US20040083920A1 - Fragment projectile - Google Patents

Fragment projectile Download PDF

Info

Publication number
US20040083920A1
US20040083920A1 US10/687,835 US68783503A US2004083920A1 US 20040083920 A1 US20040083920 A1 US 20040083920A1 US 68783503 A US68783503 A US 68783503A US 2004083920 A1 US2004083920 A1 US 2004083920A1
Authority
US
United States
Prior art keywords
projectile
fragment
fragments
heavy metal
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.)
Abandoned
Application number
US10/687,835
Inventor
Stefan Thiesen
Dieter Jungbluth
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.)
Rheinmetall W&M GmbH
Original Assignee
Rheinmetall W&M GmbH
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 Rheinmetall W&M GmbH filed Critical Rheinmetall W&M GmbH
Assigned to RHEINMETALL W & M GMBH reassignment RHEINMETALL W & M GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: JUNGBLUTH, DIETER, THIESEN, STEFAN
Publication of US20040083920A1 publication Critical patent/US20040083920A1/en
Abandoned 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
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/56Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
    • F42B12/58Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
    • F42B12/62Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
    • F42B12/64Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile the submissiles being of shot- or flechette-type

Definitions

  • the invention relates to a fragment projectile.
  • Fragment projectiles are known from, for example, German Patent No. DE 196 26 660 C2 corresponding to U.S. Pat. No. 5,900,580.
  • the subject of this patent is full-caliber projectiles having a projectile casing, which surrounds a hollow space that is filled in the front region with heavy-metal fragments. Additionally, an explosive charge is disposed inside the projectile casing. The charge is detonated at a predetermined time, and the fragments are accelerated, for example, in the direction of the target.
  • a drawback of fragment projectiles of this type is that they have a low rate of effectiveness, because the percentage by mass that causes the fragmentation effect is low relative to the projectile weight.
  • a fragment projectile comprising: a projectile casing that surrounds and defines a hollow space; heavy metal fragments at least partially filling the hollow space; and an ejector charge disposed at the rear of the hollow space to eject the fragments from the projectile casing when activated during the flight of the projectile.
  • the activation takes place at a predetermined time during flight due to a timer disposed on the projectile.
  • the invention is essentially based on the concept of omitting the use of explosives in the fragment projectile, and filling the space required for the explosive with fragments.
  • a relatively compact pyrotechnical ejector charge effects the ejection of the fragments at a desired, e.g., predetermined time.
  • the invention solves the problem of the firing reliability of explosives that is inherent to conventional fragment projectiles.
  • the fragment projectile As a subcaliber projectile in a simple manner. These projectiles possess a significantly higher muzzle velocity, and exhibit a much smaller drop in speed during flight. Furthermore, in fin-stabilized projectiles, the guidance assembly can be permanently mounted to the projectile. As a result, costs are further reduced and the hit probability is improved in comparison to full-caliber projectiles, in which collapsible guidance assemblies must usually be used.
  • FIGURE is a schematic cross-section view of a fin-stabilized sub-section projectile according to the invention providing with a propelling cage sabot
  • FIG. 1 there is shown a fin-stabilized, subcaliber fragment projectile 1 that is surrounded by an aluminum propelling cage sabot 2 , which is segmented in a known manner.
  • the projectile can be fired from a 120-mm caliber tank gun, for example.
  • the fragment projectile 1 includes a projectile casing 3 , having a hollow interior space 7 in which a packet of spherical fragments 4 comprised of heavy metal, e.g., tungsten (WSM), is disposed.
  • the projectile casing 3 also contains an ejector charge 5 at the rear of the hollow space and a programmable timer fuse 6 .
  • a fin stabilization unit 8 is affixed to the rear of the casing 3 .
  • the propellant cage sabot 2 initially is ejected in a known manner and the projectile 1 follows its flight trajectory to the vicinity of the target region.
  • the timer fuse 6 ignites the ejector charge 5 at a desired, in this case, predetermined time. The charge pushes the spherical fragments 4 out of the front of the projectile 1 by bursting the tip 7 .
  • predetermined fracture points are provided in the region of the projectile tip 7 . After the projectile tip 7 bursts, the residual projectile abruptly slows its speed because of the high air resistance. In contrast, at the time of the fragment ejection process, the relatively heavy spherical fragments 4 fly further into the target region at about the same original speed of the projectile.
  • the invention is not limited to the above-described exemplary embodiment.
  • non-spherical fragments can be used instead of spherical ones.
  • a heavy metal other than tungsten heavy metal can also be used as the fragment material.
  • the fragment projectile can also be spin-stabilized.
  • the timer fuse can also be replaced by a proximity fuse.

