US3820464A - Variable sized fragment explosive projectile - Google Patents
Variable sized fragment explosive projectile Download PDFInfo
- Publication number
- US3820464A US3820464A US00342023A US34202373A US3820464A US 3820464 A US3820464 A US 3820464A US 00342023 A US00342023 A US 00342023A US 34202373 A US34202373 A US 34202373A US 3820464 A US3820464 A US 3820464A
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- cylinder
- projectile
- base
- failure
- cylinders
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/22—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
Definitions
- This invention relates generally to fragmentation projectiles and more particularly to a projectile that may be field adjusted to produce various fragmentation size and patterns.
- Explosive fragmentation projectiles have been made and used against personnel and light vehicle targets to increase the zone of lethality.
- the projectile is made of a cylindrical shell of metal having a scored failure grid pattern filled with an explosive which detonates on impact.
- the explosive force causes the shell to fracture at the failure grids to produce and disperse the individual fragments to the surrounding zone.
- the size and mass of the fragments determine the velocity and distribution of the fragments, which is fixed by the size of the failure grid pattern at the time of manufacture.
- a suggested solution to the logistics problem would be to supply projectiles having a plurality of different size failure grid patterns to produce various sized fragments from the one shell. But the use of this type of projectile is inefiicient against both types of targets mentioned.
- an object of the present invention is to provide a new and improved fragmentation projectile.
- Another object of the instant invention is to provide a fragmentation projectile having selectable fragment size capability.
- a further object of the present invention is to provide a fragmentation projectile capable of field adjustment for fragment size.
- Still another object of the instant invention is to provide a single fragmentation projectile for efficient use against various type targets.
- a still further object of the present invention is to provide a fragmentation projectile for use against various targets and presents minimal logistics problems.
- a fragmentation projectile comprising at least two hollow concentric cylinders, each having a failure grid pattern, telescoped together to form a shell that is connected to a projectile base. Serrations formed around one edge of each cylinder mate with corresponding serrations formed on the base of the projectile. Releasable securing means permit relative rotation of the cylinders to align or misalign the failure grid pattern and preclude further relative rotation to the base when secured.
- FIG. 1 is a pictorial view, partially cut away, of the projectile of the instant invention
- FIG. 2 is a cross-sectional view of the projectile having three cylinders with their failure grids in alignment before and after detonation;
- FIG. 3 is a plan view from the inside of the cylinders showing the failure grids in perfect alignment
- FIG. 4 is a cross-sectional view of the projectile showing the three cylinders with their failure grids out of alignment, before and after detonation;
- FIG. 5 is a plan view from the inside of the cylinders showing the failure grids out of alignment.
- FIG. 1 a fragmentation projectile 10 having an ogive nose 12 carrying a fuze 14.
- the ogive nose 12 is affixed to one end of an inner cylinder 16, the other end of which is affixed to a base 18.
- An explosive 20 fills the interior of the nose, inner cylinder, and base.
- a first movable cylinder 22 fitting the inner cylinder snugly but rotatably.
- the top edge is contoured to smoothly conform to the ogive nose 12, and the bottom edge has serrations 24 all around.
- a second movable cylinder 26 fitting the first cylinder snugly but rotatably.
- the top edge is also contoured to smoothly conform to the ogive nose and the bottom edge has serrations 28 all around.
- the base 18 of the projectile 10 has serrations 30 around its top edge outside the inner cylinder 16.
- a headless set screw 32 having an allen socket or the like, is threadably engaged in the first movable cylinder 22, thus permitting it to be lifted out of engagement with the serration 24 and 30, rotated, and subsequently locked by the set screw to the inner cylinder 16.
- the second movable cylinder 26 also has a similar set screw 34 threadably engaged therein and an access slot 36 formed over the set screw 32 in the'first movable cylinder 22. Thus, access may be gained to set screw 32 and set screw 34 may be set up against the first movable cylinder after the second movable cylinder is lifted out of engagement with the serrations 28 and 30 and rotation adjustment has been completed.
