US3820463A - Shotgun grenade - Google Patents

Shotgun grenade Download PDF

Info

Publication number
US3820463A
US3820463A US00303154A US30315472A US3820463A US 3820463 A US3820463 A US 3820463A US 00303154 A US00303154 A US 00303154A US 30315472 A US30315472 A US 30315472A US 3820463 A US3820463 A US 3820463A
Authority
US
United States
Prior art keywords
grenade
shotgun
fuze
nose
explosive charge
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
US00303154A
Inventor
H Ross
G Leonard
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 US00303154A priority Critical patent/US3820463A/en
Application granted granted Critical
Publication of US3820463A publication Critical patent/US3820463A/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
    • F42B12/201Projectiles, 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 characterised by target class
    • F42B12/204Projectiles, 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 characterised by target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B30/00Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
    • F42B30/04Rifle grenades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile

Definitions

  • This invention relates to grenades. More particularly this invention relates to a grenade which can be loaded into a standard shotgun shell and launched by a stan dard shotgun.
  • Grenades which can be launched by conventional rifles and other small arms are known. These grenades, while they have gained wide spread use in warfare, have a drawback in that they require a launching device which must be attached to the muzzle of the rifle. They also have a drawback in that a special cartridge must be provided to initiate the launch. Still further they are not designed for stable flight.
  • Shotgun shells have been loaded with slugs which fragment upon impact witha target but, to the best of the inventors knowledge, there is no prior art record of a grenade of the stable flying type described herein having been launched by a shotgun from a shotgun shell.
  • the present invention resides in a grenade suitable for launching by a standard shotgun from a standard shotgun shell and in a method for launching the grenade.
  • the grenade is designed for stable flight and fragments upon detonation of an explosive charge by a fuze contained therein.
  • the fuze is activated and in turn detonates the explosive charge when the grenade strikes a target.
  • FIG. 1 is an exploded cut away view of a grenade and shotgun shell suitable for use in the practice of this invention.
  • FIG. 2 is a cross sectional view of a shotgun shell loaded with a grenade according to this invention.
  • FIG. 1 is an exploded, cut away view of grenade and shotgun shell according to this invention prior to assembly.
  • the shotgun shell which may be of any guage compatible with the sizes of the grenade parts is indicated by the numeral 10.
  • the grenade parts include a tail section 11, a fragmentation cylinder 12, a striker pin 13 with an opening 14 drilled through it to accomodate a shear pin 15, a striker guide 16, a detonator 17, an explosive charge 18, and a rifled nose 19.
  • the nose 19 has a reinforcing plate 20 fitted into it in the manner depicted in the drawing. Taken together, the striker pin, shear pin, striker guide and detonator constitute a fuze.
  • FIG. 2 is a cross sectional view of the grenade .of this invention assembled in a-conventional shotgun shell.
  • the numerals in FIG.2 correspond to the numerals in FIG. 1 and the view is self explanatory.
  • a cavity 21 which contains the powder charge of the shotgun shell is formed behind tail section 11 when the grenade is assembled in place in the shell.
  • the tail section 11 may be plastic
  • the fragmentation l2 cylinder steel, the striker pin 13 steel, the shear pin 15 and nose 19 may be lead and the reinforcing plate 20 stainless steel with a number of well known materials suitable for use in the detonator l7 and explosive charge 18.
  • striker pin 13 When a shotgun containing a shell loaded with a grenade as depicted in FIG. 2 is fired, striker pin 13 is retained in position by shear pin 15 until the grenade actually strikes a target. When a target is struck, shear pin 15 shears and the striker pin 13 activates detonator 17 which, in turn, almost instantaneously detonates explosive charge 18.
  • the rifled nose 19 and tail section 11 are very important to the invention.
  • the nose l9 imparts spin to the grenade. This spin plus the high drag of the tail section 11 stabilizes the grenade during flight.
  • the tail section 11 also serves as a gas seal.
  • Tests have shown the grenade of this invention to be very accurate and devastating.
  • a grenade designated to fit a standard 12 guage shotgun shell was fired from 30 yards at a 1 inch steel plate backed with a 2 inchpin board which was, in turn, further backed with celotex the following happened.
  • a l inch diameter hole was produced in the steel plate.
  • a 1 inch diameter hole was produced in the pine board.
  • the celotex backing was damaged by fragments.
  • an aluminum witness cylinder which was arranged concentrically about the point of impact received extensive blast damage.
  • a particularly attractive feature of the grenade design shown in the drawing is that its center of gravity is well forward and it is thus very stable in flight.
  • the center of gravity is located just forward of the rear end of the nose portion.
  • a shotgun grenade comprising:
  • a housing made up of a nose, a cylinder and a tail section within said tube in front of said powder charge;
  • an explosive charge and fuze within said housing said fuze being designed to detonate said explosive charge after the grenade has been fired from said shotgun shell by initiating said powder charge and has struck a target.
  • a shotgun grenade according to claim 2 which includes a fragmentation cylinder within said housing along with said explosive charge and fuze.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

A grenade comprising a nose, a fuze, a fragmentation cylinder, a tail section and an explosive charge loaded into a standard shotgun shell. The grenade is designed to fly in a stable state and to explode to produce fragments.

