Gun equipped with down-bore liquid propellant booster stage to increase projectile muzzle velocity

• US 5,631,436 A
• Filed: 06/15/1995
• Issued: 05/20/1997
• Est. Priority Date: 06/15/1995
• Status: Expired due to Fees

• Current Assignee: General Dynamics Armament Systems, Inc. (General Dynamics Corporation)
• Original Assignee: Martin Marietta Corporation
• Inventors: Brown, Steven J., Pate, Robert A.
• Primary Examiner(s): Eldred, J. Woodrow
• Application Number:
  US08/491,052
• Time in Patent Office: 705 Days
• Field of Search: 89/8, 89/7
• US Class Current: 89/8
• CPC Class Codes: F41A 1/04 Missile propulsion using the combustion of a liquid, loose powder or gaseous fuel, e.g. hypergolic fuel

Abstract

A booster stage is positioned down-bore from the breech of a gun to contain a charge of liquid propellant that is ignited by the combustion gases of a detonated breech propellant charge trailing the projectile down the gun bore. The detonated liquid propellant increases the bore gas pressure and thus accelerates the projectile to a higher muzzle velocity.

Claims

1. A gun comprising, in combination:

a breech for receiving a projectile and a breech propellant charge;

an elongated gun barrel having a bore communicating at one end with the breech and terminating at a muzzle; and

a booster stage including;

a cannister equipped to the gun barrel down-bore from the breech to define a reservoir in fluid communication with the bore, said cannister including a cylindrical surface radially expanded from the bore to define an annular reservoir open to the bore; and

charging apparatus connected to a source of liquid propellant to introduce the liquid propellant into the reservoir tangentially to the cylindrical surface Such as to produce a toroidal flow of liquid propellant surrounding the bore for charging the reservoir with the liquid propellant for detonation by combustion gases generated by detonation of the breech propellant charge that propels the projectile down the bore.

2. The gun defined in claim 1, wherein the cannister further defines a cylindrical chamber, and the booster stage further includes:

a piston slidingly received in the chamber to divide the chamber into an actuating cavity at a breech side of the piston and the annular reservoir at a muzzle side of the piston;

a first radial fluid passage in the gun barrel for diverting a portion of the breech propellant charge combustion gases from the bore into the actuating cavity to exert a pumping force on the piston; and

a second radial fluid passage down-bore from the first radial passage for directing liquid propellant pumped from the reservoir by the piston into the bore for detonation aft of the projectile.

3. The gun defined in claim 2, wherein the second radial fluid passage includes a bore open end located at a point spaced from the breech by a distance approximately equal to 40% of a length of the bore.

4. The gun defined in claim 3, wherein the first radial fluid passage includes a bore open end located approximately six inches up-bore from the second radial fluid passage bore open end.

5. The gun defined in claim 2, wherein the first radial fluid passage extends from the bore to the actuating cavity in a down-bore sloped direction, and the second radial fluid passage extends from the reservoir to the bore in a down-bore sloped direction.

6. The gun defined in claim 2, wherein the piston includes a sleeve slidingly received on an exterior cylindrical surface of the barrel in normally blocking relation with a reservoir open end of the second radial fluid passage, the sleeve including a slot positioned to unblock the reservoir open end of the second radial fluid passage during down-bore axial movement of the piston to pump liquid propellant from the reservoir into the bore.

7. The gun defined in claim 6, wherein the piston is slideable along a discharge path motivated by the pumping force of the breech propellant charge combustion gases from a charged position to a discharged position while the slot is axial aligned with the reservoir open end of the second radial fluid passage and along an charge path motivated by fluid pressure of the liquid propellant charging the reservoir from the discharged position to the charged position, the charge path being angularly displaced from the discharge path such that the piston sleeve blocks the reservoir open end of the second radial fluid passage during liquid propellant charging of the reservoir, the booster stage further including camming elements interacting to angularly reposition the piston between the charge and discharge paths.

