EP0069949A1 - Ensemble de projectiles pour une arme à tube de canon - Google Patents

Ensemble de projectiles pour une arme à tube de canon Download PDF

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Publication number
EP0069949A1
EP0069949A1 EP82105953A EP82105953A EP0069949A1 EP 0069949 A1 EP0069949 A1 EP 0069949A1 EP 82105953 A EP82105953 A EP 82105953A EP 82105953 A EP82105953 A EP 82105953A EP 0069949 A1 EP0069949 A1 EP 0069949A1
Authority
EP
European Patent Office
Prior art keywords
floor
wire
flight
elements
arrangement 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
EP82105953A
Other languages
German (de)
English (en)
Other versions
EP0069949B1 (fr
Inventor
Jürgen Dr. Dipl.-Phys. Dr. Böcker
Klaus Gersbach
Karl Wilhelm Dipl.-Ing. Bethmann
Gerhard Dr. Dipl.-Ing. Glotz
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
Application filed by Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of EP0069949A1 publication Critical patent/EP0069949A1/fr
Application granted granted Critical
Publication of EP0069949B1 publication Critical patent/EP0069949B1/fr
Expired 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
    • F42B12/66—Chain-shot, i.e. the submissiles being interconnected by chains or the like
    • 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
    • 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
    • F42B12/625—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other

Definitions

  • the invention relates to a floor arrangement according to the preamble of patent claim 1.
  • Targets exhibiting new types of armor especially those in which an external armor plate is accelerated when a projectile is hit by a respective explosive charge in order to render the projectile in question largely ineffective, require correspondingly complex means of combating them. It is important to first deactivate the acceleration charge and thus make it harmless for further combat in the target area concerned.
  • the invention has for its object to provide a floor arrangement of the type mentioned, which is suitable with a high probability of annihilation for fighting actively armored targets.
  • three missiles 11, 12 and 13 are located one behind the other on a common trajectory T, represented as a straight line for reasons of simplicity, whose (initially imagined) end point 58 is active on a first armored plate 54 between two armored plates 52 and 56 of a simplified and schematically illustrated one armored target 50.
  • the missile 11 flying ahead in the direction S is connected by a wire 45 to the missile 12 following at a distance EI.
  • the missile 12 is connected to the missile 13 following at a distance E2 by means of a wire 46.
  • the distances E1 and E2 are both shortened and shown the same length.
  • the armor plate 54 is accelerated in relation to the adjacent armor plates 52 and 56 in a manner not shown and described in order to disrupt the missile 11 and thereby largely impair its effect.
  • Fig. 2 with 54 * the armored plate designated in Fig. 1 with 54 during acceleration is schematic and the missile 11 is no longer shown.
  • the charge assigned to the armor plate 54 (54 ') is deactivated by the missile 11.
  • the missile 12 following at the distance EI and also directed at the area of the armor plate 54 (54 ') can now operate without disruption, while the missile 13 following the missile 12 on the common trajectory T at the distance E2 further increases the harmful effect in the target area under consideration.
  • Fig. 3 shows the structure of the second storey shown in Fig. 1, the flight floor 12.
  • Its sub-caliber main part (penetrator) 14 is delimited on the front by an essentially flat end face 16 with a circumferential tough bite edge 28 and on the back by an annular rear surface 18.
  • a ballistic hood 20 with a wall 22 and a tip 24 covers the end face 16 and is connected to the penetrator 14 in a manner not shown.
  • an insert 26 which is only indicated and is essentially designed as a thin nozzle tube, is provided in alignment with the longitudinal axis A of the projectile. It serves for the protective passage of the wire 45 for connection to the missile 11 (shown in the first place in FIG. 1).
  • One end 45 'of the wire 45 is fixed in the region of the end face 16 in an elastic tension transducer 30, not shown, which one forms the first wire attachment.
  • a second wire fastening designed as a wire magazine 33 is arranged in the penetrator 14. It is formed by a circular cylindrical recess 34 a front-side boundary surface 36.
  • the rear opening of the recess 34 which is not designated in any more detail, is provided with a circular guide element 38, the rounded inner surface 39 of which delimits a passage opening 40 (shown enlarged).
  • a coil former 42 is fixed in alignment with its first end, not designated in any more detail, in the region of the boundary surface 36 and extends through the recess 34, so that a substantially mushroom-shaped, thickened free end 43 is adjacent to the inside of the guide element 38.
  • the end 43 of the bobbin 42 has a rounded outer surface 44 with an outer diameter that is larger than the diameter of the passage opening 40.
  • the wire 46 is wound on the bobbin 42 and is guided through the passage opening 40 for connection to the subsequent missile 13 (shown in third place in FIG. 1).
  • the following missiles 12 and 13 each have at least two elements 50, for which passages 23 are provided in the wall 22 of the ballistic hood 20.
  • a device 52 is assigned to the elements 50.
  • the latter has rods 56 arranged as a parallelogram in joints 54.
  • the elements 50, the free ends 51 of which project radially beyond the unspecified outer surface of the ballistic hood 20, are fastened to joints 54 which are adjacent to one another.
  • One of the joints 54 lying on the longitudinal axis A of the floor is fixed to the elastic tension sensor of the tip-side wire fastening 30, while the end 45 ′ of the wire 45 is fastened to the other joint 54.
  • a tension spring 56 connects the two joints 54 lying on the longitudinal axis A of the floor. It ensures that the elements 50 assume a predetermined position in the initial state, in which the maximum value predetermined for a 2 (or a 3 ) is achieved. As soon as the sabot segments, which are also not shown, have separated from the missiles 11, 12 and 13 after leaving a weapon barrel (not shown), the latter take up the predetermined distance EI or E2 while the wires 45 and 46 are being unwound from the respective bobbin 42. If this is reached, the wire end 45 ′ shown in FIG.
  • the tension spring 56 exerts a tensile force on the front joint 54, the tension spring 56 is stretched and the two elements 50 move against the longitudinal axis A of the floor while reducing the value a 2 the tensile force transmitted to the wire 45, the tension spring 56 can relax again, the elements move outward again in the opposite direction, so that a value for a 2 (or a 3 ) is established in which the wire 45 (or 46) is sufficiently streamlined.
  • the respective flight floor 11 (or 12) flying ahead is not unduly braked by the subsequent flight floor 12 (or 13).
  • the inventive arrangement also ensures an exact succession in the other context: the flying floor 11 (or 12) is followed by an area in which the air resistance to the surroundings is reduced for the subsequent floor 12 (or 13).

