EP0423424B1 - Projectile-porteur de bomblets légers d'entrainement rangés par couches - Google Patents

Projectile-porteur de bomblets légers d'entrainement rangés par couches Download PDF

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Publication number
EP0423424B1
EP0423424B1 EP90109953A EP90109953A EP0423424B1 EP 0423424 B1 EP0423424 B1 EP 0423424B1 EP 90109953 A EP90109953 A EP 90109953A EP 90109953 A EP90109953 A EP 90109953A EP 0423424 B1 EP0423424 B1 EP 0423424B1
Authority
EP
European Patent Office
Prior art keywords
bomblet
housing
projectile
practice
bomblets
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.)
Expired - Lifetime
Application number
EP90109953A
Other languages
German (de)
English (en)
Other versions
EP0423424A3 (en
EP0423424A2 (fr
Inventor
Ernst-Wilhelm Altenau
Siegmar Fischer
Margret Palten
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 Industrie AG
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 Industrie AG filed Critical Rheinmetall Industrie AG
Publication of EP0423424A2 publication Critical patent/EP0423424A2/fr
Publication of EP0423424A3 publication Critical patent/EP0423424A3/de
Application granted granted Critical
Publication of EP0423424B1 publication Critical patent/EP0423424B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B8/00Practice or training ammunition
    • F42B8/12Projectiles or missiles
    • F42B8/22Fall bombs
    • 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