8. The gun defined in claim 7, wherein the camming elements include:

first and second pins mounted by the barrel, and

first and second grooves formed in the sleeve, the first and second grooves extending in opposite axial directions from respective open ends to respective terminating cam surfaces,

the first pin entering the open end of the first groove during initial piston movement along the discharge path from the charged position and engaging the cam surface of the first groove to angularly position the piston to the discharged position, the second pin entering the open end of the second groove during initial piston movement along the charge path from the discharge position and engaging the cam surface of the second groove to angularly position the piston to the charged position.

9. A method of boosting the muzzle velocity of a gun including a breech and a barrel having a bore extending from the breech to a muzzle, the method comprising the steps of:

loading a projectile and a breech propellant charge into the breech of the gun;

charging a down-bore booster stage with liquid propellant to produce a toroidal flow of liquid propellant in an annular reservoir surrounding the bore;

detonating the breech propellant charge to generate high pressure combustion gases propelling the projectile down the bore;

exposing the liquid propellant to the breech propellant charge combustion gases at a down-bore location of diminishing combustion gas pressure in the bore; and

igniting the exposed liquid propellant, using the breech propellant charge combustion gases, to generate secondary combustion gases to boost combustion gas pressure in the bore and increase the projectile muzzle velocity of the gun.

10. The method defined in claim 9, wherein the exposing step includes utilizing the combustion gas pressure in the bore generated by the detonated breech propellant charge to inject the liquid propellant into the bore for detonation by the igniting step.

11. The method defined in claim 10, wherein the liquid propellant is injected into the bore at a down-bore location spaced from the breech by a distance approximately equal to 40% of the bore length.

12. A gun comprising, in combination:

a breech for receiving a projectile and a breech propellant charge;

an elongated gun barrel having a bore communicating at one end with the breech and terminating at a muzzle; and

a booster stage including;

a cannister equipped to the gun barrel down-bore from the breech to define a cylindrical-chambered reservoir in fluid communication with the bore;

charging apparatus connectable to a source of liquid propellant for charging the reservoir with the liquid propellant for detonation by combustion gases generated by detonation of the breech propellant charge that propels the projectile down the bore;

a piston slidingly received in the chamber to divide the chamber into an actuating cavity at a breech side of the piston and the reservoir at a muzzle side of the piston;

a first radial fluid passage in the gun barrel for diverting a portion of the breech propellant charge combustion gases from the bore into the actuating cavity to exert a pumping force on the piston; and

a second radial fluid passage down-bore from the first radial passage for directing liquid propellant pumped from the reservoir by the piston into the bore for detonation aft of the projectile,

said piston including a sleeve slidingly received on an exterior cylindrical surface of the barrel in normally blocking relation with a reservoir open end of the second radial fluid passage, the sleeve including a slot positioned to unblock the reservoir open end of the second radial fluid passage during down-bore axial movement of the piston to pump liquid propellant from the reservoir into the bore.

13. The gun defined in claim 12, wherein the piston is slideable along a discharge path motivated by the pumping force of the breech propellant charge combustion gases from a charged position to a discharged position while the slot is axial aligned with the reservoir open end of the second radial fluid passage and along a charge path motivated by fluid pressure of the liquid propellant charging the reservoir from the discharged position to the charged position, the charge path being angularly displaced from the discharge path such that the piston sleeve blocks the reservoir open end of the second radial fluid passage during liquid propellant charging of the reservoir, the booster stage further including camming elements interacting to angularly reposition the piston between the charge and discharge paths.

14. The gun defined in claim 13, wherein the camming elements include:

first and second pins mounted by the barrel, and

first and second grooves formed in the sleeve, the first and second grooves extending in opposite axial directions from respective open ends to respective terminating cam surfaces,

the first pin entering the open end of the first groove during initial piston movement along the discharge path from the charged position and engaging the cam surface of the first groove to angularly position the piston to the discharged position, the second pin entering the open end of the second groove during initial piston movement along the charge path from the discharge position and engaging the cam surface of the second groove to angularly position the piston to the charged position.