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)
EP82105953A 1981-07-09 1982-07-03 Ensemble de projectiles pour une arme à tube de canon Expired EP0069949B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19813127002 DE3127002A1 (de) 1981-07-09 1981-07-09 Geschossanordnung fuer eine rohrwaffe
DE3127002 1981-07-09

Publications (2)

Publication Number Publication Date
EP0069949A1 true EP0069949A1 (fr) 1983-01-19
EP0069949B1 EP0069949B1 (fr) 1985-04-17

Family

ID=6136433

Family Applications (1)

Application Number Title Priority Date Filing Date
EP82105953A Expired EP0069949B1 (fr) 1981-07-09 1982-07-03 Ensemble de projectiles pour une arme à tube de canon

Country Status (4)

Country Link
US (1) US4524697A (fr)
EP (1) EP0069949B1 (fr)
DE (2) DE3127002A1 (fr)
IL (1) IL66189A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0087502A1 (fr) * 1982-02-27 1983-09-07 Rheinmetall GmbH Munition à projectiles multiples à sabot commun
FR2634879A1 (fr) * 1988-08-01 1990-02-02 Giroud Alexandre Cartouche de transmission ou de recuperation
DE3836187C1 (de) * 1988-10-24 2000-05-11 Deutsch Franz Forsch Inst Verfahren zur Herstellung eines gleichbleibenden kurzen Abstandes zwischen mindestens zwei aufeinanderfolgenden, ballistisch gleichartigen Geschossen und Geschoß zur Durchführung dieses Verfahrens

