EP0069899A1 - Méthode, conteneur, moyens et munition pour bombarder en tapis une zone de but - Google Patents

Méthode, conteneur, moyens et munition pour bombarder en tapis une zone de but Download PDF

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Publication number
EP0069899A1
EP0069899A1 EP82105672A EP82105672A EP0069899A1 EP 0069899 A1 EP0069899 A1 EP 0069899A1 EP 82105672 A EP82105672 A EP 82105672A EP 82105672 A EP82105672 A EP 82105672A EP 0069899 A1 EP0069899 A1 EP 0069899A1
Authority
EP
European Patent Office
Prior art keywords
active body
container
body unit
active
unit 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
EP82105672A
Other languages
German (de)
English (en)
Other versions
EP0069899B1 (fr
Inventor
Rudolf Dipl.-Ing. Romer
Manfred Dipl.-Ing. Moll
Karl Wilhelm Dipl.-Ing. Bethmann
Christian Dipl.-Ing. Dr. Jaeneke
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 EP0069899A1 publication Critical patent/EP0069899A1/fr
Application granted granted Critical
Publication of EP0069899B1 publication Critical patent/EP0069899B1/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

Definitions

  • the invention relates to a method according to the preamble of claim 1 and a device and means for carrying it out.
  • a method of the type mentioned at the outset is known, in which active bodies with impact detonators are ejected from a carrier-fixed container. Each active body has an individual trajectory and must hit an individual target, in particular armored, located on the target surface in order to be effective as desired. A broad-based effect cannot be achieved with a single approach. When the active bodies are ejected during low-level flight, there is also the risk that an active body hits the single target at a very small angle and the effectiveness of a shaped charge incorporated in the active body is thereby considerably impaired.
  • the invention has for its object to provide a method of the type mentioned, in which, in addition to sufficient area coverage, a sufficient effect of the individual active body is ensured from low-altitude flight.
  • a container is shown as a sliding missile C.1 with wings 24 and an elevator 26.
  • a search head (not shown) can be arranged in the bow region 12.
  • conventional fastening means (not shown) are provided for the notchable connection to a carrier aircraft (not shown).
  • discharge openings 34 are indicated in rows 33 one above the other, which extend from the bow area 1 "to the neck area 14. which both act in flight direction 64.
  • FIG. 2 is a cruise missile C.2; 4 trained container, which does not provide clarity, parts with receptacles 32 arranged along straight lines 36 in the interior 28 for active body units w.1, ... shown schematically.
  • the receptacles 32 are arranged one above the other in eight decks 3p, the receptacles 32 of immediately adjacent decks 30 crossing each other.
  • the straight lines 36 form an acute angle 46 with the longitudinal axis 42 of the container, the vertices 44 of the angles 46 lying in the flight direction 64 in front of the relevant outlet openings 34.
  • the marching engine 58 indicated in the rear region 14 is assigned an acceleration propulsion unit 60, which is also only indicated.
  • the search head 56 indicated in the bow area 12 will be discussed later.
  • FIG. 4 shows only two receptacles 30 arranged in adjacent decks 30 and crossing one another with active body units w housed in them.
  • FIG. 5 it can be seen that in the bottom region 22 of the container C there is arranged a longitudinal receptacle 54 with active body units w which runs essentially parallel to the longitudinal axis 42 of the container.
  • active body units w which have been brought out of the container C are indicated in FIG. This will be discussed in more detail.
  • FIG. 6 shows a detail of a receptacle 32 with an active body unit W, 1 which is moved in the dispensing direction 52 and which is shown in side elevation in FIG. 8.
  • the receptacle 32 is provided with a toothed rack 48.1 for interacting with a stub shaft 106 'having a ring gear 106' of a rotor 97 equipped with profiled blades 42 which can be freely rotated relative to the active body 72 about a common axis of rotation 78.
  • the rotor 17 rotates clockwise, while the active body 72 slides along the guide 37.
  • FIG. 7 shows a section 32 of a different shape with a further active body unit W, 2.
  • the active body unit w.2 is provided in the outer region 70 with a toothed ring 104 which corresponds in a form-fitting manner to a toothed rack 48.1 arranged on the side.
  • the active body unit w.2 moves in rotation clockwise around its central axis 78 in the dispensing direction 52 towards a dispensing opening, not shown.
  • Figure 9 illustrates in side elevational view of the shape of the active body unit w.2 7 of FIG Both in Figure 6 and also Figure 7, the racks 48.1 48.3 extend along the respective straight lines 36 which also the respective A usbringraum is rectified 52nd
  • FIG. 10 shows a cutout of the right outer side wall 18 of a further container C.
  • the receptacles 32 are designed in the form of tubes having a hexagonal cross section and extend up to a central longitudinal partition wall 40 good torsional stiffness.
  • FIG. 11 shows a detail of a first magazine M.1 for active body units W, which are separated from one another by spacers 120, so as not to interfere with one another during the clockwise rotation.
  • the rotation is achieved by the rack 48.3 arranged on the upper side.
  • the spacers 120 are divided along a butt joint 122.