- a plurality of V grooves, arranged to form a diamond-shaped failure grid pattern 38 are scored, rolled, molded, electrochemically machined, or otherwise formed in any wellknown manner in the inside surface of each of the cylinders 16, 22, and 26.
- these failure grid patterns 38 are aligned radially from the inner cylinder 16 to the first movable cylinder 22 and the second movable cylinder 26. Immediately after detonation all the cylinders are shown ruptured at the failure grid into substantial equal sized fragments. This aligned arrangement produces the least number of fragments of the largest size.
- failure grid patterns 38 are misaligned from one cylinder to another by one-third the grid pattern interval. the maximum possible misalignment.
- the inner cylinder 16 is shown ruptured at the failure grid 38.
- the first movable cylinder 22 is shown ruptured randomly over the inner cylinders failure grid as well as at its own failure grid.
- the second movable cylinder 26 is shown ruptured randomly over both the inner and first movably cylinder failure grid as well as I at its own failure grid.
- the relative number of fragments from cylinder to cylinder can be shown by the ratio 1:429, and thus this arrangement produces the most number of the smallest fragments.
- variable-sized fragment explosive projectile comprising:
- a hollow inner cylinder having a failure grid pattern formed thereon affixed at one end to said base;
- At least one hollow rotatable cylinder having a failure grid pattern formed thereon concentric with said inner cylinder, whereby said rotatable cylinder may be rotated relative to said inner cylinder to place said failure grid patterns in alignment or misalignment;
- variable-sized fragment explosive projectile of claim 1 wherein said locking means comprises:
- variable-sized fragment explosive projectile of claim 2 wherein said locking means further comprises:
- variable-sized fragment explosive projectile of claim 3 further comprising:
- variable-sized fragment explosive projectile of claim 4 further comprising an opening in said second rotatable cylinder to provide access to said set screw.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
A fragmentation projectile having a plurality of telescoping hollow concentric cylinders, each having a scored, failure, grid pattern, forming the shell of the projectile filled with an explosive. The outer cylinders may be manually rotated in the field prior to firing so as to align or misalign the failure grids of one cylinder to another to produce various fragment size and patterns. Mating serrations on the shell base and the cylinders lock the cylinders in the selected position.
Description
United States Patent [191 [111 3,820,464 Dixon 1 1 June 28, 1974 1 VARIABLE SIZED FRAGMENT EXPLOSIVE PROJECTILE Inventor: Lewis C. Dixon, Mount Airy. Md.
The United States of America as represented by the Secretary of the Navy, Washington, DC.
Filed: Mar. 9, 1973 Appl. N0.: 342,023
Assignee:
U.S. Cl. 102/67 Int. Cl. F42b 13/48 Field of Search 102/64, 67
References Cited UNITED STATES PATENTS 12/1939 Cobain 102/64 1/1965 Urdapilleta 102/64 ROTATABLE CYLINDER To BASE S FOREIGN PATENTS OR APPLICATIONS 1,142,716 2/1969 Great Britain 102/67 Primary Examiner-Verlin R. Pendegrass Donn McGiehan ABSTRACT A fragmentation projectile having a plurality of telescoping hollow concentric cylinders, each having a scored, failure, grid pattern, forming the shell of the projectile filled with an explosive. The outer cylinders may be manually rotated in the field prior to tiring so as to align or misalign the failure grids of one cylinder to another to produce various fragment size and patterns. Mating serrations on the shell base and the cylinders lock the cylinders in the selected position.
5 Claims, 5 Drawing Figures SERRATIONS LOCKING PATENTEDJUHZB m4 3820.464
sum .1 or 3 g: SERRATIONS LOCKING ROTATABLE CYLINDERS TO BASE PATENTEDJUH 28 1914 SHEET 2- OF 3 BEFORE DETONATIQN IMMEDIATEL AFTER DETON BEFORE IMMEDIATELY 4= 9 '6 DETONATIQN AFTER DETONATION VARIABLE SIZED FRAGMENT EXPLOSIV E PROJECTILE BACKGROUND OF THE INVENTION This invention relates generally to fragmentation projectiles and more particularly to a projectile that may be field adjusted to produce various fragmentation size and patterns.
