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EP1400773B1 - Device for adapting a multiple-rocket container to an artillery rocket launcher - Google Patents

Device for adapting a multiple-rocket container to an artillery rocket launcher Download PDF

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Publication number
EP1400773B1
EP1400773B1 EP03020826A EP03020826A EP1400773B1 EP 1400773 B1 EP1400773 B1 EP 1400773B1 EP 03020826 A EP03020826 A EP 03020826A EP 03020826 A EP03020826 A EP 03020826A EP 1400773 B1 EP1400773 B1 EP 1400773B1
Authority
EP
European Patent Office
Prior art keywords
container
frame
launcher
firer
fitted
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
EP03020826A
Other languages
German (de)
French (fr)
Other versions
EP1400773A2 (en
EP1400773A3 (en
Inventor
Rüdiger Dipl.-Ing. Baus
Frank Dipl.-Ing. Dieling
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.)
Krauss Maffei Wegmann GmbH and Co KG
Original Assignee
Krauss Maffei Wegmann GmbH and Co KG
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 Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP1400773A2 publication Critical patent/EP1400773A2/en
Publication of EP1400773A3 publication Critical patent/EP1400773A3/en
Application granted granted Critical
Publication of EP1400773B1 publication Critical patent/EP1400773B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket

Definitions

  • the invention relates to a device for adapting a plurality Artillerieraketen containing container to a launcher for artillery rockets with one in elevation and azimuth swiveling on a base frame, in particular a vehicle undercarriage stored, box-like launcher frame, in which at least one several Artillerieraketen containing, in its external dimensions to the inner dimensions of the launcher frame adapted container can be inserted with a rectangular cross-section from one end.
  • the invention is based on the object, a device for adaptation a container containing several artillery rockets a launcher for artillery rockets of the above and in the preamble of the patent claim 1 to create the type it allows, without changes to the launcher artillery rockets other type, in a container with other external dimensions are arranged to shoot.
  • the basic idea of the invention consists in differing Outside dimensions of a container to be used on this on the top and / or bottom of each a matching module to set, which is designed so that after the preparation and Attaching one or two adjustment modules of the container exactly has the outer dimensions that allow him in the Insert the launcher frame and fasten it there. It has have proven to be useful if, on the outsides of the adaptation modules, so at the top of the upper adjustment module and the bottom of the lower adjustment module, exactly the fastening devices are arranged, on the one hand needed to store and transport the container, and on the other hand, to fix him in the launcher frame.
  • the adaptation modules form a weapon interface that makes it possible without changing the mechanical interface of the launcher even other artillery rockets or guided missiles use.
  • Fig. 1 shows a combat vehicle with a vehicle undercarriage 1, on a cab 2 is arranged, as well as a launcher for artillery rockets, a launcher frame 3 for recording of missiles.
  • the launcher frame 3 is pivotable in elevation arranged on a top mount 4, which has a not shown Intermediate frame and a turntable in azimuth swivel is mounted on the vehicle undercarriage 1.
  • the pivoting movement in elevation is through between upper mount 4 and launcher frame 3rd arranged, electrically driven lifting spindles 5 causes.
  • In the box-like launcher frame 3 are two containers from the ends 6 inserted, each receiving six artillery rockets can.
  • the loading of the launcher frame 3 is using lifting means performed, each having two support arms 7, in which in not specifically shown way hoists are arranged.
  • Fig. 2 is one of the usual, in the launcher according to Fig.1 insertable container 6 shown. It is about one Longitudinal beams and cross members constructed, frame-like container.
  • the side members 6.1, 6.2 and 6.3 and in horizontal and vertical direction extending cross member visible from two, for example, provided with reference numerals 6.5 and 6.6 are.
  • container 6 six artillery rockets 8 are arranged. At the Top of the container 6 is a fastening device 9 for the transport of the container, at the bottom are fastening devices 10.1, 10.2 and 10.3 arranged for attachment of the container 6 within the launcher frame 3.
  • Fig. 3 shows a container 11, in a manner not shown a plurality Artillery rockets may contain and its external dimensions are smaller than the inner dimensions of the launcher frame 3, so that this container is not inserted into the launcher frame 3 and there could be attached.
  • an adaptation module 12.1 and at the bottom of the container 11 an adaptation module 12.2 arranged.
  • the Both adaptation modules 12.1 and 12.2 are in length, width and Thickness in each case dimensioned so that the dimensions of the Container 11 and the two adaptation modules 12.1 and 12.2 assembled device in length, width and height exactly correspond to the corresponding internal dimensions of the launcher frame, so that insertion into the launcher frame 3 is possible.
  • the Adaptation modules 12.1 and 12.2 are designed as flat plates made of aluminum or steel and formed by longitudinal rails 13.1 and 13.2 strengthened. The attachment of the adaptation modules 12.1, 12.2 am Container 1 via fastening devices, not shown.
  • the adaptation module 12.1 At the top of the adaptation module 12.1, as a transport module is formed, there is a suspension 15 for Suspension of the container on a hoist and hinged Lifting eyes 14.1, 14.2, 14.3 and 14.4.
  • the Adaptation module 12.2 At the bottom of the Adaptation module 12.2, which is designed as a lashing module, are located not shown fastening devices for fastening within the launcher frame 3.

