EP0424198B1 - Trägergeschoss mit einem Modulbehälter zum Abwerfen von Submunitionskörpern - Google Patents

Trägergeschoss mit einem Modulbehälter zum Abwerfen von Submunitionskörpern Download PDF

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Publication number
EP0424198B1
EP0424198B1 EP90402667A EP90402667A EP0424198B1 EP 0424198 B1 EP0424198 B1 EP 0424198B1 EP 90402667 A EP90402667 A EP 90402667A EP 90402667 A EP90402667 A EP 90402667A EP 0424198 B1 EP0424198 B1 EP 0424198B1
Authority
EP
European Patent Office
Prior art keywords
missile
container
lower pallet
submunitions
holding
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
EP90402667A
Other languages
English (en)
French (fr)
Other versions
EP0424198A1 (de
Inventor
Jacques Raynaud
Pascal Herquel
Roger Chantome
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to AT90402667T priority Critical patent/ATE100190T1/de
Publication of EP0424198A1 publication Critical patent/EP0424198A1/de
Application granted granted Critical
Publication of EP0424198B1 publication Critical patent/EP0424198B1/de
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

Definitions

  • the field of the invention is that of boarding, packaging and dropping submunitions from a carrier vehicle, such as a missile.
  • a carrier vehicle such as a missile.
  • the latter can also itself be carried by an aircraft and launched from it.
  • This type of device allows airplanes, and in general to other aircraft with on-board personnel, to fly over enemy lines or zones and drop submunitions on objectives.
  • Such devices are designed to be launched from the plane and are capable of taking on board and transporting towards the objectives to be reached, submunitions adapted to a determined mission.
  • Such devices consist mainly of a carrier vehicle and a cluster container. The role of the vehicle is to transport the container of submunitions to the objectives to be reached. The role of the container is to carry and drop the submunitions.
  • the different types of submunitions are all the more numerous as the missions can be different.
  • a cluster munition is designed specifically for a single type of cluster munition. Each new mission is defined a new submunition.
  • French patent application FR-A-2 555 731 describes a machine intended for the fight against armored vehicles and carrying one or more military charges, such as a hollow charge, intended to be propelled laterally with respect to the craft. Mention is made of the use of a pyrotechnic cord for cutting the panels surrounding the shaped charges.
  • the lower pallet, the cutting means windows and the two end frames being standard elements, whatever the types of on-board submunitions. This allows the composition of the batch of submunitions to be loaded on the lower pallet using the holding and ejection means, and then fixing this assembly to the lateral flanks.
  • the missile preferably comprises at least one intermediate frame for dividing the container into at least two different compartments.
  • the main embodiment of the container according to the invention provides that the holding and ejection means include support baskets fixed to the lower pallet, wedging pads, holding straps and pyrotechnically controlled ejection bellows.
  • the frames, the lower pallet and the lateral sides are made of sandwich panels composed of a first sheet of light alloy and of a second sheet of rigid composite material, between which foam is placed. absorbent.
  • the lower pallet has numerous fixing points for the holding and ejection means, consisting of fixing holes drilled in the first sheet and in a reinforcement made of composite material.
  • the lateral flanks are fixed to the upper flank by fixing bolts.
  • the window cutting means are pyrotechnic cords.
  • the drop missile 2 mainly comprises motor means 3, in this case a propulsion reactor, and a container 4.
  • the concept of modular container is illustrated here by the submunitions 10 of the front compartment 24 of the container which are different from the submunitions 11 of the rear compartment 26 of the container 4.
  • the containers of the prior art carry only one kind of submunitions.
  • These two front 24 and rear 26 compartments of the container 4 are shared by an intermediate frame 16, the ends front and rear of the container 4 being delimited by a front frame 12 and a rear frame 14.
  • the various submunitions 10 and 11 are held by holding and ejection means which will be detailed below.
  • Figure 2 which is a cross section of the missile according to the invention, there are the lower pallet 6, the upper flank 8 and the submunitions 10 of the front compartment, which are five in number.
  • the general structure of the modular container is completed by two lateral flanks 9.