Explosive fragmentation projectiles have been made and used against personnel and light vehicle targets to increase the zone of lethality. Typically the projectile is made of a cylindrical shell of metal having a scored failure grid pattern filled with an explosive which detonates on impact. The explosive force causes the shell to fracture at the failure grids to produce and disperse the individual fragments to the surrounding zone. The size and mass of the fragments determine the velocity and distribution of the fragments, which is fixed by the size of the failure grid pattern at the time of manufacture. However, it is desirable to use small and light fragments having a high velocity and a broad distribution against a personnel target. It is also desirable to use large, massive fragments having high penetration capability against vehicular target. In the past, this selectability has been achieved by provisioning the forces with a variety of projectiles having difference size and mass fragmentation capability. But this obviously leads to logistic problems of inventory, shipment, handling and storage.
A suggested solution to the logistics problem would be to supply projectiles having a plurality of different size failure grid patterns to produce various sized fragments from the one shell. But the use of this type of projectile is inefiicient against both types of targets mentioned.
Another suggestion found in the prior art is to make a projectile having two telescoping concentric cylinders each having fracture grid patterns of the same size that may be superimposed or not at the time of manufacture. The two orientations produce difference sized fragments having difierent speed and trajectory. But again there is the logistics problem, because the projectile must be selected in the field for the intended target.
SUMMARY OF THE INVENTION Accordingly an object of the present invention is to provide a new and improved fragmentation projectile.
Another object of the instant invention is to provide a fragmentation projectile having selectable fragment size capability.
A further object of the present invention is to provide a fragmentation projectile capable of field adjustment for fragment size.
Still another object of the instant invention is to provide a single fragmentation projectile for efficient use against various type targets.
A still further object of the present invention is to provide a fragmentation projectile for use against various targets and presents minimal logistics problems.
Briefly, these and other objects of the present invention are attained by the use of a fragmentation projectile comprising at least two hollow concentric cylinders, each having a failure grid pattern, telescoped together to form a shell that is connected to a projectile base. Serrations formed around one edge of each cylinder mate with corresponding serrations formed on the base of the projectile. Releasable securing means permit relative rotation of the cylinders to align or misalign the failure grid pattern and preclude further relative rotation to the base when secured.
BRIEF DESCRIPTION OF THE DRAWING A more complete understanding of the invention and many of the attendant advantages thereof will be readily appreciated as the same become better understood by reference to the following detailed description when considered in connection with the accompanying drawings, wherein:
FIG. 1 is a pictorial view, partially cut away, of the projectile of the instant invention;
FIG. 2 is a cross-sectional view of the projectile having three cylinders with their failure grids in alignment before and after detonation;
FIG. 3, is a plan view from the inside of the cylinders showing the failure grids in perfect alignment;
FIG. 4 is a cross-sectional view of the projectile showing the three cylinders with their failure grids out of alignment, before and after detonation; and
FIG. 5 is a plan view from the inside of the cylinders showing the failure grids out of alignment.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawings, wherein like reference numerals designate corresponding parts throughout the several views there is shown generally in FIG. 1 a fragmentation projectile 10 having an ogive nose 12 carrying a fuze 14. The ogive nose 12 is affixed to one end of an inner cylinder 16, the other end of which is affixed to a base 18. An explosive 20 fills the interior of the nose, inner cylinder, and base.
Surrounding the inner cylinder 16, is a first movable cylinder 22 fitting the inner cylinder snugly but rotatably. The top edge is contoured to smoothly conform to the ogive nose 12, and the bottom edge has serrations 24 all around. Surrounding the first movable cylinder 22 is a second movable cylinder 26, fitting the first cylinder snugly but rotatably. The top edge is also contoured to smoothly conform to the ogive nose and the bottom edge has serrations 28 all around. The base 18 of the projectile 10 has serrations 30 around its top edge outside the inner cylinder 16. A headless set screw 32, having an allen socket or the like, is threadably engaged in the first movable cylinder 22, thus permitting it to be lifted out of engagement with the serration 24 and 30, rotated, and subsequently locked by the set screw to the inner cylinder 16. The second movable cylinder 26 also has a similar set screw 34 threadably engaged therein and an access slot 36 formed over the set screw 32 in the'first movable cylinder 22. Thus, access may be gained to set screw 32 and set screw 34 may be set up against the first movable cylinder after the second movable cylinder is lifted out of engagement with the serrations 28 and 30 and rotation adjustment has been completed.