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  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
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Abstract

The adapter device (12.1, 12.2) comprises a flat rectangular plate which can be placed against and secured to the top and/or bottom side of the container (11) so that the external dimensions of the latter correspond to the internal dimensions of the launcher frame. The rocket launcher has a box-shaped launcher frame with an adjustable elevation and azimuth mounted on an undercarriage, preferably a vehicle. The container has a rectangular cross-section and can be slid into one end of the launcher frame.

Description

Die Erfindung betrifft eine Einrichtung zur Anpassung eines mehrere Artillerieraketen enthaltenden Containers an eine Abschußvorrichtung für Artillerieraketen mit einem in Elevation und Azimut schwenkbar auf einem Untergestell, insbesondere einem Fahrzeuguntergestell gelagerten, kastenartigen Werferrahmen, in welchen mindestens ein mehrere Artillerieraketen enthaltender, in seinen Außenabmessungen an die Innenabmessungen des Werferrahmens angepaßter Container mit rechteckigem Querschnitt von einem Ende her einschiebbar ist.The invention relates to a device for adapting a plurality Artillerieraketen containing container to a launcher for artillery rockets with one in elevation and azimuth swiveling on a base frame, in particular a vehicle undercarriage stored, box-like launcher frame, in which at least one several Artillerieraketen containing, in its external dimensions to the inner dimensions of the launcher frame adapted container can be inserted with a rectangular cross-section from one end.

Eine auf einem Kampffahrzeug angeordnete derartige Abschußvorrichtung für Artillerieraketen ist beispielsweise in EP 0 664 431 B1 beschrieben. Bei dieser bekannten Abschußvorrichtung müssen die Container, welche die Artillerieraketen enthalten, genau an die Innenabmessungen des Werferrahmens angepaßt sein. Dies bedeutet, daß, wenn Artillerieraketen oder Lenkflugkörper eines anderen Typs verschossen werden sollen, die Abschußvorrichtung entsprechend angepaßt werden muß, was einen beträchtlichen Aufwand darstellt.A mounted on a combat vehicle such launcher for artillery rockets is described for example in EP 0 664 431 B1 described. In this known launcher must Containers containing the artillery rockets, exactly to the inner dimensions be adapted to the pitcher frame. This means, that if artillery rockets or guided missiles of another type to be fired, the launcher accordingly must be adapted, which is a considerable effort.