Description

nited States P616111 1191 1111 3,820,463
Leonard et al. June 28, 1974 SHOTGUN GRENADE 2,730,046 1/1956 Bergstrom et al. 102/56 x Y 2,780,995 2/1957 Migliaccio 102/56 x [75] Inventors Guy Leonard Chma Lake 2,872,864 2/1959 Barnes et a1. 102/38 Hubert 3 Bethel Island 2,940,391 6/1960 Brandt 102/33 both of Callf- 3.067,685 12/1962 Ludwig 102/38 3,101,053 8/1963 Stevenson et al 102/57 [73] Assgnee' 32 2122 211? ;:g; 3,650,213 3/1972 Abbott et al 102/38 Navy Washmgton Primary Examiner-Samuel Feinberg [22] Filed: Oct. 30, 1972 Assistant Examiner-H. J. Tudor Attorney, Agent, or FirmR. S. Sciascia; Roy Miller" [21] Appl. No.. 303,154
L. E. K. Pohl [52] US. Cl 102/38, 102/57, 102/68 [51] llnt. Cl. F42b 5/02, F42b 9/02 [57] ABS CT [58] Field Of Search 102/56, 57, 3s, 67, 68 A grenade P a nose, a fuze, a fragmematwn cyhnder, a tall sectlon and an exploslve charge loaded 56] References Cited into astandard shotgun shell. The grenade is designed UNITED STATES PATENTS to fly 1n a stable state and to explode to produce fragments. 2,426,239 8/1947 Renner'. 102/38 2,573,362 lO/l951 Rouse 102/38 4 Claims, 2 Drawing Figures SHOTGUN GRENADE BACKGROUND OF THE INVENTION 1. Field of the Invention This invention relates to grenades. More particularly this invention relates to a grenade which can be loaded into a standard shotgun shell and launched by a stan dard shotgun.
2. Description of the Prior Art Grenades which can be launched by conventional rifles and other small arms are known. These grenades, while they have gained wide spread use in warfare, have a drawback in that they require a launching device which must be attached to the muzzle of the rifle. They also have a drawback in that a special cartridge must be provided to initiate the launch. Still further they are not designed for stable flight.
Shotgun shells have been loaded with slugs which fragment upon impact witha target but, to the best of the inventors knowledge, there is no prior art record of a grenade of the stable flying type described herein having been launched by a shotgun from a shotgun shell.
SUMMARY OF THE INVENTION The present invention resides in a grenade suitable for launching by a standard shotgun from a standard shotgun shell and in a method for launching the grenade. The grenade is designed for stable flight and fragments upon detonation of an explosive charge by a fuze contained therein. The fuze is activated and in turn detonates the explosive charge when the grenade strikes a target.
BRIEF DESCRIPTION OF THE DRAWING FIG. 1 is an exploded cut away view of a grenade and shotgun shell suitable for use in the practice of this invention.
FIG. 2 is a cross sectional view of a shotgun shell loaded with a grenade according to this invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT Going first to the drawing, FIG. 1 is an exploded, cut away view of grenade and shotgun shell according to this invention prior to assembly. The shotgun shell which may be of any guage compatible with the sizes of the grenade parts is indicated by the numeral 10. The grenade parts include a tail section 11, a fragmentation cylinder 12, a striker pin 13 with an opening 14 drilled through it to accomodate a shear pin 15, a striker guide 16, a detonator 17, an explosive charge 18, and a rifled nose 19. The nose 19 has a reinforcing plate 20 fitted into it in the manner depicted in the drawing. Taken together, the striker pin, shear pin, striker guide and detonator constitute a fuze.
FIG. 2 is a cross sectional view of the grenade .of this invention assembled in a-conventional shotgun shell. The numerals in FIG.2 correspond to the numerals in FIG. 1 and the view is self explanatory. In the assembled view it is clear that a cavity 21 which contains the powder charge of the shotgun shell is formed behind tail section 11 when the grenade is assembled in place in the shell.
In fabricating the grenade a wide variety of choices exists in selecting the materials from which the various parta are made. For example, the tail section 11 may be plastic, the fragmentation l2 cylinder steel, the striker pin 13 steel, the shear pin 15 and nose 19 may be lead and the reinforcing plate 20 stainless steel with a number of well known materials suitable for use in the detonator l7 and explosive charge 18.
When a shotgun containing a shell loaded with a grenade as depicted in FIG. 2 is fired, striker pin 13 is retained in position by shear pin 15 until the grenade actually strikes a target. When a target is struck, shear pin 15 shears and the striker pin 13 activates detonator 17 which, in turn, almost instantaneously detonates explosive charge 18.
The rifled nose 19 and tail section 11 are very important to the invention. The nose l9 imparts spin to the grenade. This spin plus the high drag of the tail section 11 stabilizes the grenade during flight. The tail section 11 also serves as a gas seal.
Tests have shown the grenade of this invention to be very accurate and devastating. When a grenade designated to fit a standard 12 guage shotgun shell was fired from 30 yards at a 1 inch steel plate backed with a 2 inchpin board which was, in turn, further backed with celotex the following happened. A l inch diameter hole was produced in the steel plate. A 1 inch diameter hole was produced in the pine board. The celotex backing was damaged by fragments. And, an aluminum witness cylinder which was arranged concentrically about the point of impact received extensive blast damage.
It should be noted here that a particularly attractive feature of the grenade design shown in the drawing is that its center of gravity is well forward and it is thus very stable in flight. The center of gravity is located just forward of the rear end of the nose portion.
We claim:
1. In a shotgun shell comprising a tube with a closed rear end and a powder charge adjacent to said closed rear end, a shotgun grenade comprising:
a. a housing made up of a nose, a cylinder and a tail section within said tube in front of said powder charge; and
b. an explosive charge and fuze within said housing, said fuze being designed to detonate said explosive charge after the grenade has been fired from said shotgun shell by initiating said powder charge and has struck a target.
2. A shotgun grenade according to claim 1 wherein the nose is rifled to impart spin to the grenade.
3. A shotgun grenade according to claim 2 which includes a fragmentation cylinder within said housing along with said explosive charge and fuze.
l'lOI'.