Referring now to FIGS. 2 and 3, in regard to the operation of the fragmentation projectile, a plurality of V grooves, arranged to form a diamond-shaped failure grid pattern 38 are scored, rolled, molded, electrochemically machined, or otherwise formed in any wellknown manner in the inside surface of each of the cylinders 16, 22, and 26. As shown in FIGS. 2 and 3, these failure grid patterns 38 are aligned radially from the inner cylinder 16 to the first movable cylinder 22 and the second movable cylinder 26. Immediately after detonation all the cylinders are shown ruptured at the failure grid into substantial equal sized fragments. This aligned arrangement produces the least number of fragments of the largest size.
Referring now to FIGS. 4 and 5, further showing the operation of the fragmentation projectile, failure grid patterns 38 are misaligned from one cylinder to another by one-third the grid pattern interval. the maximum possible misalignment. Immediately after detonation the inner cylinder 16 is shown ruptured at the failure grid 38. The first movable cylinder 22 is shown ruptured randomly over the inner cylinders failure grid as well as at its own failure grid. The second movable cylinder 26 is shown ruptured randomly over both the inner and first movably cylinder failure grid as well as I at its own failure grid. The relative number of fragments from cylinder to cylinder can be shown by the ratio 1:429, and thus this arrangement produces the most number of the smallest fragments.
Obviously many modifications and variations of the present invention are possible in light of the above teachings. For example only two movable cylinders or more than three may be used. The failure grid pattern may be of different size from cylinder to cylinder, and vary in the same cylinder. Further, other methods of locking the movable cylinders may be used. It is therefore to be understood that within the scope of the appended claims, the invention may be practiced otherwise than specifically described.
What is claimed as new and desired to be secured by letters Patent of the United States is:
l. A variable-sized fragment explosive projectile comprising:
a base;
a hollow inner cylinder having a failure grid pattern formed thereon affixed at one end to said base;
a nose affixed to the other end of said cylinder; i
an explosive filling said cylinder between said base and said nose;
at least one hollow rotatable cylinder having a failure grid pattern formed thereon concentric with said inner cylinder, whereby said rotatable cylinder may be rotated relative to said inner cylinder to place said failure grid patterns in alignment or misalignment; and
means for locking said rotatable cylinder against relative movement to said inner cylinder.
2. The variable-sized fragment explosive projectile of claim 1, wherein said locking means comprises:
a set of serrations on said base; and
a serrated edge on the base end of said rotatable cylinder coacting with said set of serrations on said base.
3. The variable-sized fragment explosive projectile of claim 2, wherein said locking means further comprises:
a set screw threadably engaged in said rotatable cylinder and contactable with said inner cylinder for maintaining said coacting serrations in releasable contact.
4. The variable-sized fragment explosive projectile of claim 3 further comprising:
a second hollow rotatable cylinder having a failure grid pattern formed thereon concentric with said at least one rotatable cylinder; and
means for locking said second rotatable cylinder against relative movement to said at least one rotatable cylinder and said inner cylinder.
5. The variable-sized fragment explosive projectile of claim 4 further comprising an opening in said second rotatable cylinder to provide access to said set screw.
Claims (5)
1. A variable-sized fragment explosive projectile comprising: a base; a hollow inner cylinder having a failure grid pattern formed thereon affixed at one end to said base; a nose affixed to the other end of said cylinder; an explosive filling said cylinder between said base and said nose; at least one hollow rotatable cylinder having a failure grid pattern formed thereon concentric with said inner cylinder, whereby said rotatable cylinder may be rotated relative to said inner cylinder to place said failure grid patterns in alignment or misalignment; and means for locking said rotatable cylinder against relative movement to said inner cylinder.