Der Erfindung liegt die Aufgabe zugrunde, eine Einrichtung zur Anpassung eines mehrere Artillerieraketen enthaltenden Containers an eine Abschußvorrichtung für Artillerieraketen der oben und im Oberbegriff des Patentanspruchs 1 beschriebenen Bauart zu schaffen, die es erlaubt, ohne Änderungen an der Abschußvorrichtung Artillerieraketen anderen Typs, die in einem Container mit anderen Außenabmessungen angeordnet sind, zu verschießen.The invention is based on the object, a device for adaptation a container containing several artillery rockets a launcher for artillery rockets of the above and in the preamble of the patent claim 1 to create the type it allows, without changes to the launcher artillery rockets other type, in a container with other external dimensions are arranged to shoot.

Die Lösung dieser Aufgabe erfolgt erfindungsgemäß mit den Merkmalen aus dem kennzeichnenden Teil des Patentanspruchs 1. Vorteilhafte Weiterbildungen der Erfindung sind in den abhängigen Ansprüchen beschrieben.The solution to this problem is inventively with the Characteristics of the characterizing part of patent claim 1. Advantageous developments of the invention are in the dependent Claims described.

Der Grundgedanke der Erfindung besteht darin, bei abweichenden Außenabmessungen eines zu verwendenden Containers an diesen an der Ober- und/oder der Unterseite jeweils ein Anpassungsmodul anzusetzen, welches so ausgebildet ist, daß nach dem Ansetzen und Befestigen von ein oder zwei Anpassungsmodulen der Container genau die Außenabmessungen besitzt, die es ermöglichen, ihn in den Werferrahmen einzuschieben und dort zu befestigen. Dabei hat es sich als zweckmäßig erwiesen, wenn an den Außenseiten der Anpassungsmodule, also an der Oberseite des oberen Anpassungsmoduls und der Unterseite des unteren Anpassungsmoduls, genau die Befestigungsvorrichtungen angeordnet sind, die einerseits benötigt werden, um den Container zu lagern und zu transportieren, und andererseits dazu, ihn im Werferrahmen zu befestigen. Die Anpassungsmodule bilden also eine Waffenschnittstelle, die es ermöglicht, ohne Änderung der mechanischen Schnittstelle der Abschußvorrichtung selbst andere Artillerieraketen bzw. Lenkflugkörper zu verwenden.The basic idea of the invention consists in differing Outside dimensions of a container to be used on this on the top and / or bottom of each a matching module to set, which is designed so that after the preparation and Attaching one or two adjustment modules of the container exactly has the outer dimensions that allow him in the Insert the launcher frame and fasten it there. It has have proven to be useful if, on the outsides of the adaptation modules, so at the top of the upper adjustment module and the bottom of the lower adjustment module, exactly the fastening devices are arranged, on the one hand needed to store and transport the container, and on the other hand, to fix him in the launcher frame. The adaptation modules form a weapon interface that makes it possible without changing the mechanical interface of the launcher even other artillery rockets or guided missiles use.

Im folgenden wird anhand der beigefügten Zeichnungen ein Ausführungsbeispiel für eine Einrichtung nach der Erfinung näher erläutert.In the following an embodiment will be described with reference to the accompanying drawings for a device according to the Erfinung explained in more detail.

In den Zeichnungen zeigen:

  • Fig. 1 in einer perspektivischen Darstellung schräg von hinten ein Kampffahrzeug mit einer Abschußvorrichtung für Artillerieraketen;
  • Fig. 2 in einer perspektivischen Darstellung einen sechs Artillerieraketen enthaltenden Container üblicher Bauart zum Abschuß aus der Abschußvorrichtung nach Fig. 1;
  • Fig. 3 in perspektivischer Darstellung einen Container mit anderen Abmessungen als denen der üblichen Container mit Anpassungsmodulen für den Abschuß aus einer Abschußvorrichtung nach Fig. 1.
    • In the drawings show:
  • Figure 1 is a perspective view obliquely from behind a combat vehicle with a launcher for artillery rockets.
  • Fig. 2 is a perspective view of a six Artillerieraketen containing container of conventional design for firing from the launcher of FIG. 1;
  • 3 is a perspective view of a container with different dimensions than those of the usual container with adaptation modules for the launch of a launcher of FIG .. 1