Definitions

  • the invention relates to a bomblet carrier projectile with practice bomblets arranged in the projectile shell according to the features specified in the preamble of claim 1.
  • the object of the invention is to design the bomblet carrier projectile and exercise bomblets to be transported therefrom in such a way that the exercise bomblet on the one hand withstands the high acceleration forces occurring during transport to the target area and on the other hand does not sink into it when it hits a resilient surface.
  • a very light exercise bomblet is created, whereby the total weight of the exercise bomblet is reduced in such a way that deep penetration into a flexible surface is avoided and the signature with detonation cloud, flash of light and bang is good is noticeable.
  • This paper-based and / or plastic-made practice bomblet housing also offers particularly advantageous absolute security against splintering, because compared to a practice bomblet housing made of, for example, die-cast, there can be no danger of splinters flying away.
  • a paper-based practice bomblet housing there is advantageously no residue left in the event of a misfire compared to a metal housing, because the practice bomblet housing rots early on, for example due to moisture.
  • bom-bomblet housing made on paper and / or plastic is subject to narrower limits than a metal case in terms of load capacity, for example in terms of compressive strength, support of the bom-bomblets according to the invention within the bomblet carrier floor allows the bom-bomblets to withstand the high initial accelerations Withstand transport to the target area and can be ejected over the target area in a manner known per se via an ejection charge from the rear of the carrier floor.
  • a layer-by-layer support of the practice bomblets within the carrier storey has proven to be an advantageous solution, as a result of which the practice bomblets located in one plane or position are supported in the projectile-axial direction.
  • the support elements consist of disc-shaped support plates arranged transversely to the projectile axis and of axial supports, as a result of which the exercise bomblets can be inserted and supported in layers in the bomblet carrier floor.
  • the arrangement of the exercise bomblets in one layer is not fixed in the circumferential direction and can therefore vary from layer to layer. This results in a simplified installation method.
  • the axial supports between the support plates ensure reliable maintenance of a support spacing in bomblet length, so that the individual practice bomblets do not have to absorb additional axial forces from practice bomblets of pre-stacked layers.
  • the axial forces resulting from this layer-by-layer stacking of bom bomblets arranged one above the other cannot therefore have a negative effect on the stability of the bomblet housing according to the invention, the load due to the initial acceleration being reduced further advantageously due to the reduced bomblet housing weight.
  • the axial supports can be arranged adjacent to the projectile shell in the carrier storey, whereby they can fill the free spaces of the exercise bomblets as fillers to save space or can be arranged between two adjacent support plates as a one-piece or multi-piece central support in the interior free space formed by the exercise bomblets.
  • This central support contains an axial gas passage channel for the ignition of all practice bomblets arranged in the carrier floor.
  • each support plate contains connecting grooves on the top side from the central gas pressure channel to the individual exercise bomblets, as a result of which these can be ignited from below without additional means.
  • the different axial supports also allow the installation of differently designed exercise bomblets.
  • the arrangement of external axial supports allows the installation of additional practice bomblets with lateral ignition, for example via lateral bomblet housing bores or an ignition cord located on the periphery of the bomblet housing. Due to the low axial bomblet load, inexpensive and easy to manufacture housing configurations are possible, which can consist, for example, of a simple cardboard tube with glued-in cardboard or plastic disks or a one-piece housing pot formed from cardboard.
  • FIG. 1 illustrates a bomblet carrier projectile 10, the housing 12 of which has a cylindrical area for receiving exercise bomblets 14, 16, 18, 20, 21 shown in more detail in FIGS. 2 to 11 and a front ogival projectile area 22 for receiving an igniter 24, one of a Ejection charge 26 and ejection plate 28 has existing ejection unit.
  • the ejection plate 28 contains a central gas passage duct 30 'through which the ejection charge 26 during the ejection process of the exercise bomblets over a target area in each bomblet 14, 16, 18, 20, 21 located ignition delay set 15, 74, 76 can be ignited.
  • the exercise bomblets 14, 16, 18, 20, 21, shown in more detail in FIGS. 2 to 11 and described in detail, can each be arranged in the bomblet carrier floor 12, each with a housing 32, 34, 36, 38, 40 made on paper and / or plastic .
  • the exercise bomblets 14 received by the bomblet carrier projectile 10 in FIG. 1 are supported in layers within the bomblet carrier projectile 10, for which purpose stackable supporting elements 42, 44, 46 (FIG. 5) are arranged in the carrier projectile envelope 12 in the projectile axial direction.
  • a support element is provided by an exercise bomb 14 located below each in the same flat position and disk-shaped support plate 42 arranged transversely to the projectile axis 11, which are supported to the adjacent support plates 42 by axial supports 44, the axial supports having a height corresponding to the bomblet length in order to form a sufficient support spacing.
  • the axial supports 44 shown in FIG. 1 lie between two adjacent support plates 42 on the projectile shell 12 and are designed as fillers filling the spaces 48 (FIG. 6) between the exercise bomblets 14. These axial supports 44 can also be used in advantageous use of a different weight described in DE 36 29 668 C1 for regulating the center of gravity of the support projectile 10.
  • the support plates 42 can, however, as shown in Figures 5 and 6, are supported by a centrally arranged axial support 46, which can be constructed in one or more pieces and on the inside forms a portion of the central gas passage 30 'and on the outside radially to the respective bomblet circumference of each of the bomblets 14, 20, 21 located in a flat position rests. Due to the above-described outside design of these axial supports 46, the advantage of a holder known from DE 38 08 898 A1 can be used for radial securing of the bomblets and for securing in the circumferential direction.
  • the latter is continued through the interior 30 formed by the bomblet arrangement and opens into a central gas passage duct 30 'in each plane bomblet layer, the disk-shaped support plate 42.
  • This disk-shaped support plate 42 contains, on the side facing the exercise bomb 14, for example, grooves 50, 52 shown in more detail in FIG. 7 for the passage of the Gas pressure and the flame to ignite all practice bomblets arranged on the support plate 42.
  • the gas initially flows from the axial gas passage channel 30 'via radially extending grooves 50 arranged in a star shape and from there via a circular groove 52 to each exercise bomb 14, whereby an ignition delay set 15, 74 arranged on the end face in the exercise bombs 14, 20, 21 76 is ignitable.
  • the exercise bomblets 14 fill a partial volume of the bomblet carrier floor 12 in a reduced number, the remaining partial volume being filled by a hollow cylinder 43 connected to the lowermost support plate 42.
  • the bomblet carrier floor 10 is further provided with a guide band 45 known per se and a floor 47 which can be released when the bomblets are ejected above the target area.
  • the bomblet housings 32, 34, 36, 38, 40 shown in detail in FIGS. 2, 3 and 8 to 11 consist entirely or at least part of the housing of cardboard.
  • This cardboard can have a weight between 50 to 950 g / m2 depending on the intended use as a casing tube 54, 56, 58 or as a cover 62, 64.
  • the casing tube 54, 56, 58 can consist of wrapped paper and have a greater specific weight than the cover 62, 64.
  • the strength of the practice bomblet housing 32, 34, 36, 38, 40 made of cardboard and / or plastic must be so high that the respective exercise bomblet 14, 16, 18, 20, 21 can withstand the launch acceleration of the bomblet carrier projectile 10 .
  • the cardboard or plastic housing material enables a specific weight of less than 1 kg / dm3 to be achieved for the entire practice bomblet unit, so that the practice bomblets are floatable.
  • the bomblet housings 32, 34, 36 shown in FIGS. 2, 3, 8 and 9 contain a cardboard or plastic tube 54, 56, 58 as a jacket and a cardboard or plastic cover 62, 64 on the end face, which has a deuterium charge 60 on both inside the tube Support end faces.
  • the spacing of the covers 62, 64 is advantageously determined by a spacer tube 68, which lies between the covers 62, 64 on the inside 66 of the practice bomblet housing 32, 34, 36, can be made of cardboard or plastic and with the tubular housing shell 54, 56, 58 is connected by an adhesive connection. Likewise, the covers 62, 64 are connected to the housing jacket 54, 56, 58 of the practice bomblets via an adhesive connection.
  • the practice bomb 14 shown in FIG. 2 contains a pyrotechnic detonator with ignition delay set 15, which is fastened to the bottom cover 64 in a manner shown in detail and protrudes into the Deutch 60 and can thus be easily traversed by the gas passage 30 and the grooves 50, 52 Ignite the flame of the ignition charge 26.
  • ignition delay sets 15 are known and ignite the German charge 60 after a predetermined time after the practice bomblets have hit the underground of the target area.
  • Both covers 62, 64 form with the casing tube 54 a closed cylindrical bomblet housing 14.
  • the casing tube 56 protrudes beyond the upper cover 64, the upper cover 64 carrying the ignition delay set 15 projecting down here into the Deutch 60 and the casing pipe 56 having lateral bores 57 for igniting the ignition delay set 15 .
  • a further cover 65 and a further spacer tube 68 can be connected on the inside to the casing tube 56 above the bores 57.
  • the practice bomblet 18 shown in FIG. 8 can be ignited directly by the flame passing through the gas passage duct 30.
  • the tubular jacket 58 of the practice bomblet housing 36 contains on the outside a circumferential groove 70 for receiving an ignition cord 72, from which an ignition delay set 74 protruding radially into the Deutch 60 can be ignited, the ignition delay set 74 being able to rest on the lower cover 62 in a supporting manner.
  • bomblet housing 38, 40 which according to FIGS. 10 and 11 shows cup-shaped design variants.
  • bomblet housings 38, 40 for example made of cardboard, can be produced by the mulch process, the tubular housing casing 59 (FIG. 10) either being comparatively thick-walled for stabilization or the casing 71 (FIG. 11) being reinforced with longitudinal ribs 73.
  • the end 78 of the housing shell 59, 71 which initially protrudes downward in the axial direction, can be flanged in the radial direction in an uncomplicated manner.
  • the material cardboard or plastic ensures further embodiments falling under the scope of protection Practice bomblet housing, which are not shown in the drawing and open up the possibility of arranging the practice bomblets in layers in a cheese corner shape.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Claims (10)

