Multi-charge munitions, incorporating hole-boring charge assemblies

Patent metadata

Field	Value
Publication number	US-9605935-B1
Application number	US-13766693-A
Country	US
Kind code	B1
Filing date	Oct 14, 1993
Priority date	Jan 26, 1989
Publication date	Mar 28, 2017
Grant date	Mar 28, 2017

Abstract

Multi-charge munition suitable for defeating a concrete target consists of a detonatable array of hollow primary charges ( 14 ) of explosive supported laterally of a line of target penetration on which is disposed a secondary explosive charge ( 48 ). Simultaneous detonation of the primary charges in the array causes jet penetrators to be projected together towards the target which produce wide boreholes in concrete suitable for the subsequent emplacement and detonation of the secondary charge. The munition may be an aerially-deliverable bomb or submunition.
In one preferred embodiment, the primary charges ( 14 ) are positioned in a convergent configuration behind a forwardly-tapered secondary charge ( 48 ). Detonation of the primary charges projects penetrators forwardly passed the sides of the secondary charge and thrusts the secondary charge into the borehole produced in the target by the penetrators.

First claim

The invention claimed is:

1. Multi-charge munition for attacking a target having a surface, said munition travelling towards said target, said munition comprising:
a detonatable array of at least two hollow primary charges of explosive supported laterally about a fore-and-aft line of target penetration, each primary charge including a recessed forward face and a liner of non-explosive material lining said forward face, each said primary comprising a means, when said primary charge is detonated, for projecting a penetrator derived from the liner forwards along a line of trajectory extending from the array towards the target, said at least two penetrators comprising a means for boring a hole in said target on said line of target penetration;
a secondary cratering charge of explosive located on said fore-and-aft line of target penetration rearward of said array;
a fuse system for initiating detonation of said array of primary charges and said secondary charge in sequence;
a primary detonation means, responsive to said fuse system, for detonating the primary charges in the array in a temporal relationship with respect to one another such that the penetrators are projected towards the target and said line of target penetration concurrently to produce a hole therein; and
a secondary detonation means, responsive to said fuse system, for detonating the secondary charge, said secondary detonation means including delay means for delaying detonation of the secondary charge with respect to detonation of the primary charges, said delay means comprising a means for permitting detonation of the secondary charge when the secondary charge is located partly within the hole produced in the target by the penetrators of the array of primary charges.

2. Munition according to claim 1 wherein the primary charges in the detonatable array are all identical.

3. Munition according to claim 1 wherein the primary charges in the detonatable array lie in a plane normal to the line of target penetration.

4. Munition according to claim 1 wherein the primary detonation means is arranged to detonate all the primary charges substantially simultaneously.

5. Munition according to claim 1 wherein each primary charge has a width and a center of gravity, and the center of gravity of each primary charge in the detonatable array is located within a pitch circle diameter of less than 6 primary charge widths.

6. Munition according to claim 1 wherein the primary charges are supported in the array such that the primary charge lines of trajectory lie at angles of from greater than 0° to 30° to the line of target penetration.

7. Munition according to claim 1 wherein the primary charges are geometrically supported in the array such that the lines of trajectory converge towards one another forward of the array.

8. Munition according to claim 7 wherein the lines of trajectory are substantially focused at a focal point located forwards of the secondary cratering charge.

9. Munition according to claim 8 wherein each primary charge liner has a diameter and the focal point is located at a distance of from 2 to 20 liner diameters from each of the forward faces.

10. Munition according to claim 8 wherein the focal point is substantially the same distance from each primary charge and said primary detonation means comprises a means for detonating all the primary charges substantially simultaneously.

11. Munition according to claim 8 wherein the fuse system includes primary fuse means for initiating detonation of the primary charges when said focal point is located beneath the surface of the target.

12. Munition according to claim 7 wherein the focal point lies on the line of target penetration.

13. Munition according to claim 7 wherein said liners are of different materials, said different materials react together exothermically when the penetrators meet at the focal point.

14. Munition according to claim 1 wherein each liner is made of a material having a density of less than 5 gm cm −3 .

15. Munition according to claim 14 wherein the material is selected from the group consisting of aluminum, alloys of aluminum, plastics, and plastics loaded with up to 50% by weight of at least one of particulate aluminum and particulate aluminum alloy.

16. Munition according to claim 14 wherein the forward face of each primary charge has a conical recess therein with an apex angle of from 15° to 70°.

17. Munition according to claim 16 wherein the apex angle is from 20° TO 55°.

18. Munition according to claim 1 further including a moveable support means for displacing each primary charge laterally outwards with respect to the fore-and-aft axis of target penetration from a confined position at which the primary charges are packed together in a cluster, to a detonatable position in the array.

19. Munition according to claim 18 further including an energizing means, positioned between the primary charges, for activating said moveable support means for displacing the primary charges towards said detonatable position in the array.

20. Munition according to claim 18 wherein the moveable support means includes latch means for restraining the primary charges at said detonatable positions in the array.

21. Munition according to claim 18 further including a petalled housing means for housing said primary charges, said housing means is closed when the primary charges are disposed in their confined positions and is open when the primary charges are moved outwards to said detonatable positions in the array.

22. Munition according to claim 1 wherein the number of primary charges in the detonatable array is from three to six.

23. Munition according to claim 1 wherein the secondary cratering charge has a thickened ogival nose section.

24. Munition according to claim 1 wherein the munition comprises an aerially-dispensable submunition dispensable from a multi-submunition dispenser.

25. Munition according to claim 1 wherein the munition comprises an aerially-delivered bomb, the primary charges in the detonatable array being located in front of a bomb body containing the secondary charge.

26. Munition according to claim 25 wherein said bomb includes a forward guidance system with a plurality of flight guidance canards and the primary charges are supported about the fore-and-aft axis of target penetration between the bomb body and a forward guidance system for the bomb, said system including a body member disposed along said axis of target penetration and said forward guidance system.

27. Munition according to claim 26 wherein the lines of trajectory of the primary charges in the detonatable array extend between the canards.

28. Munition according to claim 26 wherein the number of primary charges and canards are the same.

29. Munition according to claim 26 wherein the primary charges and canards are each equispaced around the fore-and-aft line of target penetration.

30. Munition according to claim 26 further including aerodynamically-shaped shielding at least part of which is fitted over the outside diameter of the bomb body for supporting said primary charges.

31. Munition according to claim 30 wherein the shielding is at least partly contoured about the primary charges, and means for mounting said primary charges and body member to be axially rotatable relative to each

Assignees

• Powell Kevin Mark
• Evans Edward
• Qinetiq Ltd

Inventors

• Powell Kevin Mark
• Evans Edward

Classifications

• F42B1/032

  characterised by the material of the liner · CPC title

• F42B12/10 Primary

  with shaped or hollow charge (shaped or hollow charges per se F42B1/02 {; mines having hollow charges F42B23/04}) · CPC title

• F42B12/14

  the symmetry axis of the hollow charge forming an angle with the longitudinal axis of the projectile · CPC title

• F42B12/16 Primary

  in combination with an additional projectile or charge, acting successively on the target {(see also F42B12/625)} · CPC title

• F42B12/12

  rotatably mounted with respect to missile housing · CPC title