Abstract

A fragment projectile (1) that can be produced at low cost, and has a sufficient fragment distribution for combating targets, while avoiding the use of explosives in the interior of space (7) of the fragment projectile (1). Instead, the interior space (7) normally required for the explosive for such proximity is at least partially filled with heavy metal fragments (4) and a relatively compact pyrotechnical ejector charge (5) is provided to effect the ejection of the fragments (4) at a desired or predetermined time. The fragment projectile (1) should preferably be a sub caliber projectile to attain the highest possible fragment speed in the target region.

Description

    CROSS REFERENCE TO RELATED APPLICATION
  • This application claims the priority of German Patent Application, DE 102 48 696.4 filed Oct. 18, 2002 and which is incorporated herein by reference. [0001]
  • BACKGROUND OF THE INVENTION
  • The invention relates to a fragment projectile. [0002]
  • Fragment projectiles are known from, for example, German Patent No. DE 196 26 660 C2 corresponding to U.S. Pat. No. 5,900,580. The subject of this patent is full-caliber projectiles having a projectile casing, which surrounds a hollow space that is filled in the front region with heavy-metal fragments. Additionally, an explosive charge is disposed inside the projectile casing. The charge is detonated at a predetermined time, and the fragments are accelerated, for example, in the direction of the target. [0003]
  • A drawback of fragment projectiles of this type is that they have a low rate of effectiveness, because the percentage by mass that causes the fragmentation effect is low relative to the projectile weight. [0004]
  • SUMMARY OF THE INVENTION
  • It is the object of the invention to provide a fragment projectile that can be produced at a low cost and has a sufficient fragment distribution in the target region for combating targets. [0005]
  • In accordance with the invention, this object generally is accomplished by a fragment projectile, comprising: a projectile casing that surrounds and defines a hollow space; heavy metal fragments at least partially filling the hollow space; and an ejector charge disposed at the rear of the hollow space to eject the fragments from the projectile casing when activated during the flight of the projectile. Preferably, the activation takes place at a predetermined time during flight due to a timer disposed on the projectile. Further advantageous embodiments of the invention are disclosed. [0006]
  • The invention is essentially based on the concept of omitting the use of explosives in the fragment projectile, and filling the space required for the explosive with fragments. A relatively compact pyrotechnical ejector charge effects the ejection of the fragments at a desired, e.g., predetermined time. [0007]
  • In addition to offering a less expensive production of such projectiles, the invention solves the problem of the firing reliability of explosives that is inherent to conventional fragment projectiles. [0008]
  • To avoid the dramatic drop in projectile speed, and thus of the fragments during flight, that occurs in full-caliber projectiles, it has proven advantageous to construct the fragment projectile as a subcaliber projectile in a simple manner. These projectiles possess a significantly higher muzzle velocity, and exhibit a much smaller drop in speed during flight. Furthermore, in fin-stabilized projectiles, the guidance assembly can be permanently mounted to the projectile. As a result, costs are further reduced and the hit probability is improved in comparison to full-caliber projectiles, in which collapsible guidance assemblies must usually be used. [0009]
  • While a sub caliber projectile offers less space for the fragments, the available space typically suffices for effective target combat, e.g., the threat of armored defense weapons in a protective position or light-armored vehicles, because of the absence of the explosive charge. [0010]
  • Further details about and advantages of the invention ensue from the following exemplary embodiment explained in conjunction with a FIGURE. [0011]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The FIGURE is a schematic cross-section view of a fin-stabilized sub-section projectile according to the invention providing with a propelling cage sabot[0012]
  • DETAILED DESCRIPTION OF THE INVENTION
  • Referring now to the FIGURE, there is shown a fin-stabilized, [0013] subcaliber fragment projectile 1 that is surrounded by an aluminum propelling cage sabot 2, which is segmented in a known manner. The projectile can be fired from a 120-mm caliber tank gun, for example.
  • The [0014] fragment projectile 1 includes a projectile casing 3, having a hollow interior space 7 in which a packet of spherical fragments 4 comprised of heavy metal, e.g., tungsten (WSM), is disposed. The projectile casing 3 also contains an ejector charge 5 at the rear of the hollow space and a programmable timer fuse 6. A fin stabilization unit 8 is affixed to the rear of the casing 3.
  • In the intended use of the [0015] fragment projectile 1 of the invention, after the projectile exits the gun barrel, not shown, the propellant cage sabot 2 initially is ejected in a known manner and the projectile 1 follows its flight trajectory to the vicinity of the target region. There, the timer fuse 6 ignites the ejector charge 5 at a desired, in this case, predetermined time. The charge pushes the spherical fragments 4 out of the front of the projectile 1 by bursting the tip 7.
  • To assure a reproducible ejection of the [0016] spherical fragments 4, predetermined fracture points, not shown in the FIGURE, are provided in the region of the projectile tip 7. After the projectile tip 7 bursts, the residual projectile abruptly slows its speed because of the high air resistance. In contrast, at the time of the fragment ejection process, the relatively heavy spherical fragments 4 fly further into the target region at about the same original speed of the projectile.
  • Of course, the invention is not limited to the above-described exemplary embodiment. For example, non-spherical fragments can be used instead of spherical ones. A heavy metal other than tungsten heavy metal can also be used as the fragment material. Furthermore, the fragment projectile can also be spin-stabilized. Finally, the timer fuse can also be replaced by a proximity fuse. [0017]
  • The invention now being fully described, it will be apparent to one of ordinary skill in the art that many changes and modifications can be made thereto without departing from the spirit or scope of the invention as set forth herein. [0018]

