Reduced energy training cartridge for self-loading firearms

• US 7,984,668 B2
• Filed: 11/24/2009
• Issued: 07/26/2011
• Est. Priority Date: 01/22/2004
• Status: Expired due to Term

• Current Assignee: General Dynamics OTS Incorporated (General Dynamics Corporation)
• Original Assignee: Federal Cartridge Company (Vista Outdoor Inc.)
• Inventors: Huffman, Rick
• Primary Examiner(s): CLEMENT, MICHELLE RENEE
• Application Number:
  US12/625,033
• Publication Number:
  US 20100236442A1
• Time in Patent Office: 609 Days
• Field of Search: 89/11.3, 102/434, 102/433, 102/444, 102/446, 102/447, 102/464, 102/469
• US Class Current: 89/1.13
• CPC Class Codes: F42B 5/02 Cartridges, i.e. cases with charge and missile
• CPC Class Codes: F42B 5/045 of telescopic type F42B5/184 takes precedence
• CPC Class Codes: F42B 5/285 formed by assembling several elements
• CPC Class Codes: F42B 5/38 Separately-loaded propellant charges, e.g. cartridge bags F42B5/16, F42B5/192 take precedence
• CPC Class Codes: F42B 8/02 Cartridges F41A33/02, F42B7/12 take precedence

Abstract

A two piece, two-stage, rechargeable, reusable, reduced-energy mechanically operating cartridge is provided for launching a bullet of various compositions from a dedicated or modified firearm. The cartridge unit is comprised of a primary case, a piston sleeve, a propellant unit, and a bullet choice of a solid light weight material for inanimate-target applications or a “marking” version for non-lethal live-target training applications. Cartridge includes a piston sleeve and a primary case coupled together via a channel and cog locking/traveling/unlocking system. The primary case includes a substantially non-deformable jacket defining a cavity to receive a propellant unit or propellant connection and provides the channels to receive piston sleeves cogs for a locking/traveling/unlocking feature. The piston sleeve includes a substantially non-deformable jacket defining a cavity to receive configured bullet. The primary case also includes a substantially non-deformable jacket for being axially coupled with the piston sleeve, and for coupling with a propellant mechanism. Upon activation of the mechanically operating cartridge within the chamber of the firearm during stage 2, the piston sleeve and primary case telescope apart from a compressed, static, stage 1 position forcing the firearm'"'"'s slide or bolt to the rear, a mechanical operation opposed to a conventional cartridge with gas blow back operations. Spent cartridge is reused by manually separating piston sleeve from primary case as to remove spent propellant unit with removal tool, recharged with new propellant unit reloaded with choice of bullet composition and placed into magazine or similar for firearm loading.

Claims

1. A two-piece, two-stage, reduced energy mechanically-operating cartridge for launching a projectile from a firearm, comprising:

a piston sleeve comprising a piston sleeve jacket having a jacket wall and defining a projectile cavity at a first longitudinal end for coupling the projectile therein and a second longitudinal end for coupling with a primary case, a sealing surface on the jacket wall proximate to the first longitudinal end, and a circumferentially extending recess in the jacket wall proximate to the second longitudinal end, wherein the thickness of the jacket wall at the sealing surface is greater than the thickness of the jacket wall at the recess;

the primary case comprising a primary case jacket for being axially coupled with the second longitudinal end of the piston sleeve and defining a primary case cavity for coupling with a propellant mechanism, wherein the primary case is slidable within the piston sleeve between a compressed and a telescoped position such that the primary case extends from the primary case jacket when in the telescoped position; and

an o-ring disposed between the piston sleeve and the primary case for sealingly engaging the piston sleeve with the primary case and is positioned against the sealing surface when in the compressed position, wherein the recess is adapted to nonsealingly receive the o-ring when the primary case is slid into the telescoped position.

2. The cartridge of claim 1, wherein the piston sleeve comprises a shoulder, such that upon sliding the primary case into the telescoped position such that the primary case telescopes from the primary case jacket, said shoulder contacts a step between a chamber and a barrel of a firearm preventing the sleeve from advancing down the barrel, and instead the primary case thrusts rearward away from the barrel.

3. The cartridge of claim 1, wherein the jacket of the piston sleeve comprises a radially inward projection at the second longitudinal end that stops the separation of the primary case from the piston sleeve as the cartridge goes to the telescoped position from the compressed position.

4. The cartridge of claim 3, wherein the primary case has a radially outward projection that engages the radially inward projection of the piston sleeve as the cartridge goes to the telescoped position from the compressed position.

5. The cartridge of claim 1, wherein the propellant mechanism comprises a detonating primer.

6. The cartridge of claim 1, a regulator hole being further defined between the primary case and bullet cavities for regulating a velocity of the projectile upon firing.

7. The cartridge of claim 1, wherein the axial coupling involves the second end of the piston sleeve overlapping the primary case.

8. The cartridge of claim 1, wherein the piston sleeve further defines a first stopping structure positioned at the second longitudinal end and extending at least partially around the circumference of the piston sleeve at the second longitudinal end.

