Dual purpose gun barrel for spin stabilized or fin stabilized projectiles and gun launched rockets

• US 4,712,465 A
• Filed: 08/28/1986
• Issued: 12/15/1987
• Est. Priority Date: 08/28/1986
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Macdonald, Kenneth A. B.
• Primary Examiner(s): BENTLEY, STEPHEN
• Application Number:
  US06/901,486
• Time in Patent Office: 474 Days
• Field of Search: 42/76.01, 42/78, 89/1.703, 89/1.704, 89/1.705, 89/1.818, 89/8, 89/14.05, 89/16, 102/372, 102/374, 102/376, 102/379, 102/380, 102/381, 102/431, 102/432, 102/437, 102/439, 102/443, 102/520, 102/521, 102/522, 102/523, 102/524, 102/526, 102/700
• US Class Current: 89/16
• CPC Class Codes: F41A 21/18 Grooves-Rifling
• CPC Class Codes: F42B 14/02 Driving bands; Rotating bands F42B14/04 takes precedence
• CPC Class Codes: F42B 30/08 Ordnance projectiles or missiles, e.g. shells

Abstract

A gun barrel and projectile system utilizes a smooth central bore gun barrel fitted with a short rifled insert near the breech end. A projectile fitted with a perforated skirt and driving band about the base of the skirt are loaded into the gun barrel so that the driving band just engages the rifled insert, and the warhead portion of the projectile extends into the smooth bore portion of the barrel. Upon firing of a breech charge, gases from the breech charge are ducted to the space between the thin side walls of the projectile and the smooth central bore, thereby establishing a gas bearing. The gas bearing provides lateral support to the projectile and lubricates the projectile in the smooth central bore. Because of the lateral support the projectile receives from the gun barrel and the gas bearing, much less projectile structural strength is required to resist set-back forces. Mass fraction ratios of ordnance payload mass to structural mass in the projectile are on the order of ninety percent. Projectiles or guided rockets utilizing flip out fins or reaction jets during the ballistic trajectory portion of the flight are loaded in the gun barrel without a driving band so that no engagement with the rifled insert and consequently no projectile rotation occurs. Thus, a single gun barrel may be used to fire a large variety of projectile or rocket designs. Because the bore does not contain rifling at the muzzle, erosion at the muzzle is greatly reduced and barrel life increased many times. Additionally, muzzle velocity may be increased to achieve much greater range.

Claims

1. A gun barrel and projectile round combination, comprising:

an elongated tube having a smooth central bore and defining a muzzle end and a breech end;

a hollow cylindrical insert retained within said breech end coaxial with said smooth central bore and having a plurality of helical grooves defining lands therebetween on the inner surface of said insert;

a projectile loaded in said breech end, extending from the breech facing end of said insert forward into said smooth central bore, said projectile having a thin sidewall surrounding a central cavity and being dimensioned in diameter to provide a close sliding fit within said smooth central bore, said projectile further defining a hollow base circumscribed by a skirt which includes a plurality of pressure equalizing ports for transmitting breech pressure from the base of said projectile to the region between said thin sidewall and said smooth central bore; and

a frangible film surrounding said projectile skirt closing said pressure equalizing ports.

2. A gun barrel and projectile round combination as set forth in claim 1, further comprising:

a driving band encircling and retained to said projectile skirt and engravingly engaging said helical grooves and lands at said breech facing end of said hollow cylindrical insert.

3. A gun barrel and projectile round combination as set forth in claim 2, further comprising a swaging ring having an internal conical taper positioned at the muzzle facing end of said hollow cylindrical insert adjacent said smooth central bore.

4. A gun barrel and projectile round combination as set forth in claim 1 wherein said hollow cylindrical insert is retained in threaded engagement with the breech end of said elongated tube.

5. A gun barrel and projectile round combination as set forth in claim 1 wherein said projectile further comprises a high explosive warhead contained within said central cavity.

6. A gun barrel and projectile round combination as set forth in claim 1 further comprising a cartridge case releasably attached to the skirt of said projectile, and propellant contained within said cartridge case and said skirt.

7. A gun barrel and projectile round combination as set forth in claim 1 wherein said hollow cylindrical insert is frictionally retained within said breech end.

8. A gun barrel and projectile round combination as set forth in claim 1 wherein said projectile and smooth central bore respective diameters are selected to achieve a projectile side wall to smooth central bore surface clearance distance of at least 0.002 inches.