Claims (9)

What is claimed is:
1. A fragment projectile, comprising:
a projectile casing having a hollow interior space;
heavy metal fragments at least partially filling the hollow space;
an ejector charge disposed at the rear of the hollow space to eject the fragments from the projectile casing, when activated, during the flight of the projectile; and
means for activating the ejector charge at a desired time during the flight of the projectile.
2. The projectile according to claim 1, wherein the means for activating, activates the charge at a predetermined time during the flight of the projectile.
3. The projectile according to claim 2, wherein the means for activating is a timer.
4. The fragment projectile according to claim 1, wherein the fragment projectile is a subcaliber projectile provided with a propelling cage sabot.
5. The fragment projectile according to claim 4, wherein the fragments are spherical.
6. The fragment projectile according to claim 5, wherein the fragments comprise tungsten heavy metal.
7. The fragment projectile according claim 1, wherein the means for activating includes a timer or proximity fuse to ignite the ejector charge.
8. The fragment projectile according to claim 1, wherein the fragments are spherical.
9. The fragment projectile according claim 8, wherein the fragments are formed of tungsten heavy metal.
US10/687,835 2002-10-18 2003-10-20 Fragment projectile Abandoned US20040083920A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10248696.4 2002-10-18
DE10248696A DE10248696A1 (en) 2002-10-18 2002-10-18 splitter floor

Publications (1)

Publication Number Publication Date
US20040083920A1 true US20040083920A1 (en) 2004-05-06

Family

ID=27798341

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/687,835 Abandoned US20040083920A1 (en) 2002-10-18 2003-10-20 Fragment projectile

Country Status (5)

Country Link
US (1) US20040083920A1 (en)
EP (1) EP1411317B1 (en)
DE (2) DE10248696A1 (en)
IL (1) IL158449A (en)
NO (1) NO327288B1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2497066C1 (en) * 2012-07-17 2013-10-27 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом"-Госкорпорация "Росатом" Hitting element of cassette fragmentation round
CN115355774A (en) * 2022-07-28 2022-11-18 中国人民解放军63856部队 Small-caliber infantry grenade fragment space distribution test method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4970960A (en) * 1980-11-05 1990-11-20 Feldmann Fritz K Anti-material projectile
US5872327A (en) * 1988-06-25 1999-02-16 Rheinmetall Industrie Aktiengesellschaft Subcaliber, spin stabilized multi-purpose projectile
US5900580A (en) * 1996-07-03 1999-05-04 Diehl Stiftung & Co. Explosive projectile
US6041713A (en) * 1997-05-30 2000-03-28 Rheinmetall W & M Gmbh Practice projectile
US6129024A (en) * 1997-11-19 2000-10-10 Oerlikon Contraves Ag Projectile with a programmable time fuse
US6536351B2 (en) * 2000-11-21 2003-03-25 Rheinmetall W & M Gmbh Warhead

