IP Library Granted Patent US 7,739,955
Granted Patent B2
US 7,739,955 · App. 10/558,754 · Granted Jun 22, 2010

Device adjacent to an explosive charge with at least two liners

Assignee: BAE Systems Bofors AB
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Quick Facts
Patent No.
US 7,739,955
App. No.
10/558,754
Granted
Jun 22, 2010
Kind
B2
Abstract

An explosive charge ( 3 ) can be equipped with two liners ( 4, 5 ) that can be attached to one another. The primary liner ( 4 ) is so devised that when choosing a first choice ( 11 ) of being able to work independently and by employing a symmetrical form achieving a forward-aimed Shaped Charge Warhead (SCW) effect upon explosive charge initiation by means of the material ( 7, 8 ) indicated for the primary liner. A secondary liner ( 5 ) is devised with a second choice ( 12 ) to be able to work together with the primary liner and together cause an asymmetric form that distributes the material ( 18, 19 ) from the liners at different velocities to thereby cause a forward-directed fragmentation effect. The ammunition unit ( 1 ) can, thus, be designed or prepared for two different combat cases in a technologically simple and unambiguous manner.

Claims (23)

1. A device at an explosive charge comprising:

a primary liner and a secondary liner being arrangeable to each other such that different combat capabilities are made possible,

the primary liner being arranged at a first selection to be able to function independently and by employment of a symmetrical form to achieve a forward-aimed Shaped Charge Warhead (SCW) effect upon initiation of the explosive charge with emitted material from the primary liner,

the secondary liner being arranged by means of a second selection to be able to function together with the primary liner and together cause a forward-directed fragmentation effect, wherein the primary liner and the secondary liner are arranged to cause an asymmetrical form that upon the initiation of the explosive charge passes on different velocities to the emitted material of the liners,

wherein the secondary liner is thinnest in a middle part and devised with a radially outwards and evenly increasing thickness, and

wherein the secondary liner is also devised with a thickness variation in a circumferential or angular direction to obtain emitted material and disallowing the occurrence of a material collision in a forward direction.

2. A device in accordance with claim 1 , wherein the primary and secondary liners are arranged with an essentially convex form having an opening, wherein the opening is aimed forwardly in a direction of motion for an explosive charge bearing ammunition unit, and wherein a rear surface of the secondary liner has an embodiment that essentially corresponds to the convex surface of the primary liner.

3. A device in accordance with claim 1 , wherein the primary liner is arranged with an essentially equal thickness with regard to its radial or diametrical extensions.

4. A device in accordance with claim 1 , wherein the secondary liner has an inner surface or convex surface formed by a number of surface sector parts fitted next to one another.

5. A device in accordance with claim 1 , wherein the secondary liner has an inner surface formed by a number of partly overlapping helical sub-surfaces.

6. A device in accordance with claim 1 , wherein the secondary liner has a center hole.

7. A device in accordance with claim 1 , the secondary liner is made of compact or prefragmented material.

8. A device in accordance with claim 1 , wherein the primary and secondary liner are embodied in essentially the same material.

9. A device in accordance with claim 1 , wherein the secondary liner is made of brittle material.

10. A device in accordance with claim 1 , wherein the secondary liner has a prefragmented design.

11. A device in accordance with claim 1 , wherein the ammunition unit is equipped during production with the primary and secondary liners and wherein the secondary liner is devised so as to be removable in case of the first selection.

12. A device in accordance with claim 2 , wherein the ammunition unit is a missile or a projectile.

13. A device in accordance with claim 2 , wherein the primary liner is arranged with an essentially equal thickness with regard to its radial or diametrical extensions.

14. A device in accordance with claim 2 , wherein the secondary liner is devised with a radially outwards and evenly increasing thickness.

15. A device in accordance with claim 3 , wherein the secondary liner is devised with a radially outwards and evenly increasing thickness.

16. A device in accordance with claim 2 , wherein the secondary liner has a center hole.

17. A device in accordance with claim 3 , wherein the secondary liner has a center hole.

18. A device in accordance with claim 1 , wherein the secondary liner has a center hole.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 10, 2006
From: RONN, TORSTEN; THUMAN, CHRISTER
To: BAE SYSTEMS BOFORS AB
Reel/Frame 017608/0201 →
Priority Claims (1)
SE 0301611 · Jun 4, 2003 · national
Continuity (1)
Related Publication 20070214991A1 · Sep 20, 2007