  1. Projectile vecteur de petites bombes ou bombettes avec des bombettes d'exercice (14, 16, 18, 20, 21), placées l'enveloppe (12) du projectile, dont les espaces libres sont remplis de pièces de garnissage (44, 46), empilables axialement, avec un détonateur (24) placé dans la zone avant (22) du projectile et une unité d'éjection constituée d'une charge d'éjection (26) et d 'une plaque d éjection (28), au moyen de laquelle les bombettes d'éjection (14, 16, 18, 20, 21) sont allumées à travers un canal de passage des gaz (30, 30′), s'étendant dans l'axe du projectile et sont éjectées de l'enveloppe du projectile vecteur, sur la zone-cible,
    caractérisé par les caractéristiques suivantes :
    a) chaque bombette d'exercice (14, 15, 18, 20n 21) contient un boîtier (32, 34, 36, 38, 40) réalisé à base de papier et/ou de manière plastique, dont la l'accélération du tir, et en ce que chaque unité de bombette présente un poids specifique inferieur à 1 kg/cm³,
    b) les pièces de garnissage (44, 46) portent comme forme de disque séparé, disposée transversalement à l'axe (11) du projectile, plaque sur laquelle prennent appui en couches les boîtiers (32, 34, 36, 38, 40) des bombettes d'exercice (14, 16, 18, 20, 21), à l'intérieur du projectile vecteur (10).
  2. Projectile vecteur de bombettes selon la revendication 1, caractérisé en ce que la plaque d'appui (42) présente, sur le côté correspondant à la bombette d'exercice (14, 20, 21), des rainures (50n 52) pour le passage de la pression des gaz et de la flamme pour l'allumage de toutes les bombettes placées sur la plaque d'appui (42), des rainures (50) radiales reliant le canal de passage des gaz (30') axial de la plaque d'appui (42) avec une rainure (52) circulaire, menant à chaque bombette d'exercice (14, 20, 21).
  3. Projectile vecteur de bombettes selon la revendication 1, caractérisé en ce que le boîtier (32, 34, 36, 38, 40) de la bombette est entièrement ou au moins en partie en carton.
  4. Projectile vecteur de bombettes selon la revendication 3, caractérisé en ce que le carton prévu comme boîtier de bombette (32, 34, 36, 40) présente un poids compris entre 50 et 950 g/m².
  5. Projectile vecteur de bombettes selon la revendication 1, caractérisé en ce que le boîtier (32, 34, 36, 38, 40) de la bombette est entièrement ou au moins en partie en polyamide.
  6. Projectile vecteur de bombettes selon l'une des revendications 1 à 5, caractérisé en ce que le boîtier (32, 34, 36) de la bombette comprend une enveloppe faite d'un tube de carton ou de matière plastique (54, 56, 58) et un couvercle en carton ou matière plastique (62, 64), qui soutiennent une charge significative (60) à l'intérieur du tube, sur les deux côtés frontaux.
  7. Projectile vecteur de bombettes selon l'une des revendications 1 à 6, caractérisé en ce que sur le côté intérieur (66) du boîtier (32, 34, 36) de la bombette il est prévu, entre les couvercles (62, 64), un tube d'écartement (68) qui est en carton ou en matière plastique.
  8. Projectile vecteur de bombettes selon la revendication 7, caractérisé en ce que le tube d'écartement (68) et les couvercles (62, 64) sont reliés entre eux avec l'enveloppe (54, 56, 58) tubulaire du boîtier, par un assemblage collé.
  9. Projectile vecteur de bombettes selon l'une des revendications 1 à 8, caractérisé en ce que l'enveloppe (58) tubulaire du boîtier (36) de la bombette présente extérieurement une rainure (70) continue destinée à loger un cordon d'allumage (72), à partir duquel un ensemble de temporisation (64) pénètre radialement dans la charge significative (60).
  10. Projectile vecteur de bombettes selon l'une des revendications 1 à 9, caractérisé en ce que le boîtier (38, 40) de la bombette est fait d'un godet en carton ou en matière plastique, qui sur son côté ouvert est replié pour loger un ensemble de temporisation (76) à placer axialement.
EP90109953A 1989-10-14 1990-05-25 Projectile-porteur de bomblets légers d'entrainement rangés par couches Expired - Lifetime EP0423424B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3934362 1989-10-14
DE3934362A DE3934362A1 (de) 1989-10-14 1989-10-14 Bomblet-traegergeschoss mit lagenweise angeordneten leicht-uebungsbomblets