9. The cartridge of claim 8, wherein the primary case further defines a complementary second stopping structure for engaging the first stopping structure of the piston sleeve, wherein the first stopping structure is engaged by the second stopping structure when the primary case is slid into the telescoping position to prevent further sliding of the primary case.

10. A two-piece, two-stage, reduced energy mechanically-operating cartridge for launching a projectile from a dedicated or modified firearm, comprising:

a piston sleeve comprising a piston sleeve jacket defining a projectile cavity at a first longitudinal end for coupling the projectile therein and a second longitudinal end for coupling with a primary case, a sealing surface on the jacket wall proximate to the first longitudinal end, and a circumferentially extending recess in the jacket wall proximate to the second longitudinal end, wherein the thickness of the jacket wall proximate to the sealing surface is greater than the thickness of the jacket wall proximate to the recess;

the primary case comprising a primary case jacket for being axially coupled with the second longitudinal end of the piston sleeve and defining a primary case cavity for coupling with a propellant mechanism, wherein the primary case is slidable within the piston sleeve between a compressed and a telescoped position such that the primary case extends from the primary case jacket when in the telescoped position;

an o-ring disposed between the piston sleeve and the primary case for sealingly engaging the piston sleeve with the primary case and is positioned against the sealing surface when in the compressed position, wherein the recess is adapted to releasably receive the o-ring when the primary case is slid into the telescoped position; and

a vent defined between the case and sleeve which opens to communicate with ambient air at a stage during dynamic action to relieve pressure within the primary case cavity an appropriate amount to achieve a sufficient balance.

11. The cartridge of claim 10, wherein the jacket of the piston sleeve comprises a radially inward projection at the second longitudinal end that stops the separation of the primary case from the piston sleeve as the cartridge goes to the telescoped position from the compressed position.

12. The cartridge of claim 11, wherein the primary case has a radially outward projection that engages the radially inward projection of the piston sleeve as the cartridge goes to the telescoped position from the compressed position.

13. The cartridge of claim 10, a regulator hole being further defined between the primary case and projectile cavities of selected size for regulating a velocity of the projectile upon activation.

14. The cartridge of claim 10, wherein the axial coupling involves the primary case overlapping the second longitudinal end of the piston sleeve.

15. The cartridge of claim 10, wherein the primary case defines an annular groove for receiving the o-ring.

16. The cartridge of claim 10, wherein the piston sleeve further defines a first stopping structure positioned at the second longitudinal end and extending at least partially around the circumference of the piston sleeve at the second longitudinal end.

17. The cartridge of claim 16, wherein the primary case further defines a complementary second stopping structure for engaging the first stopping structure of the piston sleeve, wherein the first stopping structure is engaged by the second stopping structure when the primary case is slid into the telescoping position to prevent further sliding of the primary case.

18. A two-piece, two-stage, reduced energy mechanically-operating cartridge for launching a projectile from a dedicated or modified firearm, comprising:

a piston sleeve comprising a piston sleeve jacket having a jacket wall and defining a projectile cavity at a first longitudinal end for coupling the projectile therein and a second longitudinal end for coupling with a primary case, a sealing surface on the jacket wall proximate to the first longitudinal end, and a reduced thickness wall portion extending circumferentially in the jacket wall proximate to the second longitudinal end;

the primary case comprising a primary case jacket for being axially coupled with the second longitudinal end of the piston sleeve—

and defining a primary case cavity for coupling with a propellant mechanism, wherein the primary case is slidable within the piston sleeve between a compressed and a telescoped position such that the primary case extends from the primary case jacket when in the telescoped position;

an o-ring disposed between the piston sleeve and the primary case for sealingly engaging the piston sleeve with the primary case and is positioned against the sealing surface when primary case is in the compressed position, wherein when the o-ring is positioned at the reduced thickness wall portion in a non sealing state when the primary case is in the telescoped position;

a regulator hole defined between the primary case and projectile cavities of the piston sleeve;

wherein said primary case and piston sleeve are configured for axial coupling of the primary case with the second longitudinal end of the piston sleeve.

19. The cartridge of claim 18, wherein the primary case defines an annular groove for receiving the o-ring.

20. The cartridge of claim 18, wherein the axial coupling involves the second longitudinal end of the piston sleeve overlapping the primary case.

21. The cartridge of claim 18, wherein said annular protrusion provides said axial stabilization of the coupling of the piston sleeve and primary case when said sleeve and case are coupled together in a static position.

22. The cartridge of claim 18, wherein the piston sleeve further defines a first stopping structure positioned at the second longitudinal end and extending at least partially around the circumference of the piston sleeve at the second longitudinal end.

23. The cartridge of claim 22, wherein the primary case further defines a complementary second stopping structure for engaging the first stopping structure of the piston sleeve, wherein the first stopping structure is engaged by the second stopping structure when the primary case is slid into the telescoping position to prevent further sliding of the primary case.