    • Fig. 1 zeigt ein Kampffahrzeug mit einem Fahrzeuguntergestell 1, auf dem ein Fahrerhaus 2 angeordnet ist, sowie eine Abschußvorrichtung für Artillerieraketen, die einen Werferrahmen 3 zur Aufnahme der Raketen aufweist. Der Werferrahmen 3 ist in Elevation schwenkbar auf einer Oberlafette 4 angeordnet, die über einen nicht dargestellten Zwischenrahmen und einen Drehkranz in Azimut schwenkbar auf dem Fahrzeuguntergestell 1 gelagert ist. Die Schwenkbewegung in Elevation wird durch zwischen Oberlafette 4 und Werferrahmen 3 angeordnete, elektrisch angetriebene Hubspindeln 5 bewirkt. In den kastenartigen Werferrahmen 3 sind von den Enden her zwei Container 6 eingeschoben, die jeweils sechs Artillerieraketen aufnehmen können. Das Beladen des Werferrahmens 3 wird mit Hebemitteln durchgeführt, welche jeweils zwei Tragarme 7 besitzen, an denen in nicht eigens dargestellter Weise Hebezeuge angeordnet sind.Fig. 1 shows a combat vehicle with a vehicle undercarriage 1, on a cab 2 is arranged, as well as a launcher for artillery rockets, a launcher frame 3 for recording of missiles. The launcher frame 3 is pivotable in elevation arranged on a top mount 4, which has a not shown Intermediate frame and a turntable in azimuth swivel is mounted on the vehicle undercarriage 1. The pivoting movement in elevation is through between upper mount 4 and launcher frame 3rd arranged, electrically driven lifting spindles 5 causes. In the box-like launcher frame 3 are two containers from the ends 6 inserted, each receiving six artillery rockets can. The loading of the launcher frame 3 is using lifting means performed, each having two support arms 7, in which in not specifically shown way hoists are arranged.

    In Fig. 2 ist einer der üblichen, in die Abschußvorrichtung nach Fig.1 einschiebbaren Container 6 dargestellt. Es handelt sich um einen aus Längsträgern und Querträgern aufgebauten, rahmenartigen Container. In Fig. 2 sind die Längsträger 6.1, 6.2 und 6.3 sowie in horizontaler und vertikaler Richtung verlaufende Querträger sichtbar, von denen zwei beispielsweise mit Bezugsziffer 6.5 und 6.6 versehen sind.In Fig. 2 is one of the usual, in the launcher according to Fig.1 insertable container 6 shown. It is about one Longitudinal beams and cross members constructed, frame-like container. In Fig. 2, the side members 6.1, 6.2 and 6.3 and in horizontal and vertical direction extending cross member visible from two, for example, provided with reference numerals 6.5 and 6.6 are.

    Im Container 6 sind sechs Artillerieraketen 8 angeordnet. An der Oberseite des Containers 6 befindet sich eine Befestigungsvorrichtung 9 für den Transport des Containers, an der Unterseite sind Befestigungsvorrichtungen 10.1, 10.2 und 10.3 angeordnet zur Befestigung des Containers 6 innerhalb des Werferrahmens 3.In container 6 six artillery rockets 8 are arranged. At the Top of the container 6 is a fastening device 9 for the transport of the container, at the bottom are fastening devices 10.1, 10.2 and 10.3 arranged for attachment of the container 6 within the launcher frame 3.

