Porous nozzle projectile barrel

• US 6,668,699 B2
• Filed: 02/05/2002
• Issued: 12/30/2003
• Est. Priority Date: 08/20/1998
• Status: Expired due to Term

• Current Assignee: Ronnie David Russell
• Original Assignee: Ronnie David Russell
• Inventors: Russell, Ronnie David
• Primary Examiner(s): Poon, Peter M.
• Assistant Examiner(s): Chambers, Troy
• Application Number:
  US10/068,037
• Publication Number:
  US 20020100361A1
• Time in Patent Office: 693 Days
• Field of Search: 89/140.5, 89/8, 89/143, 42/760.1
• US Class Current: 89/14.05
• CPC Class Codes: F41A 1/00 Missile propulsion characterised by the use of explosive or combustible propellant charges projecting missiles without use of explosive or combustible propellant charge F41B; launching rockets or torpedoes F41F3/00; missile self-propulsion F42B15/00
• CPC Class Codes: F41A 21/28 Gas-expansion chambers; Barrels provided with gas-relieving ports F41A1/06, F41A13/08 and F41A21/36 take precedence
• CPC Class Codes: F41B 11/00 Compressed-gas guns, e.g. air guns; Steam guns

Abstract

A porous barrel, projectile passageway, or tube as a type of supersonic nozzle for projectile propulsion therein and method for optimizing projectile velocity therethrough. The porous barrel features a barrel wall containing holes, passageways, or otherwise porous material through the barrel wall that allows gas, fluid, or other matter to exit or move in a direction away from the barrel interior. The flow of gas, fluid, or other matter away from the barrel interior allows gas within the barrel to expand in a direction transverse to the projectile path. The amount of transverse expansion of the gas in the barrel interior can be controlled by the porosity of the barrel wall to cause any desired amount of gas expansion. Transverse expansion allows axial gas velocities within the barrel to exceed the local speed of sound as if the gas had passed through a converging diverging nozzle. In one embodiment, a pressurized gas source supplies a pressure propelling the projectile through a gun barrel, and gas outflow from passageways through the barrel wall allows gas within the barrel, as well as the projectile, to obtain supersonic velocities as the gas and projectile accelerate.

Claims

1. Apparatus comprising:

a barrel formed by a barrel wall and having a breech end and a muzzle end, said barrel wall defining a passage of constant cross section extending from the breech end to the muzzle end;

a projectile having a cross section which closely matches the cross secton of the passage positioned in the passage; and

a driving gas pressure source connected to the breech end of the barrel, said driving gas pressure source having a sufficiently high pressure to accelerate the projectile to local Mach 1 in said barrel;

wherein said barrel wall has a solid region extending from the breech end toward the muzzle end and a porous region, serially arranged,

wherein said porous region is sufficiently permeable to the driving gas so that transverse expansion of the driving gas through the porous region permits the driving gas to achieve supersonic flow as if said driving gas had passed through a diverging supersonic nozzle,

and provide a projectile velocity profile equivalent to the projectile traveling through a supersonic nozzle designed to exactly conform the velocity of driving gas to the velocity of the projectile at every location along the path of the projectile through the porous region, wherein the driving gas velocity is subsonic in the solid region of the barrel and supersonic in the porous region of the barrel.

2. Apparatus as in claim 1 wherein the porous region of the barrel extends for at least 20 percent of the length of the barrel as measured between the breech end and the muzzle end.

3. Apparatus as in claim 2 wherein the porous region of the barrel comprises a plurality of longitudinally spaced apart transverse passageways extending through the barrel wall to cause a plurality of local gas mass flows from the passage and out through the barrel wall to achieve supersonic gas flow within said barrel and increasing speeds substantially greater than the speed of sound in driving gas flow within said barrel.

4. Apparatus as in claim 3 wherein the projectile has a cross section which closely matches the cross section of the passage and forms a seal against the barrel wall form the breech end and the plurality of longitudinally spaced apart passageways provide an ever increasing outflow area per unit length along the porous region of the tube, wherein the driving gas velocity is sub sonic in the solid region of the barrel and supersonic in the porous region of the barrel.