Publications (3)

Publication Number Publication Date
EP0423424A2 EP0423424A2 (fr) 1991-04-24
EP0423424A3 EP0423424A3 (en) 1992-06-17
EP0423424B1 true EP0423424B1 (fr) 1995-06-28

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EP90109953A Expired - Lifetime EP0423424B1 (fr) 1989-10-14 1990-05-25 Projectile-porteur de bomblets légers d'entrainement rangés par couches

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US (1) US5076171A (fr)
EP (1) EP0423424B1 (fr)
DE (2) DE3934362A1 (fr)

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DE10308307B4 (de) * 2003-02-26 2007-01-04 Buck Neue Technologien Gmbh Geschoß sowie Submunition mit Vorspannkörper
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US7261039B1 (en) * 2006-04-07 2007-08-28 The United States Of America As Represented By The Secretary Of The Army Artillery Rocket Kinetic Energy Rod Warhead
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
DE102007057184A1 (de) * 2007-11-26 2009-05-28 Rheinmetall Waffe Munition Gmbh Munition oder Geschoss zur Gefechtsfeldbeleuchtung
US7982653B1 (en) * 2007-12-20 2011-07-19 Raytheon Company Radar disruption device
DE102008019752A1 (de) * 2008-04-18 2009-10-22 Rheinmetall Waffe Munition Gmbh Wirkkörper für eine Submunition mit Wirkmitteln
US8250984B2 (en) * 2008-08-29 2012-08-28 Lockheed Martin Corporation Mine-defeating submunition
US8424456B2 (en) 2009-10-05 2013-04-23 Amtec Corporation Non-dud signature training cartridge and projectile
US9939239B1 (en) * 2013-05-03 2018-04-10 The United States Of America As Represented By The Secretary Of The Army Stackable collaborative engagement munition
US9726466B2 (en) * 2015-02-13 2017-08-08 Dmd Systems, Llc Fuel/air concussion apparatus
US11561075B2 (en) * 2018-12-13 2023-01-24 The United States Of America, As Represented By The Secretary Of The Navy Projectile with pyrotechnically timed release of a secondary payload
CN112537061A (zh) * 2019-09-21 2021-03-23 梁坪 一种利用废纸、废塑料制备子弹壳的方法

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Also Published As

Publication number Publication date
US5076171A (en) 1991-12-31
DE59009327D1 (de) 1995-08-03
EP0423424A3 (en) 1992-06-17
EP0423424A2 (fr) 1991-04-24
DE3934362A1 (de) 1991-04-18

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