  • the reinforced upper flank 8 has a large thickness. It constitutes a kind of rigid beam ensuring a large part of the rigidity of the missile structure.
  • the latter is supplemented by the fact that the lateral flanks 9 are rigidly fixed to this reinforced upper flank 8. They have means for cutting lateral windows made up of pyrotechnic cords 30.
  • the lower pallet 6 Before being assembled with the missile, the lower pallet 6 first receives the holding and ejection means as well as the submunitions 10.
  • the means for holding and ejecting the submunitions 10 mainly comprise support baskets of different types 32, 33.
  • at least one support basket 32 is fixed to the lower pallet 10
  • This first type of basket-support 32 contributes to maintaining the submunitions placed in the lower part of the container.
  • the submunitions are held in place with wedging pads 34, each fixed to a support basket 32 or 33.
  • the submunitions 10 are fixed to the wedging pads 34 by means of straps 36
  • the ejection is obtained using ejection bellows 38 containing air bags. The functioning of such ejection bellows is explained below with reference to FIGS. 3A and 3B.
  • the second type of basket-support 33 is intended to hold the submunitions 10 located in the upper part of the container. This second support basket 33 is therefore fixed to the first support 32.
  • the support baskets 32 are made of light alloy and are obtained either in foundries or in mechanically welded construction. They are bolted to the lower pallet and the frames.
  • FIG. 2A In the case of FIG. 2A, five submunitions 10 have been represented. Their ejection from the container is done through windows made in the lateral flanks 9 and the lower pallet 6, by means of a first set of pyrotechnic cords 30. The four lateral submunitions will be ejected laterally thanks to the windows cut in the flanks side 9 and part of the lower pallet 6. The central submunition, placed inside the first support basket 32 will be ejected through a window made in the lower pallet 6 by means of a second set of cutting cords 31 Each blocking pad 34 and ejection bellows 38 is placed relative to the corresponding submunition on the side opposite to the window through which the submunition must be ejected.
  • the lower pallet 6, the two lateral flanks 9 and their set of cutting cords 30 and 31 are standard, that is to say that they always have the same shape and the same structure, whatever the type of sub- on-board ammunition. It is the same for the end frames, marked 12 and 14 in FIG. 1. Only the structure constituting the holding and ejection means mounted on the lower pallet 6 changes according to the submunitions to be carried. There are indeed several types of support baskets, these can be easily assembled together and mounted on the lower pallet 6. For this purpose, it has very many fixing points 40. The same is true for the ejection and holding means, that is to say say that there are several types of timing pads 34, straps 36 and ejection bellows 38.
  • This modular container design is obtained by palletizing the batch of submunitions to be loaded. Indeed, it is possible to constitute on request, and at the last moment, a particular combination of different types of submunitions, according to a very precise mission to be carried out. The number and the different types of submunitions being determined, the different means of holding and ejecting the submunitions can then be mounted on the lower pallet 6. In fact, we choose the support baskets adapted to each type of submunitions and depending on the mounting of these submunitions in the container, and this for a particular use corresponding to the mission.
  • the rigid fixing of the side panels 9 on the upper side 8 can be carried out by different means.
  • a preferred embodiment is constituted by a fixing using bolts.
  • the lower pallet 6 is fixed to the lateral flanks 9 by screws around its periphery. It participates in the structural behavior of the missile.
  • the fixing points 40 on the lower pallet 6 are shown in detail in FIG. 2B. This also represents the structure of the lower pallet 6 and the lateral flanks 9. All of these elements, as well as the frames, consist of a sandwich panel. Such a panel is composed of a first sheet 44 of light alloy steel, of a second sheet 46 of rigid composite material, between which absorbent foam 48 is placed. At the place where one chooses to place a fixing point 40 for the means for holding and ejecting the submunitions, the foam 48 is replaced by a reinforcement 50 in the form of an omega connecting the first sheet 44 to second sheet 46. A bolt 42 passes through the thickness of the reinforcement 50 and of the first sheet 44 and constitutes the means for fixing a support basket 32.
  • FIGS. 3A and 3B The holding and ejection means are shown diagrammatically in FIGS. 3A and 3B.
