IP Library › Granted Patent US 8,109,212
Granted Patent B2
US 8,109,212 · App. 12/623,289 · Granted Feb 7, 2012

Sleeved projectiles

Assignee: Metal Storm Limited
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Quick Facts
Patent No.
US 8,109,212
App. No.
12/623,289
Granted
Feb 7, 2012
Kind
B2
Abstract

A projectile ( 10 ) is for use with barrel assemblies of the type having a plurality of projectiles axially disposed within a barrel having a bore and a muzzle and which projectiles are associated with discrete propellant charges for propelling said projectiles sequentially through the muzzle of the barrel. Projectile ( 10 ) comprises expandable sleeve ( 11 ) encircling at least part of core ( 12 ). Sleeve ( 11 ) and core ( 12 ) have wedging surfaces ( 14 ) operable to deform trailing part ( 21 ) of sleeve ( 11 ) into sealing engagement with the bore in response to pressure exerted on the projectile ( 10 ). When projectiles ( 10 ) are axially disposed in the bore, rear face ( 24 ) of the leading projectile cooperates with leading face ( 20 ) of the trailing projectile to define a discrete space about spine ( 23 ) for receipt of the propellant charge. Sleeve ( 11 ) is retained about the core ( 12 ) during travel to the target.

Claims (28)

1. A projectile for use with barrel assemblies having a plurality of projectiles axially disposed within a barrel having a bore and a muzzle, the projectiles being associated with discrete propellant charges for propelling said projectiles sequentially through the muzzle of the barrel, the projectile comprising:

a sleeve for engagement with the bore of the barrel; and

a projectile core about which the sleeve is disposed, wherein the sleeve surrounds and engages with a trailing portion of the projectile core;

a spacer tube extending rearwardly from the sleeve for extending over a portion of a trailing projectile, the spacer tube abutting a sleeve of the trailing projectile to form a column of sleeves and spacer tubes of said projectiles, the spacer tube having an end portion with a load transferring face for operatively transferring a load applied to the spacer tube to the abutting sleeve of the trailing projectile; and

a discrete propellant charge contained in the spacer tube to facilitate propelling of the projectile core and sleeve from the barrel, wherein the sleeve is retained about the projectile core and the spacer tube is carried away with the projectile when the projectile is propelled from the barrel.

2. A projectile according to claim 1 wherein the sleeve and projectile core have cooperating surfaces operable against each other to expand the sleeve into a sealing engagement with the bore of the barrel in response to a relative axial pressure exerted upon the sleeve by the projectile.

3. A projectile according to claim 2 wherein the cooperating surfaces are in a form of complementary wedging surfaces.

4. A projectile according to claim 2 wherein the projectile core comprises a mandrel portion which cooperates with a deformable annular sleeve.

5. A projectile according to claim 2 wherein the projectile core includes a rearwardly tapering wedging surface and the sleeve includes a complementary surface which assists the sleeve to expand as the projectile core moves rearwardly in the barrel relative to the sleeve.

6. A projectile according to claim 1 wherein the sleeve is retained about the projectile core by at least one shoulder located on one of the sleeve and the core, and wherein the shoulder is engaged with a corresponding recess on one of the core and the sleeve.

7. A projectile according to claim 1 wherein the cooperating surfaces are disposed on an end portion of the spacer tube and a leading face of the sleeve respectively, wherein the sleeve of the trailing projectile is urged into engagement with the bore of the barrel in response to relative axial compression between the spacer tube and the sleeve of the trailing projectile.

8. A projectile according to claim 1 wherein the sleeve is formed as a discarding sabot about the projectile core and is configured to discard upon impact with a target.

9. A projectile according to claim 1 wherein the sleeve is formed as a discarding sabot about the projectile core and is configured to discard in flight once the projectile core and sleeve have been propelled from the barrel.

10. A barrel assembly having a plurality of projectiles axially disposed within a barrel having a bore and a muzzle, the projectiles being associated with discrete propellant charges for propelling said projectiles sequentially and selectively through the muzzle of the barrel, each projectile comprising:

a sleeve for engagement with the bore of the barrel; and

a projectile core about which the sleeve is disposed, wherein the sleeve surrounds and engages with a trailing portion of the projectile core;

a spacer tube extending rearwardly from the sleeve for extending over a front portion of a trailing projectile core, the spacer tube abutting a sleeve of the trailing projectile to form a column of sleeves and spacer tubes of said projectiles, the spacer tube having an end portion with a load transferring face for operatively transferring a load applied to the spacer tube to the abutting sleeve of the trailing projectile; and

a discrete propellant charge contained in the spacer tube to facilitate propelling of the projectile core and sleeve from the barrel, wherein the sleeve is retained about the projectile core and the spacer tube is carried away with the projectile when the projectile is propelled from the barrel.

11. A projectile according to claim 7 wherein the cooperating surfaces comprise tapering wedging surfaces.

12. A projectile according to claim 11 wherein the tapering surfaces comprise rearwardly tapering surfaces.

13. A projectile according to claim 1 wherein the propellant charge is an encased propellant charge including a primer.

14. A projectile according to claim 1 wherein the propellant charge includes an electric primer.

15. A barrel assembly according to claim 10 wherein the barrel comprises a non metallic disposable barrel.

16. A barrel assembly according to claim 10 wherein the sleeve is retained about the projectile core by at least one shoulder located on one of the sleeve and the core, and wherein the shoulder is engaged with a corresponding recess on one of the core or the sleeve.

17. A barrel assembly according to claim 10 wherein cooperating surfaces are disposed on an end portion of the spacer tube and a leading face of the sleeve respectively, wherein the sleeve of the trailing projectile is urged into engagement with the bore of the barrel in response to relative axial compression between the spacer tube and the sleeve of the trailing projectile.

18. A barrel assembly according to claim 17 wherein the cooperating surfaces comprise rearwardly tapering wedging surfaces.

19. A barrel assembly according to claim 10 wherein the propellant charge is an encased propellant charge including a primer.

20. A barrel assembly according to claim 10 wherein the propellant charge includes an electric primer.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 9, 2015
From: METAL STORM LIMITED
To: DEFENDTEX PTY. LTD.
Reel/Frame 036767/0431 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 12, 2015
From: O'DWYER, JAMES MICHAEL
To: METAL STORM LIMITED
Reel/Frame 036311/0232 →
Priority Claims (1)
AU PQ 7499 · May 15, 2000 · national
Continuity (3)
Division 11387714 · Mar 24, 2006
Division 10275714
Related Publication 20100126370A1 · May 27, 2010