9. A gun barrel and projectile round combination as set forth in claim 1 wherein said skirt includes a base bulkhead and said skirt joins said thin sidewall in a threaded connection.

10. A gun barrel and projectile round combination as set forth in claim 1, wherein said projectile further comprises a forward portion having an ogive contour.

11. A gun barrel and projectile round combination as set forth in claim 10, further comprising a fuze mounted on said projectile at the apex of said ogive contour.

12. A gun barrel and projectile round combination as set forth in claim 1 wherein said pressure equalizing ports are angled toward the muzzle end of said elongated tube from the inside of the skirt to the outside.

13. A gun barrel and projectile round combination as set forth in claim 2 wherein said driving band comprises copper.

14. A gun barrel and projectile round combination as set forth in claim 2 wherein said skirt further defines a circumferential receiving groove positioned adjacent said driving band at the breech facing end of said skirt.

15. A gun barrel and projectile round combination as set forth in claim 6 wherein said cartridge case further comprises an initiating primer for igniting said propellant in response to an external firing signal.

16. A gun barrel and projectile round combination which achieves increased projectile velocity and extends barrel life, comprising:

an elongated tube having a muzzle end, a breech end and a smooth central bore therebetween, said breech end further defining a receiving bore coaxial with said smooth central bore and having a diameter which is larger than the diameter of said smooth central bore, and meeting said smooth central bore at a step transition, said breech end further defining a chamber having a diameter which is larger than the diameter of said receiving bore and meeting said receiving bore at a contoured bottleneck transition;

a swaging ring having a conically tapered interior surface oriented to taper from a larger diameter on a breech facing side to a smaller diameter on a muzzle facing side, said swaging ring being retained within said receiving bore against said step transition;

a replaceable hollow cylindrical sleeve retained within said receiving bore abutting said swaging ring, said sleeve defining a plurality of helical grooves and lands, said sleeve being contoured on a breech facing end to match the chamber bottleneck transition;

a cylindrical projectile having a warhead section and a base section, said warhead section including a hollow cylindrical thin walled shell having an ogive contour on one end and being open on the other end, an ordnance payload contained within said thin walled shell, and a fuze for functioning the payload in response to the projectile encountering a target surface, said base section including a bulkhead and a cylindrical skirt depending therefrom forming a hollow base for said projectile, said base section being mechanically joined to said warhead section, said skirt defining a plurality of pressure equalizing ports distributed evenly about the periphery of said skirt;

a frangible film covering the exterior of said skirt, closing said plurality of pressure equalizing ports;

a slotted driving band encircling said cylindrical skirt at a point spaced from said breech facing end of said skirt and engaging said helical grooves and lands on the breech facing end of said sleeve;

the exterior surface of said skirt on said breech facing end defining a reception groove adjacent said slotted driving band;

a hollow case releasably attached to said skirt;

propellant contained within said hollow case; and

means attached to said case for igniting said propellant in response to an external firing commend;

whereby upon reception of a firing command, the propellant is ignited and pressurizes the base of the projectile, high pressure gas from the propellant flowing through the pressure equalizing ports fracturing said frangible film and entering the space between the thin sidewall and the smooth central bore surface, said projectile being accelerated toward said muzzle end, said slotted driving band being engraved by said helical grooves and lands causing said projectile to rotate, said slotted driving band upon reaching said swaging ring being reshaped by said swaging ring and deposited into said reception groove just prior to entering the smooth central bore, said flowing high pressure gas forming a gas bearing between said projectile thin sidewall and said smooth central bore surface which balances setback forces operating on said projectile caused by acceleration and transmits lateral support to the thin sidewalls from the gun barrel to resist projectile deformation while also lubricating said projectile as it transits said gun barrel smooth central bore.

17. A gun barrel and projectile round combination as set forth in claim 16 wherein said sleeve is contoured on said breech facing end to join said chamber at said bottleneck transition.

18. A gun barrel and projectile round combination as set forth in claim 16 wherein said plurality of helical grooves have a depth which is greater than the engraving depth of the lands on the driving band, whereby high pressure gas from ignition of said propellant is enabled to flow past said driving band through said plurality of grooves.

19. A gun barrel and projectile round combination as set forth in claim 16 wherein said means for igniting said propellant comprises an electrically initiated primer.

20. A gun barrel and projectile round combination as set forth in claim 16 wherein said means for igniting said propellant comprises a percussion initiated primer.