  • FIG. 3A explains the operation of the ejection means, and in particular of the inflatable bag of the ejection bellows 38.
  • the latter has a first end rigidly fixed to a structure 52 of light alloy, itself integral with the basket -support.
  • the other end of the airbag 38 is movable and supports the timing pad 34, which is preferably made of hard foam.
  • the gas generator 54 supplies gas to the airbag 38, the latter inflates and expands by pushing the wedging pad 34, after rupture of the strap 36. The latter is then displaced by a length L with sufficient acceleration to eject the submunition.
  • FIG. 3B shows a gas generator 54 opening into a distribution ring 56.
  • the latter surrounds the airbag and the wedging pad 34 placed in the middle of the latter.
  • Handles 58 for fixing the holding straps 36 are integral with the support baskets and can be placed on this distribution crown 56.
  • Each strap 36 has a reduced section 37 at which the strap 36 breaks when it is stressed in extension by the submunition that is ejected.
  • a lower window 60 is made in the lower pallet 6.
  • the shape of this window corresponds to the profile of all submunitions placed centrally and at the bottom of the container.
  • a lateral window 62 is formed in a lateral flank 9, below the upper flank 8.
  • the shape of this lateral window 62 corresponds to the profile of all the submunitions to be ejected from the corresponding sidewall.
  • These lateral and lower windows are obtained at the time of ejection using pyrotechnic cords delimiting, by mixed lines, the shapes of these two windows 60 and 62.
  • the lateral windows 62 are astride the lower pallet 6 and the lateral flanks 9, two pyrotechnic cords are therefore necessary for each window 62.
  • the lower window 60 only one pyrotechnic cord is necessary. The ignition of the cords 64 is doubled to increase their reliability.
  • these pyrotechnic cords 64 are mounted against the internal sheet 66, and surrounded by silicone 68. This assembly is held by a longitudinal reinforcement 70.
  • All frames, intermediate or end are identical. They are made of light alloy foundry. They are bolted to the lower pallet. They also have fixing points necessary for some of the support baskets.
  • connection interface comprises a connector 20 for the supply of electric current to the container 4, a mechanical safety device 21 for the pyrotechnic chain of the container 4.
  • the connection interface also includes boxes for the pyrotechnic safety 22 of firing the cutting cords of the ejection windows and for the safety and firing of the gas generators and ejection systems. It may possibly include a security and initialization box for submunitions.
  • the connector 20 and the connection boxes 22 are placed on the rear frame 14 according to known means.
  • the ejection of the submunitions can be done in one or two stages, this depending on the type of submunitions.
  • Figure 5A reproduces the arrangement described in Figure 2. It shows five submunitions of large diameter ejected individually by five ejection systems.
  • FIG. 5B shows a second possibility of arrangement of the container with ten smaller submunitions 72. They are distributed symmetrically.
  • the upper submunitions 74 are ejected individually.
  • the submunitions 72 placed below these upper submunitions 74 are ejected in groups of two 76, each group 76 having its own ejection system 78. The latter is carried out in two stages.
  • the right part of this FIG. 5B shows the second stage when the two submunitions 72 of group 76 are separated by the ejection system means 78 which is specific to them.
  • FIG. 5C shows a system similar to that represented in FIG. 5B, except that the groups of submunitions 80 comprise three submunitions 82, separated in a second step after the ejection of group 80.
  • FIG. 5D shows a container comprising two groups of submunitions 84 of four submunitions 86. These two groups 84 are first ejected of the container each by their own ejection system. Once each group 84 is ejected from the container 4, the submunitions 86 are separated by an ejection system 88 which is specific to them.
  • the submunitions or groups of submunitions contained in the same basket can be ejected at different speeds by adapting the pyrotechnic charge for inflating the ejection bags.
  • the structure of the container according to the invention comprising identical elements whatever the types of submunitions used and standard elements, allows the layout of the batch of submunitions to be loaded.
  • the lower pallet can be fitted with holding and ejection systems containing submunitions chosen according to this mission.
  • the assembly is then mounted on the missile, under the upper flank and between the lateral flanks. The whole is fixed by screwing.