    Fig. 3 zeigt einen Container 11, der in nicht dargestellter Weise mehrere Artillerieraketen enthalten kann und dessen Außenabmessungen kleiner sind als die Innenabmessungen des Werferrahmens 3, so daß dieser Container nicht in den Werferrahmen 3 eingeschoben und dort befestigt werden könnte. Um dies zu erreichen, ist an der Oberseite des Containers 11 ein Anpassungsmodul 12.1 und an der Unterseite des Containers 11 ein Anpassungsmodul 12.2 angeordnet. Die beiden Anpassungsmodule 12.1 und 12.2 sind in Länge, Breite und Dicke jeweils so dimensioniert, daß die Abmessungen der aus dem Container 11 und den beiden Anpassungsmodulen 12.1 und 12.2 zusammengesetzten Einrichtung in Länge, Breite und Höhe genau den entsprechenden Innenabmessungen des Werferrahmens entsprechen, so daß ein Einschieben in den Werferrahmen 3 möglich ist. Die Anpassungsmodule 12.1 und 12.2 sind als flache Platten aus Aluminium oder Stahl ausgebildet und durch Längsschienen 13.1 und 13.2 verstärkt. Die Befestigung der Anpassungsmodule 12.1, 12.2 am Container 1 erfolgt über nicht dargestellte Befestigungsvorrichtungen.Fig. 3 shows a container 11, in a manner not shown a plurality Artillery rockets may contain and its external dimensions are smaller than the inner dimensions of the launcher frame 3, so that this container is not inserted into the launcher frame 3 and there could be attached. To achieve this is at the top of the container 11, an adaptation module 12.1 and at the bottom of the container 11 an adaptation module 12.2 arranged. The Both adaptation modules 12.1 and 12.2 are in length, width and Thickness in each case dimensioned so that the dimensions of the Container 11 and the two adaptation modules 12.1 and 12.2 assembled device in length, width and height exactly correspond to the corresponding internal dimensions of the launcher frame, so that insertion into the launcher frame 3 is possible. The Adaptation modules 12.1 and 12.2 are designed as flat plates made of aluminum or steel and formed by longitudinal rails 13.1 and 13.2 strengthened. The attachment of the adaptation modules 12.1, 12.2 am Container 1 via fastening devices, not shown.

    An der Oberseite des Anpassungsmoduls 12.1, das als Transportmodul ausgebildet ist, befindet sich eine Aufhängevorrichtung 15 zur Aufhängung des Containers an einem Hebezeug sowie klappbare Transportösen 14.1, 14.2, 14.3 und 14.4. An der Unterseite des Anpassungsmoduls 12.2, das als Zurrmodul ausgebildet ist, befinden sich nicht dargestellte Befestigungsvorrichtungen zum Befestigen innerhalb des Werferrahmens 3.At the top of the adaptation module 12.1, as a transport module is formed, there is a suspension 15 for Suspension of the container on a hoist and hinged Lifting eyes 14.1, 14.2, 14.3 and 14.4. At the bottom of the Adaptation module 12.2, which is designed as a lashing module, are located not shown fastening devices for fastening within the launcher frame 3.

    Claims (4)

    1. An apparatus for adapting a container (11) containing a plurality of artillery rockets to a launching mechanism for artillery rockets having a box-type firer frame (3) mounted on an underframe, in particular a vehicle chassis (1), so as to be pivotable in elevation and azimuth, into which firer frame (3) at least one container (11) containing a plurality of artillery rockets, conformed in its external dimensions to the internal dimensions of the firer frame (3) and having a rectangular cross-section may be inserted from one end, characterised in that, in the case of a container (11) with smaller external dimensions, an adapter module (12.1, 12.2) substantially in the form of a rectangular, flat plate may be fitted to the top and/or bottom of the container and fastened thereto, the external dimensions of which adapter module (12.1, 12.2) are such that the container (11) with fitted adapter module or fitted adapter modules (12.1, 12.2) corresponds in its external dimensions to the internal dimensions of the firer frame (3).
    2. An apparatus according to claim 1, characterised in that an adapter module (12.1) fitted to the top of the container (11) takes the form of a transport module, which comprises on its outer side at least one suspension device (15) designed for transportation of the container.
    3. An apparatus according to claim 1 or claim 2, characterised in that an adapter module (12.2) fitted to the bottom of the container (11) takes the form of an anchor module, which comprises fastening devices on its outer side for fastening the container in the firer frame (3).
    4. An apparatus according to claim 2, characterised in that, in the edge areas of at least one adapter module (12.1), transport eyelets (14.1, 14.2, 14.3, 14.4) are arranged for fastening purposes on the container (11) during transportation.
    EP03020826A 2002-09-23 2003-09-13 Device for adapting a multiple-rocket container to an artillery rocket launcher Expired - Lifetime EP1400773B1 (en)

