC); Michael John Worsham (Mooresville, NC); James Edward Painter, III (Mooresville, NC)
Assignee: Corvid Technologies LLC
F42B12/60F42B12/32
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Quick Facts
Patent No.
US 11,609,073
App. No.
17/127,505
Granted
Mar 21, 2023
Kind
B2
Abstract

A warhead includes a gas generator, a plurality of barrels, and a plurality of projectiles. The warhead is configured to selectively actuate the gas generator to generate a pressurized gas that energetically propels the projectiles through and out from the barrels to strike a target.

Claims (73)

1. A warhead comprising:

a gas generator;

a plurality of barrels;

a pressure distribution manifold; and

a plurality of projectiles;

wherein the warhead is configured to selectively actuate the gas generator to generate a pressurized gas that energetically propels the projectiles through and out from the barrels to strike a target; and

wherein the pressure distribution manifold is configured to direct the pressurized gas from the gas generator to the barrels.

2. The warhead of claim 1 wherein:

the gas generator includes a combustible gas generating material; and

when the gas generator is actuated, the gas generating material is combusted to generate the pressurized gas.

3. The warhead of claim 2 wherein the gas generating material is an explosive material.

4. The warhead of claim 3 wherein, when the gas generator is actuated, the gas generating material deflagrates and is not detonated.

5. The warhead of claim 4 wherein the gas generating material is a low explosive material.

6. The warhead of claim 4 wherein the gas generating material is a high explosive material.

7. The warhead of claim 1 wherein:

the warhead has a leading end and an opposing trailing end, and a warhead axis extending in a forward direction from the trailing end to the leading end; and

at least some of the barrels have a barrel axis that extends radially outward relative to the warhead axis.

8. The warhead of claim 7 wherein at least some of the barrels have a barrel axis the forms an oblique barrel angle relative to the warhead axis.

9. The warhead of claim 8 wherein at least some of the barrels have a barrel axis that forms an acute barrel angle relative to the warhead axis in the forward direction.

10. The warhead of claim 9 wherein at least some of the barrels have different barrel angles from one another.

11. The warhead of claim 1 wherein a plurality of the barrels are fluidly coupled to the pressure distribution manifold at circumferentially and axially distributed locations about the pressure distribution manifold.

12. The warhead of claim 11 wherein:

at least some of the barrels are provided with a gas restriction section between the pressure distribution manifold and the barrel; and

the gas restriction section is configured to regulate a gas pressure from the pressure distribution manifold into the barrel.

13. The warhead of claim 11 wherein:

the warhead includes a warhead body; and

the pressure distribution manifold and the barrels are defined in the warhead body.

14. The warhead of claim 13 wherein:

the warhead body has an outer surface; and

exit ports of the barrels are defined in the outer surface of the warhead body.

15. The warhead of claim 14 including a cover sheet covering the exit ports.

16. The warhead of claim 14 including muzzle plugs disposed in the exit ports.

17. The warhead of claim 13 wherein:

the gas generator includes a container and the gas generating material disposed in the container; and

the gas generator is mounted on the warhead body to direct the pressurized gas into the manifold.

18. The warhead of claim 1 wherein the manifold is a tubular chamber.

19. The warhead of claim 18 including a volume reducer member than defines an inner boundary of the tubular chamber.

20. The warhead of claim 1 wherein each barrel includes:

a breech section and projectile guide section;

at least one projectile mounted in the breech section thereof; and

a retainer plug holding the at least one projectile in the breech section until the gas generator is actuated.

21. The warhead of claim 1 wherein at least some of the projectiles are spherical.

22. The warhead of claim 1 wherein at least some of the projectiles are disc-shaped.

23. The warhead of claim 1 wherein the warhead includes at least 20 barrels.

24. The warhead of claim 1 wherein at least one of the barrels includes multiple projectiles disposed therein to be fired.

25. The warhead of claim 1 including a gas generator actuation system configured to actuate the gas generator.

26. The warhead of claim 1 wherein the gas generator actuation system includes a hot wire.

27. The warhead of claim 1 wherein the gas generator actuation system includes a shock initiation device.

28. The warhead of claim 1 wherein the warhead is configured such that the pressurized gas pressurizes the barrels via the manifold to substantially simultaneously drive the projectiles out from their respective barrels.

29. A munition comprising:

a munition platform;

a warhead on the munition platform for flight therewith, the warhead including:

a gas generator;

a plurality of barrels;

a pressure distribution manifold; and

a plurality of projectiles;

wherein the warhead is configured to selectively actuate the gas generator to generate a pressurized gas that energetically propels the projectiles through and out from the barrels to strike a target; and

wherein the pressure distribution manifold is configured to direct the pressurized gas from the gas generator to the barrels.

30. The munition of claim 29 including a seeker subsystem, wherein the munition is operative to actuate the gas generator responsive to a signal from the seeker subsystem.

31. The munition of claim 30 wherein:

the seeker subsystem includes a height of burst (HOB) sensor; and

the munition is operative to actuate the gas generator responsive to a signal from the HOB sensor.

32. The munition of claim 29 wherein the munition platform includes a propulsion system.

33. A method for damaging a target, the method comprising:

providing a warhead including:

a gas generator;

a plurality of barrels;

a pressure distribution manifold; and

a plurality of projectiles;

wherein the warhead is configured to selectively actuate the gas generator to generate a pressurized gas that energetically propels the projectiles through and out from the barrels to strike a target; and

wherein the pressure distribution manifold is configured to direct the pressurized gas from the gas generator to the barrels; and

actuating the gas generator to generate a pressurized gas that energetically propels the projectiles through and out from the barrels in a forward direction to strike a target and such that the energetically propelled projectiles form a cone of effect;

wherein, after the projectiles are energetically propelled from the barrels, the warhead impacts within the cone of effect while the warhead is substantially intact.

Assignments (4)
RELEASE OF SECURITY INTEREST Recorded Jul 2, 2026
From: TRUIST BANK, AS ADMINISTRATIVE AGENT
To: CORVID TECHNOLOGIES, LLC
Reel/Frame 075163/0652 →
SECURITY INTEREST Recorded Jun 30, 2026
From: CORVID TECHNOLOGIES LLC
To: TRUIST BANK
Reel/Frame 075136/0352 →
SECURITY INTEREST Recorded Nov 13, 2025
From: CORVID TECHNOLOGIES, LLC
To: TRUIST BANK, AS ADMINISTRATIVE AGENT
Reel/Frame 072898/0012 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 18, 2020
From: TREADWAY, SEAN KEVIN; WEMLINGER, ERIK CHARLES; WORSHAM, MICHAEL JOHN; PAINTER, JAMES EDWARD, III
To: CORVID TECHNOLOGIES LLC
Reel/Frame 054698/0602 →
Continuity (4)
Continuation In Part 16745016 · Jan 16, 2020
Provisional Application 62955608 · Dec 31, 2019
Provisional Application 62821645 · Mar 21, 2019
Related Publication 20210404782A1 · Dec 30, 2021
Cited By (4)
US 12,352,544 US 12,365,458 US 12,366,436 US 12,429,317