Extended range projectile

• US 7,823,510 B1
• Filed: 05/14/2008
• Issued: 11/02/2010
• Est. Priority Date: 05/14/2008
• Status: Expired due to Fees

• Current Assignee: Aerojet Rocketdyne Of De, Inc. (L3Harris Technologies, Inc.)
• Original Assignee: Pratt & Whitney Rocketdyne Incorporated (L3Harris Technologies, Inc.)
• Inventors: Hobart, Stephen Alan, Kokan, Timothy S., Massey, Frederic H., Minick, Alan B.
• Primary Examiner(s): ELDRED, JOHN W
• Application Number:
  US12/120,345
• Time in Patent Office: 902 Days
• Field of Search: 102/490, 102/440, 102/473, 102/501, 102/530
• US Class Current: 102/490
• CPC Class Codes: F42B 10/40 with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles

Abstract

A projectile and method of extending the range of the projectile. The projectile includes a storage tank operable to release a working fluid through an exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight.

Claims

1. A projectile comprising:

a projectile base;

an exhaust manifold defined within said projectile base; and

an initiator operable to release a working fluid from a storage tank in response to an acceleration of the projectile, the working fluid released through said exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight.

2. The projectile as recited in claim 1, wherein said exhaust manifold comprises an aperture.

3. The projectile as recited in claim 2, wherein said aperture comprises a nozzle.

4. The projectile as recited in claim 1, wherein said exhaust manifold comprises a multiple of apertures.

5. The projectile as recited in claim 4, wherein said multiple of apertures defines a ring pattern.

6. The projectile as recited in claim 4, wherein said multiple of apertures defines a showerhead pattern with a multiple of rings.

7. The projectile as recited in claim 1, further comprising a core contained at least partially within a jacket, said core defines a cavity which contains said storage tank.

8. The projectile as recited in claim 1, further comprising a distribution manifold between said storage tank and said exhaust manifold.

25. The projectile as recited in claim 1, wherein said working fluid is stored above 5000 psi.

9. A projectile comprising:

a projectile base;

an exhaust manifold defined within said projectile base;

a storage tank operable to release a working fluid through said exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight; and

an initiator adjacent said storage tank, at lest one of said initiator and said storage tank relatively movable to the other of said initiator and said storage tank to release the working fluid from said storage tank in response to an acceleration of the projectile.

10. A projectile comprising:

a projectile base;

an exhaust manifold defined within said projectile base;

a storage tank operable to release a working fluid through said exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight; and

a plug which seals said storage tank, said plug dislodgeable from said storage tank to release the working fluid from said storage tank in response to an acceleration of the projectile.

11. A projectile comprising:

a projectile base;

an exhaust manifold defined within said projectile base;

a storage tank operable to release a working fluid through said exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight; and

a plug which seals said storage tank, said plug opens to release the working fluid from said storage tank in response to an acceleration of the projectile.

12. A projectile comprising:

a projectile base;

an exhaust manifold defined within said projectile base;

a storage tank operable to release a working fluid through said exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight; and

an initiator which activates upon initial acceleration of the projectile to release the working fluid.

13. A projectile comprising:

a projectile base;

an exhaust manifold defined within said projectile base; and

a storage tank operable to release a working fluid through said exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight; and

an initiator which activates at a predetermined time after initial acceleration of the projectile to release the working fluid.

14. A projectile comprising:

a projectile base;

an exhaust manifold defined within said projectile base; and

a storage tank operable to release a working fluid through said exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight; and

a heat source adjacent said storage tank, said heat source operable to increase the temperature of the working fluid upon initial acceleration of the projectile.

15. A round of ammunition comprising:

a cartridge case;

a projectile seated within said cartridge case, said projectiles having a projectile base;

an exhaust manifold defined within said projectile base; and

a storage tank operable to release a working fluid through said exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight; and

an initiator operable to release the working fluid from said storage tank in response to an acceleration of the projectile.

16. The round of ammunition as recited in claim 15, wherein said projectile further comprises:

a core which defines a cavity which contains said storage tank; and

a jacket which surrounds said core, said jacket defines a cannelure at which said cartridge case is crimped to said projectile.

17. A method of extending the range of a non-propulsive projectile comprising:

activating an initiator to release a working fluid from a storage tank contained within a projectile in response to an acceleration of the projectile, the working fluid released through an exhaust manifold during a flight of the projectile to at least partially fill a wake aft of the projectile.

19. A method as recited in claim 17, further comprising releasing the working fluid upon firing of the projectile from a cartridge case.

21. A method as recited in claim 17, wherein at least partially filling the wake aft of the projectile reduces projectile base drag.

22. A method as recited in claim 17, further comprising:

expanding the working fluid at a pressure which exceeds a base pressure of the projectile.

23. A method as recited in claim 17, further comprising:

expanding the working fluid to below approximately one atmospheric pressure though the exhaust manifold.

24. A method as recited in claim 17, further comprising:

expanding the working fluid to below approximately one atmospheric pressure though the exhaust manifold.

18. A method of extending the range of a non-propulsive projectile comprising:

releasing a working fluid at a predetermined time after firing of the projectile from a cartridge case from a storage tank contained within a projectile through an exhaust manifold during a flight of the projectile to at least partially fill a wake aft of the projectile.

20. A method of extending the range of a non-propulsive projectile comprising:

releasing a working fluid from a storage tank contained within a cavity of a projectile through an exhaust manifold during a flight of the projectile to at least partially fill a wake aft of the projectile, the storage tank movable within the cavity to initiate release of the working fluid.