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4638737A (en) * 1985-06-28 1987-01-27 The United States Of America As Represented By The Secretary Of The Army Multi-warhead, anti-armor missile
DE3609092A1 (de) * 1986-03-19 1990-11-22 Rheinmetall Gmbh Geschoss fuer eine rohrwaffe zum bekaempfen aktiv und passiv reagierender sonderpanzerungen
FR2609542B1 (fr) * 1987-01-14 1994-05-06 Serat Perfectionnements apportes aux projectiles a charges creuses tandem
DE3822998C1 (en) * 1988-07-07 1992-04-09 Rheinmetall Gmbh, 4000 Duesseldorf, De Submunition system with coupling cable - incorporates cable motion damping system with piston and high viscosity hydraulic oil
DE4007677C1 (de) * 1990-03-10 1998-05-14 Diehl Gmbh & Co Vorrichtung zum Bekämpfen von insbes. für Fluggeräte vorgesehenen gepanzerten Unterständen
DE4112915A1 (de) * 1990-06-05 1991-12-12 Serat Gefechtskopf mit tandem-sprengladungen
US5526752A (en) * 1994-09-06 1996-06-18 Rockwell International Corporation Weapon for destruction of deeply buried and hardened targets
AUPR867101A0 (en) * 2001-11-02 2001-11-29 Marine Research Wa Pty Ltd Munitions
US6931994B2 (en) * 2002-08-29 2005-08-23 Raytheon Company Tandem warhead
JP2007508524A (ja) 2003-10-14 2007-04-05 レイセオン・カンパニー 地雷防護システム
US7827900B2 (en) * 2004-10-07 2010-11-09 Innovative Survivability Technologies, Inc. Explosive round countermeasure system
US20090320711A1 (en) 2004-11-29 2009-12-31 Lloyd Richard M Munition
US8082199B2 (en) 2005-04-05 2011-12-20 Ming Yat Kwok Multiple variable outlets shooting apparatus
WO2006116589A2 (fr) * 2005-04-26 2006-11-02 Lockheed Martin Corporation Dispositif d'arrimage compact pour penetrateurs

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2379203A (en) * 1941-06-20 1945-06-26 Vladimiras N Vertzinsky Projectile
US3665861A (en) * 1968-10-17 1972-05-30 Us Army Ammunition

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1321667A (en) * 1919-11-11 Projectile
US1343747A (en) * 1918-10-25 1920-06-15 Radakovich Michael Projectile
US2348240A (en) * 1941-12-11 1944-05-09 Alexander N Braun Cluster bomb
US2368587A (en) * 1942-09-17 1945-01-30 Wise Edward Brooks Antiaircraft shell
US4212244A (en) * 1977-12-09 1980-07-15 Abraham Flatau Small arms ammunition
US4271761A (en) * 1979-04-23 1981-06-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration High acceleration cable deployment system
US4327644A (en) * 1979-05-01 1982-05-04 Stahan Corporation Projectile deployed cable weapons system

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2379203A (en) * 1941-06-20 1945-06-26 Vladimiras N Vertzinsky Projectile
US3665861A (en) * 1968-10-17 1972-05-30 Us Army Ammunition

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0087502A1 (fr) * 1982-02-27 1983-09-07 Rheinmetall GmbH Munition à projectiles multiples à sabot commun
US4516502A (en) * 1982-02-27 1985-05-14 Rheinmetall Gmbh Impact projectile assembly
FR2634879A1 (fr) * 1988-08-01 1990-02-02 Giroud Alexandre Cartouche de transmission ou de recuperation
DE3836187C1 (de) * 1988-10-24 2000-05-11 Deutsch Franz Forsch Inst Verfahren zur Herstellung eines gleichbleibenden kurzen Abstandes zwischen mindestens zwei aufeinanderfolgenden, ballistisch gleichartigen Geschossen und Geschoß zur Durchführung dieses Verfahrens

Also Published As

Publication number Publication date
EP0069949B1 (fr) 1985-04-17
DE3263119D1 (en) 1985-05-23
IL66189A (en) 1987-03-31
US4524697A (en) 1985-06-25
DE3127002A1 (de) 1983-01-20

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