  • three compression springs 124 are provided, which ensure that the two halves of the spacers 110 separate in the direction of arrows 126 128 when they pass the relevant discharge opening and in this way do not hinder the active body units w.
  • FIG. 13 shows in a receptacle 32 with a side rack 48, 1, three active body units W.2, W, 3, two of which are identical to one another on the outside, while the middle one differs by a different circumferential region 70.
  • an area XIV outlined in dash-dotted lines in FIG. 13 is shown enlarged in FIG. 14.
  • the two outer active body units w.2 have a toothed ring 104 in the peripheral region 70 both for meshing with the toothed rack 48.1 and with a recessed toothed ring 104 'between two circumferential sliding surfaces 107 of the middle active body unit W.3. This results in a different direction of rotation 111 113 of the active body units W.3, W.3 when the arrangement is moved in the dispensing direction 52.
  • FIG. 14a shows two receptacles 32 which extend between the two lateral outer walls 16, 18 of the container C in question.
  • the arrangement of the active body units W.2, W.3 corresponds to that in FIGS. 13 and 14, a magazine M .2 being only indicated.
  • Dispensing aids in the form of rocket propellants 53 are arranged in the vicinity of an opening 38 in the side wall 18.
  • a toothed belt 48.2 is provided as the positive-locking element which extends along the straight line 36 and is fastened with its one end L.1 in the region of the side wall 18.
  • the free end L. 2 of the toothed belt 48.2 wraps around the circumference 70 of the active body unit W.2 arranged on the left most near the dispensing opening 34.
  • the free end L.2 of the toothed belt 48.2 is first stretched, so that the relevant external active body unit W.2 .mu.m is also sufficiently rotated.
  • a circular cylindrical wall 80 encloses a charge 82 which is delimited on the underside by a P-charge insert 84, so that the actual active body is formed from the arrangement of the wall 80 and the insert 84 72 results.
  • At least one sensor and an igniter 90 to be actuated by it are cast in a conventional manner in a circular ring 85 of essentially triangular cross section and are connected in a manner not shown to the charge 82 in order to be effective.
  • An axis of action 83 of the P charge falls in the axis of rotation 78; the effective direction of the sensor 86 (or the sensors) essentially coincides with that of the P charge of the active body 70.
  • FIGS. 17 and 18 show a sixth exemplary embodiment of an active body unit W.6 with rocket propulsion units 99 arranged opposite one another in the circumferential ring 85 on a diameter 91 to ensure sufficient rotation about the axis of rotation 78 coinciding with the active axis.
  • the rocket propellants are on Ignited manner not described until it passes the discharge opening in question.
  • Figures 22 and 23 show a ninth embodiment of an active body device W.9 in an asymmetrical design.
  • a sheet V.3 which tapers from the active body wall 80 to a free end 100 and is essentially rectangular in plan, the dimension of which transversely to the longitudinal direction corresponds to the diameter 81 of the active body 72.
  • the positive locking elements in the area of the receptacle are unnecessary; they are arranged essentially in a scaly manner one above the other and next to one another in a relevant dispensing tube in such a way that, with the free end 100 of sheet V.3 ahead, they leave the relevant dispensing opening.
  • the initial trajectory is essentially dependent on the application force, a magazine (not shown) being moved against the application opening in question by an application aid designed as a rocket propellant.
  • an application aid designed as a rocket propellant.
  • Figure 24 left half shows in a simplified representation the principle of operation of the invention in a clear manner. While each ejected active body unit W is assigned a corresponding active corridor 132, of which only one is shown, so that this results in a largely complete area coverage over the target area 130, the representation on the right half, which relates to a known method, allows the the difference in effect becomes apparent.
  • the inertial forces are used which, with positive or negative acceleration due to the respective receptacle arranged at an acute angle to the longitudinal axis of the container, act on the respective active body unit and as a result of that in the direction of the respective one Straight 36 outward movement component ensures the respective application process.
  • the container is used in a carrier-proof manner, it is deployed at right angles to the longitudinal axis of the projectile or at an acute angle to the rear, so that the carrier aircraft is not endangered by its own cluster munitions.
  • the elevator 26 is actuated at the same time in such a way that the container rears up on the bow side and the active bodies are shown on Leave the discharge openings as a result of their gravity and with appropriate rotation.
  • a search head 56 is integrated in the container, then a computer and other known devices can be used to ensure that the application process is carried out either cover-wise or pipe-wise, which advantageously results in an ammunition-saving manner of combating individual targets on a target area in question.
EP82105672A 1981-07-14 1982-06-26 Méthode, conteneur, moyens et munition pour bombarder en tapis une zone de but Expired EP0069899B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19813127674 DE3127674A1 (de) 1981-07-14 1981-07-14 Verfahren und vorrichtung zum belegen einer zielflaeche mit munition
DE3127674 1981-07-14

