US3618250A - Launching arrangement for sub-caliber projectiles - Google Patents
Launching arrangement for sub-caliber projectiles Download PDFInfo
- Publication number
- US3618250A US3618250A US850462A US3618250DA US3618250A US 3618250 A US3618250 A US 3618250A US 850462 A US850462 A US 850462A US 3618250D A US3618250D A US 3618250DA US 3618250 A US3618250 A US 3618250A
- Authority
- US
- United States
- Prior art keywords
- sub
- launching
- arrangement
- caliber
- traveling barrel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000003380 propellant Substances 0.000 abstract description 11
- 238000000926 separation method Methods 0.000 abstract description 2
- 238000010304 firing Methods 0.000 description 5
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/10—Insert barrels, i.e. barrels for firing reduced calibre ammunition and being mounted within the normal barrels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/10—Cartridges, i.e. cases with charge and missile with self-propelled bullet
- F42B5/105—Cartridges, i.e. cases with charge and missile with self-propelled bullet propelled by two propulsive charges, the rearwardly situated one being separated from the rest of the projectile during flight or in the barrel; Projectiles with self-ejecting cartridge cases
Definitions
- the invention relates to weapon systems and, more particularly, to weapon systems for launching sub-caliber cartridges or projectiles.
- Another object of the invention is to provide such an arrangement which is inexpensive and includes a lightweight, easily distinguishable cartridge.
- FIG. 1 is a partial sectional view of a weapon arrangement embodying the principles of the invention.
- FIG. 2 is a similar view of a modified arrangement.
- the rifle stock (FIG. 1) has its launching tube 11 secured thereto by means (not shown).
- the inner end of the launching tube, rearward of its rifling groove means 12, is provided with annular recesses 13, 14 to accommodate similarly shaped peripheral portions of an obturator 15 that is secured to the rearward circumferential flange 16 of an expendable traveling barrel 17 by a light crimp or the equivalent.
- the longitudinally spaced, circumferential flanges 16, 18 on the barrel 17 have predetermined peripheral dimensioning such that their outer surfaces can slidably function with clearance within or inside the lands or smallest dimensioning of the launch tube rifling grooves 12.
- the obturator 15 has its forward face centrally recessed to contain a first propellant charge 20 that is initiated by its primer 21 upon actuation of an appropriate firing pin (not shown).
- a second firing pin 22, responsive to ignition of charge 20 is slidably mounted in the centrally apertured closed end 23 of traveling barrel 17 for igniting a second primer 24 that is centrally secured in the rearward closed end 25 of sub-caliber cartridge case 26.
- a retaining sleeve 27 is cemented to the interior surface of the traveling barrel 17 with its rearward end abutting the cartridge case circumferential. lip or flange 28 to secure the cartridge case 26 in the desired position within the traveling barrel.
- a second propellant charge 30, initiated by its primer 24, is located within the cartridge case 26 rearwardly of intermediately positioned wad means 31, 32 that separates the propellant charge 30 from the forwardly positioned shot load or mass 33.
- a suitable shotshell closure 34 normally retains the shot load 33 within the cartridge prior to firing of the round.
- the expendable traveling barrel 17 is separated from obturator 15 and is propelled toward the muzzle end of launching tube 11, as the firing pin 22 actuates a delay ignition of propellant charge 30 that produces a second and relatively higher gas pressure build-up within tube 11 and at a higher velocity propels the shot mass 33 out the muzzle end of tne expendable traveling barrel 17 and launching tube 11.
- the cartridge case 26 and retaining sleeve have been eliminated, and the propellant charge 30, wad means 31, 32, shot. mass 33 and its closure 34 are placed directly in the traveling barrel 17 with the same relative positioning to form a sub-caliber cartridge.
- the second primer 24A is positioned in an appropriate central cavity or recess provided in the base of the expendable traveling barrel 17.
- a cylindrical traveling barrel having a substantially closed rearward end secured to said obturator, an open forward end, and a plurality of longitudinally spaced circumferential ridges for slidably mounting said traveling barrel within said launching tube, said traveling barrel rearward end having a central passage therethrough,
- a sub-caliber cartridge positioned within said traveling barrel and having a propellant charge and primer
- a firing pin positioned in said traveling barrel passage to initiate said sub-caliber cartridge primer when actuated by said obturator propellant charge.
- a retaining sleeve is secured to the traveling barrel and is positioned forwardly of and in abutment with a portion of said sub-caliber cartridge.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Casting Support Devices, Ladles, And Melt Control Thereby (AREA)
Abstract
ARRANGEMENT FOR LAUNCHING SUB-CALLER CARTRIDGES FROM EXISTING WEAPONS WHILE MAINTAINING THE WEAPON CAPABLE OF ITS NORMAL USE. A SUB-CALIBER CARTRIDGE IS POSITIONED WITHIN A TRAVELING BARREL FROM WHICH IT IS SEPARATED SUBSEQUENT TO JOINT INITIAL TRAVEL THROUGH A PORTION OF A LAUNCHING TUBE. SEPRATE PROPELLANT CHARGES ARE PROVIDED TO OBTAIN AN INITIAL LAUNCHING PRESSURE AND A SUBSEQUENT SEPARATION PRESSURE WITHIN THE LAUNCH TUBE.
