EP0249678A2 - Munition pour combattre des cibles à blindage actif - Google Patents

Munition pour combattre des cibles à blindage actif Download PDF

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Publication number
EP0249678A2
EP0249678A2 EP87102607A EP87102607A EP0249678A2 EP 0249678 A2 EP0249678 A2 EP 0249678A2 EP 87102607 A EP87102607 A EP 87102607A EP 87102607 A EP87102607 A EP 87102607A EP 0249678 A2 EP0249678 A2 EP 0249678A2
Authority
EP
European Patent Office
Prior art keywords
charge
active body
target
active
body according
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.)
Granted
Application number
EP87102607A
Other languages
German (de)
English (en)
Other versions
EP0249678A3 (en
EP0249678B2 (fr
EP0249678B1 (fr
Inventor
Jörg Dr. Peters
Benjamin Furch
Jürg Pfaehler
Jürgen Dr. Böcker
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 Industrie AG
Original Assignee
Rheinmetall 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=6302869&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP0249678(A2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Rheinmetall GmbH filed Critical Rheinmetall GmbH
Priority to AT87102607T priority Critical patent/ATE55831T1/de
Publication of EP0249678A2 publication Critical patent/EP0249678A2/fr
Publication of EP0249678A3 publication Critical patent/EP0249678A3/de
Application granted granted Critical
Publication of EP0249678B1 publication Critical patent/EP0249678B1/fr
Publication of EP0249678B2 publication Critical patent/EP0249678B2/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
    • F42B1/02—Shaped or hollow charges
    • F42B1/032—Shaped or hollow charges characterised by the material of the liner
    • 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
    • F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
    • F42B12/16—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge in combination with an additional projectile or charge, acting successively on the target
    • F42B12/18—Hollow charges in tandem arrangement

Definitions

  • the invention relates to an active body according to the preamble of patent claim 1.
  • a generic object is known from DE-OS 34 16 787.
  • the two landings are essentially of the same diameter, and each of them is arranged in a respective housing with stabilizing wings and forms an independent projectile after the initiation of a separate separating charge.
  • an active body 10 has a casing 11 with a charge 12 that is rotationally symmetrical with respect to the longitudinal axis A.
  • a connection means 13 serves as a receptacle for devices 22 for the power supply for control electronics 24.
  • a tube 15 defines an A coaxial channel 16 for a shaped charge beam to be formed from an insert 14 after the charge 12 has been initiated.
  • the tube 15 serves as a receptacle with a front region of the channel 16 of a charge 18 with a casing 19 and a flat projectile-forming insert 20.
  • the active body 10 is particularly advantageously suitable for combating, in particular actively, armored targets.
  • a proximity fuse not shown and known per se, specifies a predeterminable distance a signal to the control electronics 24 from a target.
  • a first control signal for initiating the front load 18 is formed from the signal, and a projectile from the flat insert 20 leads the active body 10 ahead of the target.
  • a known interference device is brought into effect there by the impact of the projectile and is thus rendered harmless for a shaped charge jet which is formed from the insert 14 of the rear charge 12 initiated by a second control signal.
  • the target-side "interference suppression effect" is achieved with space-saving means, with the lowest possible dead load component and without a separation charge which increases and complicates the susceptibility of the active body and complicates it, which is known from the publication cited at the beginning.
  • the flat insert 20 of the front load 18 is preferably made of a material with an average density between about 16 and about 19 g / cm3.
  • a target-side interfering device is made harmless with a high probability, so that the shaped charge jet from the insert 14 can become fully effective.
  • a cheapest stand-off can be observed. Because of the comparatively small size of the insert 20, the price for the insert material does not need to play such an important role, so that, for example, the use of tantalum does not hinder the cost.
  • FIGS. 2, 3 and 4 of the drawing it can be seen in connection with the above description how versatile the active body 10 according to the invention is.
  • the active body 10 is inserted into a warhead 40, which can be ejected from a cargo floor as a steerable submunition unit.
  • a warhead 40 which can be ejected from a cargo floor as a steerable submunition unit.
  • the connection means 13 ⁇ extends to a known seeker 52 and serves electronics 44 and a control block 46 with gas generators 48 and control nozzles 50 as a receptacle, the aforementioned devices behind the seeker 52 around the pipe 15 with the channel 16 to save space group.
  • Stabilizing wings 42 can be pivoted in a known manner from a space-saving transport position into the operative position shown.
  • the direction of flight of the warhead 40 with the active body 10 is indicated by an arrow F.
  • the active body 10 slightly modified, (reference is made, inter alia, to the shape of the insert 64) of an anti-tank mine 60. It has a launch tube 62 on a tripod mount 74.
  • the central longitudinal axis (not shown) of a known target device 66 with the required control electronics runs parallel to the longitudinal axis A.
  • a rocket engine 70 can be initiated via an ignition device 68.
  • the launch tube 62 is set up by means of the mount 74 so that its longitudinal axis is directed towards an area in which armored targets to be combated are expected. If the target device 66 has identified such a target, the ignition device 68 is initiated via a signal and the rocket motor 70 is ignited by it.
  • the active body 10 leaves the tube 62 after blasting away its cover 76 in the direction of an arrow F, and stabilizing wing 72 fold out of their rest position shown in the drawing into their operative position. Because of the sequence of functions, reference is made to the description in conjunction with FIG. 1.
  • FIG. 4 shows an anti-tank projectile 80 of a known ammunition for a cannon.
  • the tube 15 is designed as a standoff tube 82 and carries on the front side a known approach nozzle 86, which is therefore not shown or described in detail.
  • a known stabilizing stabilizer 90 is arranged on a tail boom 88.

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)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Valve Device For Special Equipments (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Chemical And Physical Treatments For Wood And The Like (AREA)
  • Fire-Extinguishing Compositions (AREA)
  • Agricultural Chemicals And Associated Chemicals (AREA)
EP87102607A 1986-06-18 1987-02-24 Munition pour combattre des cibles à blindage actif Expired - Lifetime EP0249678B2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT87102607T ATE55831T1 (de) 1986-06-18 1987-02-24 Wirkkoerper zum bekaempfen, insbesondere aktiv gepanzerter ziele.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19863619791 DE3619791A1 (de) 1986-06-18 1986-06-18 Wirkkoerper zum bekaempfen, insbesondere aktiv, gepanzerter ziele
DE3619791 1986-06-18

Publications (4)

Publication Number Publication Date
EP0249678A2 true EP0249678A2 (fr) 1987-12-23
EP0249678A3 EP0249678A3 (en) 1988-02-17
EP0249678B1 EP0249678B1 (fr) 1990-08-22
EP0249678B2 EP0249678B2 (fr) 1993-08-18

Family

ID=6302869

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87102607A Expired - Lifetime EP0249678B2 (fr) 1986-06-18 1987-02-24 Munition pour combattre des cibles à blindage actif

Country Status (9)

Country Link
EP (1) EP0249678B2 (fr)
JP (1) JPS62299700A (fr)
AT (1) ATE55831T1 (fr)
CA (1) CA1303905C (fr)
DE (2) DE3619791A1 (fr)
ES (1) ES2016939B3 (fr)
IL (1) IL82794A0 (fr)
NO (1) NO871542L (fr)
ZA (1) ZA874366B (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0452541A2 (fr) * 1990-04-14 1991-10-23 W.C. Heraeus GmbH Procédé de fabrication d'objets creux en tantale
US5780766A (en) * 1996-04-30 1998-07-14 Diehl Gmbh & Co. Guided missile deployable as mortar projectile
DE4117871C1 (de) * 1991-05-31 1999-08-19 Diehl Stiftung & Co Gefechtkopf gegen eine reaktive Zielpanzerung
RU193124U1 (ru) * 2019-07-12 2019-10-15 Федеральное государственное бюджетное военное образовательное учреждение высшего образования "Черноморское высшее военно-морское ордена Красной Звезды училище имени П.С. Нахимова" Министерства обороны Российской Федерации Универсальная кумулятивная мина
EP3882563A1 (fr) * 2020-03-17 2021-09-22 Diehl Defence GmbH & Co. KG Projectile, agencement de moyen d'action et procédé
DE102020113411A1 (de) 2020-05-18 2021-11-18 Rheinmetall Waffe Munition Gmbh Vorrichtung eines wehrtechnischen Effektors

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3924087C1 (de) * 1989-07-20 1997-05-28 Rheinmetall Ind Ag Tandem-Gefechtskopf zur Bekämpfung aktiver Ziele
DE3926711C2 (de) * 1989-08-12 1995-12-07 Rheinmetall Ind Gmbh Geschoß mit Innenraum
DE3934850C1 (de) * 1989-10-19 2000-09-28 Daimlerchrysler Aerospace Ag Gefechtskopf

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR999974A (fr) * 1946-02-11 1952-02-06 Soc Tech De Rech Ind Perfectionnements aux engins à charges creuses
FR2310547A1 (fr) * 1975-05-06 1976-12-03 Realisa Et Applic Tech Et Perfectionnements aux charges creuses
DE2829002A1 (de) * 1978-07-01 1984-03-29 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Multi-gefechtskopf
EP0160118A2 (fr) * 1983-10-07 1985-11-06 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Revêtement pour charge creuse ou plate
EP0201433A1 (fr) * 1985-05-10 1986-12-17 ETAT-FRANCAIS représenté par le DELEGUE GENERAL POUR L'ARMEMENT (DPAG) Projectile Antichar

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE449528B (sv) * 1983-05-13 1987-05-04 Bofors Ab Pansarbrytande projektil
DE3601051C1 (en) * 1986-01-16 1987-06-11 Messerschmitt Boelkow Blohm Warhead

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR999974A (fr) * 1946-02-11 1952-02-06 Soc Tech De Rech Ind Perfectionnements aux engins à charges creuses
FR2310547A1 (fr) * 1975-05-06 1976-12-03 Realisa Et Applic Tech Et Perfectionnements aux charges creuses
DE2829002A1 (de) * 1978-07-01 1984-03-29 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Multi-gefechtskopf
EP0160118A2 (fr) * 1983-10-07 1985-11-06 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Revêtement pour charge creuse ou plate
EP0201433A1 (fr) * 1985-05-10 1986-12-17 ETAT-FRANCAIS représenté par le DELEGUE GENERAL POUR L'ARMEMENT (DPAG) Projectile Antichar

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0452541A2 (fr) * 1990-04-14 1991-10-23 W.C. Heraeus GmbH Procédé de fabrication d'objets creux en tantale
EP0452541A3 (en) * 1990-04-14 1992-01-02 W.C. Heraeus Gmbh Method of manufacturing hollow objects from tantalum
DE4117871C1 (de) * 1991-05-31 1999-08-19 Diehl Stiftung & Co Gefechtkopf gegen eine reaktive Zielpanzerung
US5780766A (en) * 1996-04-30 1998-07-14 Diehl Gmbh & Co. Guided missile deployable as mortar projectile
DE19617221C2 (de) * 1996-04-30 1999-07-01 Diehl Stiftung & Co Als Mörsergeschoß verbringbares Lenkprojektil
RU193124U1 (ru) * 2019-07-12 2019-10-15 Федеральное государственное бюджетное военное образовательное учреждение высшего образования "Черноморское высшее военно-морское ордена Красной Звезды училище имени П.С. Нахимова" Министерства обороны Российской Федерации Универсальная кумулятивная мина
EP3882563A1 (fr) * 2020-03-17 2021-09-22 Diehl Defence GmbH & Co. KG Projectile, agencement de moyen d'action et procédé
DE102020113411A1 (de) 2020-05-18 2021-11-18 Rheinmetall Waffe Munition Gmbh Vorrichtung eines wehrtechnischen Effektors
EP3913318A1 (fr) 2020-05-18 2021-11-24 Rheinmetall Waffe Munition GmbH Dispositif d'un effecteur de la technique militaire

Also Published As

Publication number Publication date
DE3619791A1 (de) 1988-01-14
EP0249678A3 (en) 1988-02-17
EP0249678B2 (fr) 1993-08-18
IL82794A0 (en) 1987-12-20
ZA874366B (en) 1987-12-18
NO871542D0 (no) 1987-04-13
ES2016939B3 (es) 1990-12-16
JPS62299700A (ja) 1987-12-26
EP0249678B1 (fr) 1990-08-22
ATE55831T1 (de) 1990-09-15
CA1303905C (fr) 1992-06-23
DE3764406D1 (de) 1990-09-27
NO871542L (no) 1987-12-21
DE3619791C2 (fr) 1988-04-14

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