2. The variable-sized fragment explosive projectile of claim 1, wherein said locking means comprises: a set of serrations on said base; and a serrated edge on the base end of said rotatable cylinder coacting with said set of serrations on said base.
3. The variable-sized fragment explosive projectile of claim 2, wherein said locking means further comprises: a set screw threadably engaged in said rotatable cylinder and contactable with said inner cylinder for maintaining said coacting serrations in releasable contact.
4. The variable-sized fragment explosive projectile of claim 3 further comprising: a second hollow rotatable cylinder having a failure grid pattern formed thereon concentric with said at least one rotatable cylinder; and means for locking said second rotatable cylinder against relative movement to said at least one rotatable cylinder and said inner cylinder.
5. The variable-sized fragment explosive projectile of claim 4 further comprising an opening in said second rotatable cylinder to provide access to said set screw.
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US00342023A US3820464A (en) | 1973-03-09 | 1973-03-09 | Variable sized fragment explosive projectile |
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US00342023A US3820464A (en) | 1973-03-09 | 1973-03-09 | Variable sized fragment explosive projectile |
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Cited By (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2406178A1 (en) * | 1977-06-30 | 1979-05-11 | Michel Gerard | Anti-personnel and armour piercing projectile - has casing with high fragmentation outer layer and harder inner layer |
US4312274A (en) * | 1977-01-17 | 1982-01-26 | Whittaker Corporation | Method for selecting warhead fragment size |
US4448129A (en) * | 1979-11-30 | 1984-05-15 | Fabrique Nationale Herstal | Telescopic projectile |
EP0181539A1 (en) * | 1984-10-24 | 1986-05-21 | Rheinmetall GmbH | Submissile with hollow charge |
US4592283A (en) * | 1984-04-02 | 1986-06-03 | Aktiebolaget Bofors | Explosive shell case |
US4664035A (en) * | 1982-03-01 | 1987-05-12 | Science Applications International Corp. | Missile warheads |
US5040464A (en) * | 1977-05-31 | 1991-08-20 | The United States Of America As Represented By The Secretary Of The Navy | Controlled fragmentation with fragment mix |
US5131329A (en) * | 1989-12-07 | 1992-07-21 | Rheinmetall Gmbh | Fragmentation projectile |
US5157225A (en) * | 1983-04-19 | 1992-10-20 | The United States Of America As Represented By The Secretary Of The Navy | Controlled fragmentation warhead |
FR2678723A1 (en) * | 1981-06-26 | 1993-01-08 | France Etat | Explosive, particularly anti-aircraft, projectile, comprising a rotary directional-effect charge |
FR2685077A1 (en) * | 1991-12-13 | 1993-06-18 | Thomson Brandt Armements | Explosive device with programmable fragmentation |
US5313887A (en) * | 1990-05-23 | 1994-05-24 | J.E.M. Smoke Machine Company | Pyrotechnic device |
FR2704638A1 (en) * | 1993-04-30 | 1994-11-04 | Thomson Brandt Armements | Multi-function military charge |
US5540156A (en) * | 1993-08-16 | 1996-07-30 | The United States Of America As Represented By The Secretary Of The Army | Selectable effects explosively formed penetrator warhead |
FR2730558A1 (en) * | 1995-02-14 | 1996-08-14 | Tda Armements Sas | Fragmentation weapon with increased destructive power |
FR2778978A1 (en) * | 1996-11-22 | 1999-11-26 | Diehl Gmbh & Co | ARTILLERY PROJECTILE |
WO2001090683A1 (en) * | 2000-05-23 | 2001-11-29 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Fragment-generating warhead for attacking semi-hard technical targets |