Claims (4)

1. In a shotgun shell comprising a tube with a closed rear end and a powder charge adjacent to said closed rear end, a shotgun grenade comprising: a. a housing made up of a nose, a cylinder and a tail section within said tube in front of said powder charge; and b. an explosive charge and fuze within said housing, said fuze being designed to detonate said explosive charge after the grenade has been fired from said shotgun shell by initiating said powder charge and has struck a target.
2. A shotgun grenade according to claim 1 wherein the nose is rifled to impart spin to the grenade.
3. A shotgun grenade according to claim 2 which includes a fragmentation cylinder within said housing along with said explosive charge and fuze.
4. A shotgun grenade according to claim 3 wherein said tail section is shaped in a manner that a cavity to contain said powder charge is formed in its rear exterior.
US00303154A 1972-10-30 1972-10-30 Shotgun grenade Expired - Lifetime US3820463A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US00303154A US3820463A (en) 1972-10-30 1972-10-30 Shotgun grenade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00303154A US3820463A (en) 1972-10-30 1972-10-30 Shotgun grenade

Publications (1)

Publication Number Publication Date
US3820463A true US3820463A (en) 1974-06-28

Family

ID=23170755

Family Applications (1)

Application Number Title Priority Date Filing Date
US00303154A Expired - Lifetime US3820463A (en) 1972-10-30 1972-10-30 Shotgun grenade

Country Status (1)

Country Link
US (1) US3820463A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5000094A (en) * 1984-12-21 1991-03-19 Sullivan Leroy J Shotgun cartridge with explosive shell
US5189250A (en) * 1988-10-05 1993-02-23 Frag, Ltd. Projectile for smooth bore weapon
EP0801287A2 (en) * 1996-04-12 1997-10-15 DIEHL GMBH & CO. Fragmentation projectile with base fuze and cartridge case
WO1999051933A1 (en) * 1998-04-03 1999-10-14 Sabot Technologies, Inc. Sabot pressure wad
US20040079256A1 (en) * 2002-08-21 2004-04-29 Mcmurray Christopher R. Lead attached sabot slug
US8616129B1 (en) * 2011-08-19 2013-12-31 The United States Of America As Represented By The Secretary Of The Navy Cartridge actuator and method of manufacture thereof
US9010248B1 (en) * 2011-12-19 2015-04-21 The United States Of America As Represented By The Secretary Of The Army 40 mm gun sleeve cartridge case for M320 grenade launcher ammunition
US20170191810A1 (en) * 2015-08-23 2017-07-06 Ispra Ltd. Firearm projectile usable as a hand grenade
US9982978B2 (en) * 2014-12-16 2018-05-29 Rafael Advanced Defense Systems Ltd. Warhead for generating a blast on an extended region of a target surface
US11293730B1 (en) * 2016-06-14 2022-04-05 Douglas Burke Bullet projectile with enhanced mechanical shock wave delivery for warfare
US20220412706A1 (en) * 2017-06-23 2022-12-29 Douglas Burke Bullet projectile with internal hammer and post for enhanced mechanical shock wave delivery for demolition