Description
NOV. 9, 197] J GRANDY 3,618,250
LAUNCHING ARRANGEMENT FOR SUB-CALIBER PROJECTILES Filed Aug. 15, 1969 INVENTOR, ANDREW J.. GRANDY m. 1 2139 4, WMQ X. QM mronmnrs:
3,618,250 LAUNCHING ARRANGEMENT FOR SUB-CALIBER PRUJEC'HLES Andrew .1. Grandy, North Hills, Pa, assignor to the United tates of America as represented by the Secretary of the Army Filed Aug. 15, 196?, Ser. No. 850,462 int. Cl. F41c 21/10; F4211) 5/14 11.3. C]. 4277 2 Claims ABSTRACT OF THE lDlISClLOfiURE Arrangement for launching sub-caliber cartridges from existing weapons while maintaining the weapon capable of its normal use. A sub-caliber cartridge is positioned within a traveling barrel from which it is separated subsequent to joint initial travel through a portion of a launching tube. Separate propellant charges are provided to obtain an initial launching pressure and a subsequent separation pressure Within the launch tube.
The invention described herein may be manufactured, used, and licensed by or for the Government for governmental purposes without the payment to me of any royalty thereon.
The invention relates to weapon systems and, more particularly, to weapon systems for launching sub-caliber cartridges or projectiles.
It is an object of the invention to provide a sub-caliber cartridge launching arrangement for use in existing weapons which are readily capable of versatile operation with their normal cartridges.
Another object of the invention is to provide such an arrangement which is inexpensive and includes a lightweight, easily distinguishable cartridge.
It is a further object to provide such an arrangement that produces an increased muzzle velocity and energy accompanied by lower instantaneous recoil forces.
These and other objects, features and advantages will become more apparent from the following description and accompanying drawings in which:
FIG. 1 is a partial sectional view of a weapon arrangement embodying the principles of the invention.
FIG. 2 is a similar view of a modified arrangement.
The rifle stock (FIG. 1) has its launching tube 11 secured thereto by means (not shown). The inner end of the launching tube, rearward of its rifling groove means 12, is provided with annular recesses 13, 14 to accommodate similarly shaped peripheral portions of an obturator 15 that is secured to the rearward circumferential flange 16 of an expendable traveling barrel 17 by a light crimp or the equivalent. Preferably, the longitudinally spaced, circumferential flanges 16, 18 on the barrel 17 have predetermined peripheral dimensioning such that their outer surfaces can slidably function with clearance within or inside the lands or smallest dimensioning of the launch tube rifling grooves 12.
The obturator 15 has its forward face centrally recessed to contain a first propellant charge 20 that is initiated by its primer 21 upon actuation of an appropriate firing pin (not shown). A second firing pin 22, responsive to ignition of charge 20 is slidably mounted in the centrally apertured closed end 23 of traveling barrel 17 for igniting a second primer 24 that is centrally secured in the rearward closed end 25 of sub-caliber cartridge case 26.
3,618,25h Patented Nov. 9, 1971 A retaining sleeve 27 is cemented to the interior surface of the traveling barrel 17 with its rearward end abutting the cartridge case circumferential. lip or flange 28 to secure the cartridge case 26 in the desired position within the traveling barrel. A second propellant charge 30, initiated by its primer 24, is located within the cartridge case 26 rearwardly of intermediately positioned wad means 31, 32 that separates the propellant charge 30 from the forwardly positioned shot load or mass 33. A suitable shotshell closure 34 normally retains the shot load 33 within the cartridge prior to firing of the round.
Opon initiation of propellant charge 20, the expendable traveling barrel 17 is separated from obturator 15 and is propelled toward the muzzle end of launching tube 11, as the firing pin 22 actuates a delay ignition of propellant charge 30 that produces a second and relatively higher gas pressure build-up within tube 11 and at a higher velocity propels the shot mass 33 out the muzzle end of tne expendable traveling barrel 17 and launching tube 11.
In the FIG. 2 modification, the cartridge case 26 and retaining sleeve have been eliminated, and the propellant charge 30, wad means 31, 32, shot. mass 33 and its closure 34 are placed directly in the traveling barrel 17 with the same relative positioning to form a sub-caliber cartridge. In this instance, the second primer 24A is positioned in an appropriate central cavity or recess provided in the base of the expendable traveling barrel 17.
I wish it to be understood that I do not desire to be limited to the exact details of construction shown and described, for obvious modification will occur to a person skilled in the art.