US20020014177A1 (en) * | 2000-07-28 | 2002-02-07 | Giat Industries. | Explosive ammunition with fragmenting structure |
DE10151573A1 (en) * | 2001-10-23 | 2003-05-15 | Tdw Verteidigungstech Wirksys | Splinter protection to minimize collateral damage |
US6694888B2 (en) * | 2001-10-02 | 2004-02-24 | Bill Jopson | Frangible bullet |
US6817299B1 (en) | 2003-12-10 | 2004-11-16 | The United States Of America As Represented By The Secretary Of The Navy | Fragmenting projectile having threaded multi-wall casing |
US20040231551A1 (en) * | 2002-02-14 | 2004-11-25 | Doris Nebel Beal Inter Vivos Patent Trust | Projectile having frangible trailing end barrier and method |
US20050109234A1 (en) * | 2001-08-23 | 2005-05-26 | Lloyd Richard M. | Kinetic energy rod warhead with lower deployment angles |
US7451704B1 (en) * | 2003-03-20 | 2008-11-18 | The United States Of America As Represented By The Secretary Of The Army | Multifunctional explosive fragmentation airburst munition |
FR2961590A1 (en) * | 2010-06-16 | 2011-12-23 | Nexter Munitions | Bomb, has fragilization network formed by helical lines including pitch that is constant along rear cylindrical part, where pitch is regularly crossed along warhead front part, so that delimited splinters comprise same mass |
US8522685B1 (en) * | 2010-02-22 | 2013-09-03 | The United States Of America As Represented By The Secretary Of The Army | Multiple size fragment warhead |
US8627771B1 (en) * | 2009-09-21 | 2014-01-14 | The United States of America as Reperesented by the Secretary of the Army | Selectable fragment size fragmentation warhead |
US20170167839A1 (en) * | 2014-02-11 | 2017-06-15 | Raytheon Company | Shock-resistant fuzewell for munition |
RU2627505C1 (en) * | 2016-04-12 | 2017-08-08 | Роман Николаевич Серёгин | Shell body |
US10247531B1 (en) | 2016-09-30 | 2019-04-02 | The United States Of America As Represented By The Department Of The Navy | Monolithic fragmentation casing |
US10415939B2 (en) * | 2014-03-14 | 2019-09-17 | Hirtenberger Defence Europe GmbH | Projectile |
US10634472B1 (en) | 2016-03-22 | 2020-04-28 | Northrop Grumman Innovation Systems, Inc. | Prefragmented warheads with enhanced performance |
JP2021071246A (en) * | 2019-10-31 | 2021-05-06 | ダイキン工業株式会社 | warhead |
RU2772649C1 (en) * | 2021-04-23 | 2022-05-23 | Акционерное общество "Научно-производственное объединение "Прибор" имени С.С. Голембиовского" | Shot for an automatic grenade launcher |
US20220252381A1 (en) * | 2019-07-04 | 2022-08-11 | Cta International | Telescoped ammunition comprising a shell |
US11454480B1 (en) | 2019-06-12 | 2022-09-27 | Corvid Technologies LLC | Methods for forming munitions casings and casings and munitions formed thereby |
US11614311B1 (en) | 2016-03-22 | 2023-03-28 | Northrop Grumman Systems Corporation | Prefragmented warheads with enhanced performance |
US20230132848A1 (en) * | 2020-03-19 | 2023-05-04 | The Secretary Of State For Defence | Casing for a fragmentation weapon, fragmentation weapon, and method of manufacture |
-
1973
- 1973-03-09 US US00342023A patent/US3820464A/en not_active Expired - Lifetime
Cited By (51)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4312274A (en) * | 1977-01-17 | 1982-01-26 | Whittaker Corporation | Method for selecting warhead fragment size |
US5040464A (en) * | 1977-05-31 | 1991-08-20 | The United States Of America As Represented By The Secretary Of The Navy | Controlled fragmentation with fragment mix |
FR2406178A1 (en) * | 1977-06-30 | 1979-05-11 | Michel Gerard | Anti-personnel and armour piercing projectile - has casing with high fragmentation outer layer and harder inner layer |
