US3820464A - Variable sized fragment explosive projectile - Google Patents

Variable sized fragment explosive projectile Download PDF

Info

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
Authority
US
United States
Prior art keywords
cylinder
projectile
base
failure
cylinders
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
Application number
US00342023A
Inventor
L Dixon
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
US Department of Navy
Original Assignee
US Department of Navy
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by US Department of Navy filed Critical US Department of Navy
Priority to US00342023A priority Critical patent/US3820464A/en
Application granted granted Critical
Publication of US3820464A publication Critical patent/US3820464A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20Projectiles, 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
    • F42B12/22Projectiles, 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.

Landscapes

  • 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.
US00342023A 1973-03-09 1973-03-09 Variable sized fragment explosive projectile Expired - Lifetime US3820464A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US00342023A US3820464A (en) 1973-03-09 1973-03-09 Variable sized fragment explosive projectile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00342023A US3820464A (en) 1973-03-09 1973-03-09 Variable sized fragment explosive projectile

Publications (1)

Publication Number Publication Date
US3820464A true US3820464A (en) 1974-06-28

Family

ID=23340006

Family Applications (1)

Application Number Title Priority Date Filing Date
US00342023A Expired - Lifetime US3820464A (en) 1973-03-09 1973-03-09 Variable sized fragment explosive projectile

Country Status (1)

Country Link
US (1) US3820464A (en)

Cited By (38)

* Cited by examiner, † Cited by third party
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

Cited By (51)

* Cited by examiner, † Cited by third party
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
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
US20170167839A1 (en) * 2014-02-11 2017-06-15 Raytheon Company Shock-resistant fuzewell for munition
US9816793B2 (en) * 2014-02-11 2017-11-14 Raytheon Company Shock-resistant fuzewell for munition
US10184763B2 (en) 2014-02-11 2019-01-22 Raytheon Company Munition with nose kit connecting to aft casing connector
US10267607B2 (en) 2014-02-11 2019-04-23 Raytheon Company Munition with outer enclosure
US10401135B2 (en) 2014-02-11 2019-09-03 Raytheon Company Penetrator munition with enhanced fragmentation
US10520289B2 (en) 2014-02-11 2019-12-31 Raytheon Company Munition with multiple fragment layers
US10415939B2 (en) * 2014-03-14 2019-09-17 Hirtenberger Defence Europe GmbH Projectile
US10648783B2 (en) 2014-03-14 2020-05-12 Hirtenberger Defence Europe GmbH Projectile
US11105596B1 (en) 2016-03-22 2021-08-31 Northrop Grumman Systems Corporation Prefragmented warheads with enhanced performance
US10634472B1 (en) 2016-03-22 2020-04-28 Northrop Grumman Innovation Systems, Inc. Prefragmented warheads with enhanced performance
US11614311B1 (en) 2016-03-22 2023-03-28 Northrop Grumman Systems Corporation Prefragmented warheads with enhanced performance
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
US11454480B1 (en) 2019-06-12 2022-09-27 Corvid Technologies LLC Methods for forming munitions casings and casings and munitions formed thereby
US11747122B1 (en) 2019-06-12 2023-09-05 Corvid Technologies LLC Methods for forming munitions casings and casings and munitions formed thereby
US20220252381A1 (en) * 2019-07-04 2022-08-11 Cta International Telescoped ammunition comprising a shell
US11796293B2 (en) * 2019-07-04 2023-10-24 Cta International Telescoped ammunition comprising a shell
JP2021071246A (en) * 2019-10-31 2021-05-06 ダイキン工業株式会社 warhead
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
RU2772649C1 (en) * 2021-04-23 2022-05-23 Акционерное общество "Научно-производственное объединение "Прибор" имени С.С. Голембиовского" Shot for an automatic grenade launcher

Similar Documents

Publication Publication Date Title
US3820464A (en) Variable sized fragment explosive projectile
US2798431A (en) Fragmentation warhead
US8161884B1 (en) System and method for explosively stamping a selective fragmentation pattern
US4305333A (en) Warhead for projectiles and rockets
US4108074A (en) Frangible target practice projectile
US8276520B1 (en) Adaptive fragmentation mechanism to enhance lethality
US3566794A (en) Controlled fragmentation of multi-walled warheads
US4497253A (en) Armor-piercing projectile
US6619210B1 (en) Explosively formed penetrator (EFP) and fragmenting warhead
US3913483A (en) Grenade with fuze
US3677183A (en) Pre-shaped fragmentation device
US3247795A (en) Spinning projectile for smooth bore guns
US5325787A (en) Armor-piercing fragmentation projectile
US5291833A (en) Armor-piercing fragmentation subcaliber projectile
US5540156A (en) Selectable effects explosively formed penetrator warhead
US3714897A (en) Directed warhead
US6817299B1 (en) Fragmenting projectile having threaded multi-wall casing
US3081704A (en) Rod producing warhead
US8272329B1 (en) Selectable lethality warhead patterned hole fragmentation insert sleeves
US4974516A (en) Fragmentation bomb
US6325325B1 (en) Device for translational braking of a projectile on its trajectory
US3720168A (en) Elliptical warhead
US3490374A (en) Continuous rod warhead
US3906860A (en) Dual purpose projectile
US5445079A (en) Armor-piercing fragmentation projectile