Publications (2)

Publication Number Publication Date
EP0069899A1 true EP0069899A1 (fr) 1983-01-19
EP0069899B1 EP0069899B1 (fr) 1986-04-09

Family

ID=6136817

Family Applications (1)

Application Number Title Priority Date Filing Date
EP82105672A Expired EP0069899B1 (fr) 1981-07-14 1982-06-26 Méthode, conteneur, moyens et munition pour bombarder en tapis une zone de but

Country Status (3)

Country Link
US (2) US4555971A (fr)
EP (1) EP0069899B1 (fr)
DE (2) DE3127674A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2558585A1 (fr) * 1984-01-19 1985-07-26 Stauff Emile Sous-munitions largables pour projectile, notamment antichar
EP0176045A1 (fr) * 1984-09-22 1986-04-02 Rheinmetall GmbH Charge militaire explosive
FR2654822A1 (fr) * 1987-03-17 1991-05-24 Thomson Brandt Armements Dispenseur de sous-projectiles.

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3438305A1 (de) * 1984-10-19 1986-04-24 Diehl GmbH & Co, 8500 Nürnberg Unbemanntes fluggeraet fuer die bekaempfung von bodenzielen
US4967667A (en) * 1985-03-14 1990-11-06 Dese Research And Engineering, Inc. Method and system for preventing salvage fusing of nuclear attack weapons
US4750423A (en) * 1986-01-31 1988-06-14 Loral Corporation Method and system for dispensing sub-units to achieve a selected target impact pattern
US4750403A (en) * 1986-01-31 1988-06-14 Loral Corporation Spin dispensing method and apparatus
US4676167A (en) * 1986-01-31 1987-06-30 Goodyear Aerospace Corporation Spin dispensing method and apparatus
DE3739370A1 (de) * 1987-11-20 1989-06-01 Diehl Gmbh & Co Bomblet-gefechtskopf
DE3843164C1 (fr) * 1988-12-22 1990-05-10 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
DE3911654C2 (de) * 1989-04-10 1994-05-11 Deutsche Aerospace Verfahren zum gleichmäßigen Verteilen von Submunitionskörpern
DE4000902A1 (de) * 1990-01-15 1991-07-18 Diehl Gmbh & Co Sperrwaffe mit verschiessbaren wirkkoerpern
DE4014292C2 (de) * 1990-05-04 1993-12-16 Deutsche Aerospace Dispenser zum Transport und Ausstoß von Streumunition
SE508475C2 (sv) * 1993-03-30 1998-10-12 Bofors Ab Sätt och anordning för spridning av stridsdelar
US6003809A (en) * 1997-02-25 1999-12-21 Honigsbaum; Richard F. Process and apparatus for discouraging countermeasures against a weapon transport device
US6869604B1 (en) * 1998-03-27 2005-03-22 The United States Of America As Represented By The Secretary Of The Department Of Health And Human Services Recombinant anti-tumor RNAse
AUPQ776300A0 (en) * 2000-05-25 2000-08-10 Metal Storm Limited Missile control
JP3902169B2 (ja) * 2003-09-08 2007-04-04 日東電工株式会社 配線回路基板の製造方法および製造装置
PL1711528T3 (pl) 2003-12-23 2012-11-30 Genentech Inc Leczenie nowotworu nowymi przeciwciałami monoklonalnymi anty-IL13
US7185848B2 (en) * 2004-06-21 2007-03-06 Ltas Holdings, Llc Mass transfer system for stabilizing an airship and other vehicles subject to pitch and roll moments