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  • 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)
  • Pallets (AREA)
  • Medical Preparation Storing Or Oral Administration Devices (AREA)
  • Toys (AREA)
  • Housing For Livestock And Birds (AREA)
  • Adornments (AREA)
  • Packaging Of Machine Parts And Wound Products (AREA)
  • Stackable Containers (AREA)

Claims (9)

  1. Rakete zum Abwerfen eines Loses Submunition, umfassend:
    - Antriebs- und Führungs-/Lenkungseinrichtungen (3);
    - einen Modulbehälter (4), den Rumpf der Rakete (2) bildend, beitragend zur strukturellen Steifheit des Raketenaufbaus und hauptsächlich enthaltend:
    - Einrichtungen zum Halten und Auswerfen der Submunitionskörper (10, 11 72, 74, 82, 86), um das Halten, den Transport und das Auswerfen von wenigstens einer Gruppe Submunitionskörper zu gewährleisten.;
    - eine verstärkte obere Flanke (8);
    - zwei fest mit der oberen Flanke (8) verbundene Seitenflanken (9), jede Schneideinrichtungen (30) von Seitenfenstern (62) enthaltend;
    - eine untere Palette (6), fest verbunden mit den beiden Seitenflanken (9) und Schneideinrichtungen (31) eines unteren Fensters (60) enthaltend, und die Halte- und Auswurfeinrichtungen tragend;
    - zwei Endrahmen (12, 14) des Behälters (4);
    - eine Verbindungsschnittstelle (20, 21, 22) des Behälters (4) mit der Rakete (2),
    wobei die untere Palette (6), die Seitenflanken (9), die Schneideinrichtungen der Fenster (30, 31) und die beiden Endrahmen (12, 14) Standardteile sind, unabhängig von den Typen der aufgenommenen Submunitionskörper, dies, um die Zusammensetzung des aufzunehmenden Submunitionsloses auf der unteren Palette (6) durchzuführen mittels Halte- und Auswurfeinrichtungen und diesen Aufbau anschließend an den Seitenflanken (9) zu befestigen.
  2. Rakete nach Anspruch 1, dadurch gekennzeichnet, daß sie wenigstens einen mittleren Rahmen (16) enthält, um den Behälter (4) in wenigstens zwei Abteile (24, 26) aufzuteilen.
  3. Rakete nach Anspruch 1, dadurch gekennzeichnet, daß die Halte- und Auswurfeinrichtungen Trägerkörbe (32), befestigt an der unteren Palette (6), Unterkeilungsfüße (34), Haltegurte (36) und pyrotechnisch betätigte Auswurfbälge (38) umfassen.
  4. Rakete nach Anspruch 1, dadurch gekennzeichnet, daß die Verbindungsschnittstelle umfaßt:
    - einen Steckverbinder (20) für die Versorgung des Behälters (4) mit elektrischem Strom;
    - eine mechanische Sicherheitseinrichtung (21), um die Unterbrechung der pyrotechnischen Ketten zu gewährleisten während die Rakete (2) sich auf einer Trägermaschine befindet; und
    - pyrotechnische Sicherheitsgehäuse (22).
  5. Rakete nach Anspruch 1, dadurch gekennzeichnet, daß die Rahmen (12, 14, 16), die untere Palette (6) und die Seitenflanken (9) aus Sandwich-Platten sind, gebildet durch ein erstes Blech (44) aus einem leichten Legierungsstahl und einem zweiten Blech (46) aus einem steifen Kompositmaterial, wobei zwischen diesen Blechen ein absorbierender Schaum angebracht ist.
  6. Rakete nach Anspruch 1, dadurch gekennzeichnet, daß die untere Palette (6) zahlreiche Befestigungspunkte (40) für die Halte- und Auswurfeinrichtungen aufweist, gebildet durch Befestigungslöcher, in das erste Blech (44) und eine Verstärkung (50) aus Kompositmaterial gebohrt.
  7. Rakete nach Anspruch 5, dadurch gekennzeichnet, daß die Seitenflanken (9) an der oberen Flanke (8) durch Befestigungsschrauben angebracht sind.
  8. Rakete nach Anspruch 5, dadurch gekennzeichnet, daß die untere Palette (6) an den Seitenflanken (9) mittels Schrauben befestigt ist.
  9. Rakete nach Anspruch 1, dadurch gekennzeichnet, daß die Schneideinrichtungen der Fenster pyrotechnische Schüre (30, 31) sind.
EP90402667A 1989-09-29 1990-09-27 Trägergeschoss mit einem Modulbehälter zum Abwerfen von Submunitionskörpern Expired - Lifetime EP0424198B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT90402667T ATE100190T1 (de) 1989-09-29 1990-09-27 Traegergeschoss mit einem modulbehaelter zum abwerfen von submunitionskoerpern.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8912767A FR2652642B1 (fr) 1989-09-29 1989-09-29 Missile de largage de sous-munitions equipe d'un conteneur modulable.
FR8912767 1989-09-29