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE77C (en) * 1877-07-07 GANZ & CO. in Ratibor Construction of double ring shrapnel
BE676051A (en) * 1965-02-12 1966-06-16
DE19524726B4 (en) * 1994-08-10 2006-05-24 Rheinmetall W & M Gmbh warhead

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4970960A (en) * 1980-11-05 1990-11-20 Feldmann Fritz K Anti-material projectile
US5872327A (en) * 1988-06-25 1999-02-16 Rheinmetall Industrie Aktiengesellschaft Subcaliber, spin stabilized multi-purpose projectile
US5900580A (en) * 1996-07-03 1999-05-04 Diehl Stiftung & Co. Explosive projectile
US6041713A (en) * 1997-05-30 2000-03-28 Rheinmetall W & M Gmbh Practice projectile
US6129024A (en) * 1997-11-19 2000-10-10 Oerlikon Contraves Ag Projectile with a programmable time fuse
US6536351B2 (en) * 2000-11-21 2003-03-25 Rheinmetall W & M Gmbh Warhead

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2497066C1 (en) * 2012-07-17 2013-10-27 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом"-Госкорпорация "Росатом" Hitting element of cassette fragmentation round
CN115355774A (en) * 2022-07-28 2022-11-18 中国人民解放军63856部队 Small-caliber infantry grenade fragment space distribution test method

Also Published As

Publication number Publication date
EP1411317B1 (en) 2008-10-08
IL158449A (en) 2012-07-31
NO20033393L (en) 2004-04-19
NO327288B1 (en) 2009-06-02
NO20033393D0 (en) 2003-07-30
DE10248696A1 (en) 2004-04-29
IL158449A0 (en) 2004-09-27
EP1411317A1 (en) 2004-04-21
DE50310603D1 (en) 2008-11-20

Similar Documents

Publication Publication Date Title
US4882996A (en) Explosive projectile assembly with a projectile body
RU2275585C2 (en) Method for control of missile flight direction and missile
US3877383A (en) Munition
US6722283B1 (en) Controlled terminal kinetic energy projectile
EP0597142B1 (en) A practice projectile
JP2004501339A (en) Self-propelled projectile with penetrating core
US8528480B2 (en) Warhead
US4498394A (en) Arrangement for a terminally guided projectile provided with a target seeking arrangement and path correction arrangement
JPS6158760B2 (en)
US6988450B1 (en) Anti-personnel ammunition
US6981450B1 (en) Grenade dispense mechanism for non-spin dual purpose improved conventional munitions
US2091635A (en) Projectile
US20040083920A1 (en) Fragment projectile
KR102662184B1 (en) Device and method for attenuating contact-impact events of elongated sub-projectiles
EP0735342B1 (en) Munition to self-protect a tank
US6895864B2 (en) Subcalibre kinetic energy projectile
CA2534842C (en) Universal ke projectile, in particular for medium-calibre munitions
EP0895054B1 (en) Cover for a shaped charge projectile
RU2080548C1 (en) Multipurpose shell
RU2244246C2 (en) Armor-piercing bullet
US20220026187A1 (en) Sub-caliber projectile and method of neutralizing a target using such a projectile
RU2400697C2 (en) 'tveritch-3' high-explosive projectile for short-range artillery piece
RU2363919C1 (en) "toropetz" splinter-in-beam projectile
RU2346231C2 (en) "tverskoy" fragmenting-bundle shell
RU2079099C1 (en) Projectile with arrow-like destruction components

Legal Events

Date Code Title Description
AS Assignment

Owner name: RHEINMETALL W & M GMBH, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:THIESEN, STEFAN;JUNGBLUTH, DIETER;SIGNING DATES FROM 20030923 TO 20031007;REEL/FRAME:014628/0197

Owner name: RHEINMETALL W & M GMBH, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:THIESEN, STEFAN;JUNGBLUTH, DIETER;REEL/FRAME:014628/0197;SIGNING DATES FROM 20030923 TO 20031007

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION