EP0268049A2 - Obus d'artillerie avec sous-munitions - Google Patents

Obus d'artillerie avec sous-munitions Download PDF

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Publication number
EP0268049A2
EP0268049A2 EP87114463A EP87114463A EP0268049A2 EP 0268049 A2 EP0268049 A2 EP 0268049A2 EP 87114463 A EP87114463 A EP 87114463A EP 87114463 A EP87114463 A EP 87114463A EP 0268049 A2 EP0268049 A2 EP 0268049A2
Authority
EP
European Patent Office
Prior art keywords
submunitions
submunition
storage space
artillery
projectile
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
EP87114463A
Other languages
German (de)
English (en)
Other versions
EP0268049B1 (fr
EP0268049A3 (fr
Inventor
Wolfgang von Entress-Fürsteneck
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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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 Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of EP0268049A2 publication Critical patent/EP0268049A2/fr
Publication of EP0268049A3 publication Critical patent/EP0268049A3/fr
Application granted granted Critical
Publication of EP0268049B1 publication Critical patent/EP0268049B1/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
    • 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
    • F42B12/36—Projectiles, 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
    • F42B12/56—Projectiles, 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
    • F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
    • F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile

Definitions

  • the invention relates to an artillery projectile with several identical submunitions, each having a projectile-forming charge and an antenna on one side and a flight stabilization means on the other side.
  • an artillery projectile is loaded with submunitions, such an artillery projectile usually has a different weight and a different center of gravity than a corresponding artillery projectile which is filled with an explosive charge. This must be taken into account when firing.
  • the object of the invention is to propose an artillery projectile of the type mentioned in the introduction, in which the submunitions are designed and housed in such a way that the projectile has the same center of gravity and the same weight as an artillery projectile loaded with a charge.
  • the above-mentioned object is achieved in that at least two submunitions are arranged axially one above the other in the projectile casing, in that a hollow storage space is formed between two adjacent submunitions is, which is divided by a cone-shaped partition lid, that the flight stabilizer of one submunition is stowed in the storage space on the convex side of the partition lid and the antenna of the adjacent submunition is located in the storage space on the concave side of the partition lid.
  • the storage spaces between the at least two submunitions By dimensioning the storage spaces between the at least two submunitions, these can be distributed in the shell so that the center of gravity and the weight of the artillery shell coincide with an artillery shell filled with a load.
  • the moments of inertia of the artillery projectiles also coincide around the longitudinal and transverse axes.
  • a projectile has a head (1), a projectile casing (2) and a projectile floor (3).
  • the shell (2) three submunitions (4,5,6) are axially aligned.
  • Each submunition (4, 5, 6) has a projectile-forming charge (8) and an ignition device (9) in a housing (7).
  • An antenna (10) is arranged on one side of the submunition (4, 5 or 6).
  • a parachute (11) is attached to the opposite side.
  • a hollow storage space (12) is created between the middle submunition (5) and the submunition (4) or the submunition (6). Its height is determined by an insertion sleeve (13). The insertion sleeve (13) keeps the neighboring submunitions at a distance.
  • the storage space (12) is divided by a cone-shaped partition lid (14).
  • the parachute (11) is located in the storage space (12) on the convex side of the separating cover (14).
  • the antenna (10) of the submunition (5 or 6) is located in the storage space (12) on the concave side of the separating cover (14).
  • a recess (15) is provided in the floor (3) to accommodate the parachute (11) of the submunition (6).
  • the antenna (10) of the uppermost submunition (4) runs under a cover plate (16) which is conical in shape in accordance with the shape of the antenna (10).
  • an insulation plate (17), for example made of steel, is inserted into the bottom of the housing (7).
  • the projectile has a weight and a center of gravity which are the same as a conventional artillery projectile of the same dimensions.

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)
  • Details Of Aerials (AREA)
  • Radar Systems Or Details Thereof (AREA)
EP87114463A 1986-10-17 1987-10-03 Obus d'artillerie avec sous-munitions Expired - Lifetime EP0268049B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19863635361 DE3635361A1 (de) 1986-10-17 1986-10-17 Artilleriegeschoss mit submunitionen
DE3635361 1986-10-17

Publications (3)

Publication Number Publication Date
EP0268049A2 true EP0268049A2 (fr) 1988-05-25
EP0268049A3 EP0268049A3 (fr) 1991-07-17
EP0268049B1 EP0268049B1 (fr) 1993-01-20

Family

ID=6311918

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87114463A Expired - Lifetime EP0268049B1 (fr) 1986-10-17 1987-10-03 Obus d'artillerie avec sous-munitions

Country Status (3)

Country Link
US (1) US4807533A (fr)
EP (1) EP0268049B1 (fr)
DE (2) DE3635361A1 (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3926711C2 (de) * 1989-08-12 1995-12-07 Rheinmetall Ind Gmbh Geschoß mit Innenraum
DE3937762C2 (de) * 1989-11-14 1993-11-25 Diehl Gmbh & Co Artilleriegeschoß-Submunition
DE4041612A1 (de) * 1990-12-22 1992-07-02 Rheinmetall Gmbh Deckelentriegelung fuer eine submunition
DE4123649C2 (de) * 1991-07-17 1993-11-11 Rheinmetall Gmbh Ausstoßvorrichtung
FR2684754B1 (fr) * 1991-12-10 1995-04-07 Thomson Brandt Armements Obus dont le culot fait office de pot de parachute d'une sous-munition.
DE4429292C2 (de) * 1994-08-18 1998-04-09 Rheinmetall Ind Ag Drallstabilisiertes Trägergeschoß
FR2741143B1 (fr) * 1995-11-13 1998-01-02 Giat Ind Sa Dispositif de maintien d'un revetement d'une charge generatrice de noyau
AU755006B2 (en) * 1997-12-11 2002-11-28 Lockheed Martin Corporation Shrouded aerial bomb
AU763036B2 (en) * 1997-12-11 2003-07-10 Lockheed Martin Corporation Shrouded aerial bomb
DK1038152T3 (da) * 1997-12-11 2004-12-13 Lockheed Corp Beklædt flyvemaskinebombe
US6227119B1 (en) * 1998-10-30 2001-05-08 Lockheed Martin Corporation Lightweight warhead assembly
DE102007033831A1 (de) * 2007-07-18 2009-01-22 Rheinmetall Waffe Munition Gmbh Submunitionseinheit
DE102007056785A1 (de) * 2007-11-23 2009-05-28 Rheinmetall Waffe Munition Gmbh Geschoss
DE102007056786A1 (de) * 2007-11-23 2009-05-28 Rheinmetall Waffe Munition Gmbh Geschoss
US10030953B2 (en) 2013-08-20 2018-07-24 Bae Systems Plc Illumination munition
WO2015025141A1 (fr) * 2013-08-20 2015-02-26 Bae Systems Plc Sous-munition à chargeur commun
AU2014310467B2 (en) * 2013-08-20 2017-10-12 Bae Systems Plc Frangible munition
JP2016531265A (ja) 2013-08-20 2016-10-06 ビ−エイイ− システムズ パブリック リミテッド カンパニ−ＢＡＥ ＳＹＳＴＥＭＳ ｐｌｃ 煙ペイロード装置
US9234728B2 (en) 2013-11-08 2016-01-12 Lonestar Inventions, L.P. Rocket or artillery launched smart reconnaissance pod
SE540780C2 (sv) 2016-04-06 2018-11-06 Bae Systems Bofors Ab Delningsbar granat med fallskärmsanordning

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3946672A (en) * 1974-08-13 1976-03-30 Thiokol Corporation Rocket propelled projectile
DE2205074A1 (de) * 1972-02-03 1977-03-17 Messerschmitt Boelkow Blohm Sprengkoerper mit hohlladungs- und splitterbelegungen
DE2654827A1 (de) * 1976-12-03 1978-06-08 Rheinmetall Gmbh Mittels eines traegergeschosses verschiessbare hohlladungstochtergeschosse
DE3326876A1 (de) * 1983-07-26 1985-02-07 Diehl GmbH & Co, 8500 Nürnberg Submunitionskoerper mit zieldetektionseinrichtung

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1090007A (en) * 1913-10-01 1914-03-10 Krupp Ag Luminous projectile.
US4050381A (en) * 1972-04-12 1977-09-27 The United States Of America As Represented By The Secretary Of The Army Low density indirect fire munition system (U)
FR2204294A5 (fr) * 1972-10-25 1974-05-17 Cnim
FR2260772B1 (fr) * 1974-02-08 1976-06-25 France Etat
DE2608067C3 (de) * 1976-02-28 1984-07-26 Diehl GmbH & Co, 8500 Nürnberg Zündschaltung für Streumunition

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2205074A1 (de) * 1972-02-03 1977-03-17 Messerschmitt Boelkow Blohm Sprengkoerper mit hohlladungs- und splitterbelegungen
US3946672A (en) * 1974-08-13 1976-03-30 Thiokol Corporation Rocket propelled projectile
DE2654827A1 (de) * 1976-12-03 1978-06-08 Rheinmetall Gmbh Mittels eines traegergeschosses verschiessbare hohlladungstochtergeschosse
DE3326876A1 (de) * 1983-07-26 1985-02-07 Diehl GmbH & Co, 8500 Nürnberg Submunitionskoerper mit zieldetektionseinrichtung

Also Published As

Publication number Publication date
US4807533A (en) 1989-02-28
DE3783724D1 (de) 1993-03-04
EP0268049B1 (fr) 1993-01-20
EP0268049A3 (fr) 1991-07-17
DE3635361A1 (de) 1988-04-21

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