Publications (2)

Publication Number Publication Date
EP0424198A1 EP0424198A1 (de) 1991-04-24
EP0424198B1 true EP0424198B1 (de) 1994-01-12

Family

ID=9385955

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90402667A Expired - Lifetime EP0424198B1 (de) 1989-09-29 1990-09-27 Trägergeschoss mit einem Modulbehälter zum Abwerfen von Submunitionskörpern

Country Status (7)

Country Link
US (1) US5094170A (de)
EP (1) EP0424198B1 (de)
AT (1) ATE100190T1 (de)
DE (1) DE69005979T2 (de)
DK (1) DK0424198T3 (de)
ES (1) ES2049947T3 (de)
FR (1) FR2652642B1 (de)

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US7004073B2 (en) * 2003-09-26 2006-02-28 Lockheed Martin Corporation System for dispensing projectiles and submunitions
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WO2008033170A2 (en) * 2006-05-16 2008-03-20 Textron Systems Corporation Controlled dispense system for deployment of components into desired pattern and orientation
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US8607685B2 (en) 2008-04-16 2013-12-17 QinetiQ North America, Inc. Load sharing hard point net
US20110079135A1 (en) 2008-04-16 2011-04-07 Farinella Michael D Vehicle and structure shield net/frame arrangement
US8245620B2 (en) * 2008-04-16 2012-08-21 QinetiQ North America, Inc. Low breaking strength vehicle and structure shield net/frame arrangement
US8443709B2 (en) * 2008-04-16 2013-05-21 QinetiQ North America, Inc. Vehicle and structure shield hard point
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US8615851B2 (en) * 2008-04-16 2013-12-31 Foster-Miller, Inc. Net patching devices
US8464627B2 (en) 2008-04-16 2013-06-18 QinetiQ North America, Inc. Vehicle and structure shield with improved hard points
US8677882B2 (en) 2010-09-08 2014-03-25 QinetiQ North America, Inc. Vehicle and structure shield with flexible frame
US8813631B1 (en) 2013-02-13 2014-08-26 Foster-Miller, Inc. Vehicle and structure film/hard point shield
FR3035076B1 (fr) * 2015-04-17 2018-04-20 Thales Procede d'amenagement d'une pluralite de vaisseaux spatiaux sous la coiffe d'un lanceur, assemblage resultant d'un tel procede et dispenser adapte a un tel assemblage
DE102016108951A1 (de) * 2016-05-13 2017-11-16 Jörg Kreisel Raumkörper
RU2636068C1 (ru) * 2016-09-06 2017-11-20 Акционерное общество "Научно-производственное объединение "Базальт" (АО "НПО "Базальт") Разовая бомбовая кассета

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Also Published As

Publication number Publication date
EP0424198A1 (de) 1991-04-24
ATE100190T1 (de) 1994-01-15
DK0424198T3 (da) 1994-05-30
US5094170A (en) 1992-03-10
DE69005979D1 (de) 1994-02-24
DE69005979T2 (de) 1994-07-14
FR2652642A1 (fr) 1991-04-05
ES2049947T3 (es) 1994-05-01
FR2652642B1 (fr) 1992-01-24

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