I claim:
1. In a weapon having a launching tube with a forward bore muzzle end and a rearward bore breech end,
an obturator secured in said launching tube rearward end and containing a propellant charge and a primer,
a cylindrical traveling barrel having a substantially closed rearward end secured to said obturator, an open forward end, and a plurality of longitudinally spaced circumferential ridges for slidably mounting said traveling barrel within said launching tube, said traveling barrel rearward end having a central passage therethrough,
a sub-caliber cartridge positioned within said traveling barrel and having a propellant charge and primer, and
a firing pin positioned in said traveling barrel passage to initiate said sub-caliber cartridge primer when actuated by said obturator propellant charge.
2. The structure in accordance with claim 1 wherein a retaining sleeve is secured to the traveling barrel and is positioned forwardly of and in abutment with a portion of said sub-caliber cartridge.
References Cited UNITED STATES PATENTS 2,657,630 11/1953 Blacker l0265.2 X 3,403,624 10/1968 Fosler et a] 42l F X 3,416,401 12/1968 Golbeck et al 102--38 X BENJAMIN A. BORCHELT, Primary Examiner J. M. HANLEY, Assistant Examiner US. Cl. X.R.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US85046269A | 1969-08-15 | 1969-08-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3618250A true US3618250A (en) | 1971-11-09 |
Family
ID=25308175
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US850462A Expired - Lifetime US3618250A (en) | 1969-08-15 | 1969-08-15 | Launching arrangement for sub-caliber projectiles |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3618250A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3670651A (en) * | 1971-04-21 | 1972-06-20 | Avco Corp | Ammunition round |
| US4682528A (en) * | 1985-02-25 | 1987-07-28 | General Dynamics Land Systems, Inc. | Active protection system |
| US4694755A (en) * | 1986-04-09 | 1987-09-22 | Esperanza Y Cia, S.A. | Shell for firing practice |
| US5222996A (en) * | 1992-08-19 | 1993-06-29 | The United States Of America As Represented By The Secretary Of The Navy | Buoy launch container extender |
| US5811715A (en) * | 1994-01-11 | 1998-09-22 | Simbal Ab | Practice weapon for a carried recoilless anti-tank weapon |
| US20060236888A1 (en) * | 2005-04-20 | 2006-10-26 | Michael Brunn | Buckshot round |
| US20060260500A1 (en) * | 2004-02-06 | 2006-11-23 | Engel John W | High-pressure fixed munition for low-pressure launching system |
| US8365669B1 (en) * | 2011-08-24 | 2013-02-05 | Utm Ip Limited | Training cartridge |
| WO2018172198A1 (en) * | 2017-03-23 | 2018-09-27 | Rheinmetall Waffe Munition Gmbh | Adaptive projectile |
| DE102023116148A1 (en) * | 2023-06-20 | 2024-12-24 | Rws Gmbh | anti-drone projectile and ammunition |
-
1969
- 1969-08-15 US US850462A patent/US3618250A/en not_active Expired - Lifetime
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3670651A (en) * | 1971-04-21 | 1972-06-20 | Avco Corp | Ammunition round |
| US4682528A (en) * | 1985-02-25 | 1987-07-28 | General Dynamics Land Systems, Inc. | Active protection system |
| US4694755A (en) * | 1986-04-09 | 1987-09-22 | Esperanza Y Cia, S.A. | Shell for firing practice |
| US5222996A (en) * | 1992-08-19 | 1993-06-29 | The United States Of America As Represented By The Secretary Of The Navy | Buoy launch container extender |
| US5811715A (en) * | 1994-01-11 | 1998-09-22 | Simbal Ab | Practice weapon for a carried recoilless anti-tank weapon |
| US20060260500A1 (en) * | 2004-02-06 | 2006-11-23 | Engel John W | High-pressure fixed munition for low-pressure launching system |
| US7481167B2 (en) * | 2004-02-06 | 2009-01-27 | John Whitworth Engel | High-pressure fixed munition for low-pressure launching system |
| US20090095187A1 (en) * | 2004-02-06 | 2009-04-16 | Engel Ballistic Research Inc. | High-pressure fixed munition for low-pressure launching system |
| US7690310B2 (en) * | 2004-02-06 | 2010-04-06 | John Whitworth Engel | High-pressure fixed munition for low-pressure launching system |
| US20060236888A1 (en) * | 2005-04-20 | 2006-10-26 | Michael Brunn | Buckshot round |
| US7207273B2 (en) * | 2005-04-20 | 2007-04-24 | Michael Brunn | Buckshot round |
| US8365669B1 (en) * | 2011-08-24 | 2013-02-05 | Utm Ip Limited | Training cartridge |
| WO2018172198A1 (en) * | 2017-03-23 | 2018-09-27 | Rheinmetall Waffe Munition Gmbh | Adaptive projectile |
| DE102023116148A1 (en) * | 2023-06-20 | 2024-12-24 | Rws Gmbh | anti-drone projectile and ammunition |
| EP4481319A1 (en) * | 2023-06-20 | 2024-12-25 | RWS GmbH | Drone defense projectil and munition |
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