US4448129A (en) * | 1979-11-30 | 1984-05-15 | Fabrique Nationale Herstal | Telescopic projectile |
FR2678723A1 (en) * | 1981-06-26 | 1993-01-08 | France Etat | Explosive, particularly anti-aircraft, projectile, comprising a rotary directional-effect charge |
US4664035A (en) * | 1982-03-01 | 1987-05-12 | Science Applications International Corp. | Missile warheads |
US5157225A (en) * | 1983-04-19 | 1992-10-20 | The United States Of America As Represented By The Secretary Of The Navy | Controlled fragmentation warhead |
US4592283A (en) * | 1984-04-02 | 1986-06-03 | Aktiebolaget Bofors | Explosive shell case |
EP0181539A1 (en) * | 1984-10-24 | 1986-05-21 | Rheinmetall GmbH | Submissile with hollow charge |
US5131329A (en) * | 1989-12-07 | 1992-07-21 | Rheinmetall Gmbh | Fragmentation projectile |
US5375523A (en) * | 1990-05-23 | 1994-12-27 | J.E.M. Smoke Machine Company, Ltd. | Pyrotechnic device |
US5313887A (en) * | 1990-05-23 | 1994-05-24 | J.E.M. Smoke Machine Company | Pyrotechnic device |
FR2685077A1 (en) * | 1991-12-13 | 1993-06-18 | Thomson Brandt Armements | Explosive device with programmable fragmentation |
FR2704638A1 (en) * | 1993-04-30 | 1994-11-04 | Thomson Brandt Armements | Multi-function military charge |
US5540156A (en) * | 1993-08-16 | 1996-07-30 | The United States Of America As Represented By The Secretary Of The Army | Selectable effects explosively formed penetrator warhead |
FR2730558A1 (en) * | 1995-02-14 | 1996-08-14 | Tda Armements Sas | Fragmentation weapon with increased destructive power |
FR2778978A1 (en) * | 1996-11-22 | 1999-11-26 | Diehl Gmbh & Co | ARTILLERY PROJECTILE |
WO2001090683A1 (en) * | 2000-05-23 | 2001-11-29 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Fragment-generating warhead for attacking semi-hard technical targets |
US20020014177A1 (en) * | 2000-07-28 | 2002-02-07 | Giat Industries. | Explosive ammunition with fragmenting structure |
US6857372B2 (en) * | 2000-07-28 | 2005-02-22 | Giat Industries | Explosive ammunition with fragmenting structure |
US20050109234A1 (en) * | 2001-08-23 | 2005-05-26 | Lloyd Richard M. | Kinetic energy rod warhead with lower deployment angles |
US6694888B2 (en) * | 2001-10-02 | 2004-02-24 | Bill Jopson | Frangible bullet |
DE10151573B4 (en) * | 2001-10-23 | 2004-04-29 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Splinter protection to minimize collateral damage |
DE10151573A1 (en) * | 2001-10-23 | 2003-05-15 | Tdw Verteidigungstech Wirksys | Splinter protection to minimize collateral damage |
US20040231551A1 (en) * | 2002-02-14 | 2004-11-25 | Doris Nebel Beal Inter Vivos Patent Trust | Projectile having frangible trailing end barrier and method |
US7121211B2 (en) * | 2002-02-14 | 2006-10-17 | Doris Nebel Beal Inter Vivos Patent Trust | Projectile having frangible trailing end barrier and method |
US7451704B1 (en) * | 2003-03-20 | 2008-11-18 | The United States Of America As Represented By The Secretary Of The Army | Multifunctional explosive fragmentation airburst munition |
US6817299B1 (en) | 2003-12-10 | 2004-11-16 | The United States Of America As Represented By The Secretary Of The Navy | Fragmenting projectile having threaded multi-wall casing |
US8627771B1 (en) * | 2009-09-21 | 2014-01-14 | The United States of America as Reperesented by the Secretary of the Army | Selectable fragment size fragmentation warhead |
US8522685B1 (en) * | 2010-02-22 | 2013-09-03 | The United States Of America As Represented By The Secretary Of The Army | Multiple size fragment warhead |
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