    Applications Claiming Priority (2)

    Application Number Priority Date Filing Date Title
    DE20214679U 2002-09-23
    DE20214679U DE20214679U1 (en) 2002-09-23 2002-09-23 Device for adapting a container containing several artillery rockets to a launching device for artillery rockets

    Publications (3)

    Publication Number Publication Date
    EP1400773A2 EP1400773A2 (en) 2004-03-24
    EP1400773A3 EP1400773A3 (en) 2004-03-31
    EP1400773B1 true EP1400773B1 (en) 2005-01-05

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    ID=31896435

    Family Applications (1)

    Application Number Title Priority Date Filing Date
    EP03020826A Expired - Lifetime EP1400773B1 (en) 2002-09-23 2003-09-13 Device for adapting a multiple-rocket container to an artillery rocket launcher

    Country Status (5)

    Country Link
    US (1) US6901838B2 (en)
    EP (1) EP1400773B1 (en)
    AT (1) ATE286590T1 (en)
    DE (2) DE20214679U1 (en)
    DK (1) DK1400773T3 (en)

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    WO2020093115A1 (en) * 2018-11-09 2020-05-14 Mac Jee Indústria De Defesa Ltda. Replenishment system for a rocket launcher vehicle

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    IL169481A (en) * 2005-06-30 2011-11-30 Rafael Advanced Defense Sys Mobile carrier for a projectile launcher
    FR2936305B1 (en) * 2008-09-24 2010-10-22 Nexter Systems MANUALLY RETRACTABLE TURRET
    DE102010016542C5 (en) * 2010-04-20 2017-08-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Apparatus and method for straightening a launching container
    DE102011054963B3 (en) * 2011-10-31 2013-01-03 Krauss-Maffei Wegmann Gmbh & Co. Kg Military vehicle, transport container and method for stowing equipment
    US10386167B2 (en) * 2016-02-26 2019-08-20 General Dynamics—OTS, Inc. Ammunition container with improved latching and sealing arrangements
    EP3671100A4 (en) * 2017-08-17 2021-03-10 Mac Jee Industria de Defesa Ltda. Rocket launch module and rocket launch vehicle
    IT201800004993A1 (en) * 2018-05-02 2019-11-02 Missile launch unit and missile launcher including said launch unit
    CN110104197B (en) * 2019-04-03 2022-06-17 贵州航天天马机电科技有限公司 Small rocket launching pad
    CN111765808A (en) * 2020-07-10 2020-10-13 北京星途探索科技有限公司 Novel storage, transportation and delivery module
    US20230088169A1 (en) * 2020-11-08 2023-03-23 Noam Kenig System and methods for aiming and guiding interceptor UAV

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    Also Published As

    Publication number Publication date
    DK1400773T3 (en) 2005-04-04
    US6901838B2 (en) 2005-06-07
    US20040134338A1 (en) 2004-07-15
    EP1400773A2 (en) 2004-03-24
    DE20214679U1 (en) 2004-02-19
    DE50300239D1 (en) 2005-02-10
    EP1400773A3 (en) 2004-03-31
    ATE286590T1 (en) 2005-01-15

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