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5000094A (en) * 1984-12-21 1991-03-19 Sullivan Leroy J Shotgun cartridge with explosive shell
US5189250A (en) * 1988-10-05 1993-02-23 Frag, Ltd. Projectile for smooth bore weapon
EP0801287A2 (en) * 1996-04-12 1997-10-15 DIEHL GMBH & CO. Fragmentation projectile with base fuze and cartridge case
EP0801287A3 (en) * 1996-04-12 1998-11-18 Diehl Stiftung & Co. Fragmentation projectile with base fuze and cartridge case
WO1999051933A1 (en) * 1998-04-03 1999-10-14 Sabot Technologies, Inc. Sabot pressure wad
US6067909A (en) * 1998-04-03 2000-05-30 Sabot Technologies, Inc. Sabot pressure wad
US20070119330A1 (en) * 2002-08-21 2007-05-31 Ra Brands, L.L.C. Lead Attached Sabot Slug
US7201104B2 (en) 2002-08-21 2007-04-10 Ra Brands, L.L.C. Lead attached sabot slug
US20040079256A1 (en) * 2002-08-21 2004-04-29 Mcmurray Christopher R. Lead attached sabot slug
US8261667B2 (en) 2002-08-21 2012-09-11 Ra Brands, L.L.C. Lead attached sabot slug
US8616129B1 (en) * 2011-08-19 2013-12-31 The United States Of America As Represented By The Secretary Of The Navy Cartridge actuator and method of manufacture thereof
US9010248B1 (en) * 2011-12-19 2015-04-21 The United States Of America As Represented By The Secretary Of The Army 40 mm gun sleeve cartridge case for M320 grenade launcher ammunition
US9982978B2 (en) * 2014-12-16 2018-05-29 Rafael Advanced Defense Systems Ltd. Warhead for generating a blast on an extended region of a target surface
US20170191810A1 (en) * 2015-08-23 2017-07-06 Ispra Ltd. Firearm projectile usable as a hand grenade
US9952025B2 (en) * 2015-08-23 2018-04-24 Yesh On Ltd. Firearm projectile usable as a hand grenade
US11293730B1 (en) * 2016-06-14 2022-04-05 Douglas Burke Bullet projectile with enhanced mechanical shock wave delivery for warfare
US20220412706A1 (en) * 2017-06-23 2022-12-29 Douglas Burke Bullet projectile with internal hammer and post for enhanced mechanical shock wave delivery for demolition
US11841214B2 (en) * 2017-06-23 2023-12-12 Douglas Burke Bullet projectile with internal hammer and post for enhanced mechanical shock wave delivery for demolition

Similar Documents

Publication Publication Date Title
US3877383A (en) Munition
US2674923A (en) Instruction device
US5107766A (en) Follow-thru grenade for military operations in urban terrain (MOUT)
US4648324A (en) Projectile with enhanced target penetrating power
US4096804A (en) Plastic/mischmetal incendiary projectile
US4488490A (en) Percussion initiated spotting charge
US4653404A (en) High velocity notched ammunition sabot
US3820463A (en) Shotgun grenade
US3013495A (en) Spotter-tracer projectile
JP7108685B2 (en) Fully armored safety bullet especially for multi-purpose use
US9389053B2 (en) 40mm door-breaching grenade
US3620162A (en) Rifle launched rocket
US3633510A (en) Dual mode fuze explosive train
JPS6158760B2 (en)
NO316339B1 (en) Br degree no degree stainless, ballistic blasting projectile
EP0171534B1 (en) Bullet trap and bullet deflector in rifle grenade
US3922967A (en) Closed-breech-gun-fired rocket-assisted projectile
US10030955B1 (en) Multi-purpose non-lethal blunt trauma grenade
RU2751328C1 (en) Projectile with a pyrotechnical battle charge
US3101053A (en) Combination fragmentation structural incendiary damage projectile
US5591935A (en) Shock sensing dual mode warhead
US4404911A (en) Self-sparging inertia armed nose fuze
US4013013A (en) Ordnance fuze time delay mechanism
US5612505A (en) Dual mode warhead
US4426932A (en) Contact fuze for mine munitions