KR101247908B1 (ko) * 2004-09-02 2013-03-26 제넨테크, 인크. 항-ｆｃ-감마 ｒｉｉｂ 수용체 항체 및 그의 용도
US7494089B2 (en) * 2005-11-23 2009-02-24 Raytheon Company Multiple kill vehicle (MKV) interceptor and method for intercepting exo and endo-atmospheric targets
US20090173250A1 (en) * 2007-03-29 2009-07-09 Mechanical Solutions Inc. System for protection against missiles
US7762196B1 (en) * 2007-04-12 2010-07-27 Lockheed Martin Corporation Munition containing sub-munitions that disperse in a circular delta grid impact pattern and method therefor

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3093072A (en) * 1957-01-30 1963-06-11 George L Pigman Spin-induced dispersal bomb
US4172407A (en) * 1978-08-25 1979-10-30 General Dynamics Corporation Submunition dispenser system
US4178851A (en) * 1972-03-08 1979-12-18 The United States Of America As Represented By The Secretary Of The Army Dual purpose munition
DE2934620B1 (de) * 1979-08-28 1981-01-08 Messerschmitt Boelkow Blohm Verfahren zum Belegen einer Flaeche mit Streumunition
GB1588114A (en) * 1969-11-19 1981-04-15 Messerschmitt Boelkow Blohm Airborne projectile container

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3818833A (en) * 1972-08-18 1974-06-25 Fmc Corp Independent multiple head forward firing system
US4264045A (en) * 1979-09-04 1981-04-28 Avco Corporation Despinning method and apparatus
US4318328A (en) * 1979-10-09 1982-03-09 The Boeing Company Removable external payload carrier for aircraft
US4356770A (en) * 1979-11-09 1982-11-02 Avco Corporation Overflying munitions device and system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3093072A (en) * 1957-01-30 1963-06-11 George L Pigman Spin-induced dispersal bomb
GB1588114A (en) * 1969-11-19 1981-04-15 Messerschmitt Boelkow Blohm Airborne projectile container
US4178851A (en) * 1972-03-08 1979-12-18 The United States Of America As Represented By The Secretary Of The Army Dual purpose munition
US4172407A (en) * 1978-08-25 1979-10-30 General Dynamics Corporation Submunition dispenser system
DE2934620B1 (de) * 1979-08-28 1981-01-08 Messerschmitt Boelkow Blohm Verfahren zum Belegen einer Flaeche mit Streumunition

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2558585A1 (fr) * 1984-01-19 1985-07-26 Stauff Emile Sous-munitions largables pour projectile, notamment antichar
EP0176045A1 (fr) * 1984-09-22 1986-04-02 Rheinmetall GmbH Charge militaire explosive
FR2654822A1 (fr) * 1987-03-17 1991-05-24 Thomson Brandt Armements Dispenseur de sous-projectiles.

Also Published As

Publication number Publication date
US4616567A (en) 1986-10-14
US4555971A (en) 1985-12-03
DE3270386D1 (en) 1986-05-15
EP0069899B1 (fr) 1986-04-09
DE3127674A1 (de) 1983-02-24

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