EP1825211B1 - Combat vehicle with anti-aircraft system - Google Patents

Combat vehicle with anti-aircraft system Download PDF

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Publication number
EP1825211B1
EP1825211B1 EP05849522A EP05849522A EP1825211B1 EP 1825211 B1 EP1825211 B1 EP 1825211B1 EP 05849522 A EP05849522 A EP 05849522A EP 05849522 A EP05849522 A EP 05849522A EP 1825211 B1 EP1825211 B1 EP 1825211B1
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EP
European Patent Office
Prior art keywords
combat vehicle
vehicle
combat
firing device
vehicle 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.)
Not-in-force
Application number
EP05849522A
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German (de)
French (fr)
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EP1825211A1 (en
Inventor
Frank Dieling
Andreas Pollert
Manfred Kempin
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.)
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Publication date
Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Priority to PL05849522T priority Critical patent/PL1825211T3/en
Publication of EP1825211A1 publication Critical patent/EP1825211A1/en
Application granted granted Critical
Publication of EP1825211B1 publication Critical patent/EP1825211B1/en
Not-in-force legal-status Critical Current
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
    • F41A23/34—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles on wheeled or endless-track vehicles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
    • F41A23/20—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles for disappearing guns

Definitions

  • the invention relates to a combat vehicle with anti-aircraft system having the features of the preamble of patent claim 1.
  • Such a combat vehicle is in EP 03 88 762 A2 described. It is a military combat vehicle upgrade kit with a combat platform that can be a simple rocket box and is located on the roof of a battle tank behind the tower. The rocket box can be erected to launch from the horizontal position to the vertical.
  • DE 102 47 350 A1 a device for the protection of objects against ammunition designed as a missile, which may also be arranged on a combat vehicle and in which warning sensors are arranged on a common equipment carrier above a launching device for firing action means.
  • the invention has the object of providing a combat vehicle with anti-aircraft system having the features of the preamble of claim 1, so as to form an anti-aircraft hybrid system that allows the use of both guns and missiles as a means of action on a weapon system
  • a basic idea of the invention is that the launcher for launching in the vertical direction Lenklug emotions is arranged at the rear of the combat vehicle, that they in two movement steps from a transport position in which they are preferably in the vehicle contour is integrated and oriented horizontally, is movable into a Abschuswolf in which it is vertically aligned and can be arranged at a predetermined distance from the vehicle.
  • the combat vehicle shown in the drawings has a vehicle trough 1, which is supported by a chain chassis 1.1.
  • a rotatable in azimuth tower 3 is arranged, which is equipped with a designed as a twin-tube weapon machine gun 4.
  • a target assignment radar device 5 is arranged at the turret rear, which is located in the working position above the machine gun 4 and - as in Fig. 4 with 5 'indicated - is formed foldable.
  • a target tracking sensor 6 is arranged on the tower front, and on the tower roof is an additional, regardless of mounted to other sensors directional all-round sensor 7, the crew allows the optronische terrain monitoring using a CCD camera or thermal imaging device.
  • the machine gun 4 represents a first means of action for air defense.
  • a second active means is provided, which is designed as a launching device 8 or 8 'for launching missile in the vertical direction.
  • the launcher can take two positions, namely once a Abschuswolf in which it is vertically aligned and arranged at a predetermined distance from the vehicle pan and on the other hand, a transport position in which it is aligned horizontally and integrated into the vehicle contour.
  • a transport position in which it is aligned horizontally and integrated into the vehicle contour.
  • the firing position respectively denoted by reference numeral 8.
  • two such launchers 8 and 8 'are provided, which are arranged on both sides of the vehicle longitudinal axis at the rear of the vehicle.
  • the integration of the launcher in the vehicle contour is done in the trained as a tracked vehicle combat vehicle by the launcher 8 'are arranged in the transport position in each case in the chain case 1.3 parallel to the vehicle longitudinal axis.
  • the movement of the launcher from the transport position to the Abschuswolf done in two steps.
  • a first movement step the horizontal launching device 8 'is displaced horizontally in a horizontal plane perpendicular to the vehicle longitudinal axis until the launching device lies outside the vehicle contour.
  • a second movement step then takes place a pivoting of the launching device from the horizontal to the vertical position, which is designated by reference numeral 8.
  • each launching device is associated with a bearing and drive unit 9 arranged at the rear of the combat vehicle.
  • This serves u.a. for the storage of transversely across the vehicle width reaching linear guideways 9.2, on which slidable holders are guided, are arranged on which outwardly facing, in its longitudinal direction in a horizontal plane perpendicular to the vehicle longitudinal axis slidable support arms 9.1.
  • the support arms can be moved 9.1 to the outside.
  • each launcher 8 ' is pivotally mounted about a horizontal, perpendicular to the vehicle longitudinal axis pivot axis.
  • Both the sliding movement and the pivotal movement of the launcher are arranged by arranged in the storage and drive units 9, not shown electrical drive devices.
  • the drive device for the pivoting movement of the Abschuss dressed is realized by a cable 10, which in the Fig. 1 . 3 and 4 is indicated in its visible to the outside elements.
  • a cable 10 which in the Fig. 1 . 3 and 4 is indicated in its visible to the outside elements.
  • the respective storage and drive unit 9 is a driven by a drive motor, not shown, cable drum on which the pull cable 10 is wound.
  • the traction cable 10 is guided via cable guides or rollers to the launcher 8 or 8 ', the end 10.1 of the traction cable 10 being fastened in the region of the end of the launcher 8 or 8' facing away from the pivot axis.
  • the launcher 8 ' is pivoted down under the effect of the dead weight of the launcher, while the swinging up takes place via the pull cable 10.
  • the end positions of the movements are secured by locking devices, not shown.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Automatic Cycles, And Cycles In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Emergency Protection Circuit Devices (AREA)

Abstract

The invention relates to a combat vehicle with an anti-aircraft system. A device carrier configured as an azimuth-pivotable turret (4) is arranged on the top side of the combat vehicle (1), and carries as the first effective element for the purpose of air defense an automatic weapon (4) which can be pivoted into an elevation position. The second effective element for the purpose of air defense is at least one launching device (8', 8) for vertically taking off guided missiles mounted at the rear of the combat vehicle (1). The launching device (8', 8) can be displaced from a horizontal transport position into a vertically oriented launching position. The launching device (8') can be integrated into the vehicle contour in the transport position and can be arranged at a defined distance to the combat vehicle in the launching position.

Description

Die Erfindung betrifft ein Kampffahrzeug mit Flugabwehrsystem mit den Merkmalen aus dem Oberbegriff des Patentanspruchs 1.The invention relates to a combat vehicle with anti-aircraft system having the features of the preamble of patent claim 1.

Ein derartiges Kampffahrzeug ist in EP 03 88 762 A2 beschrieben. Es handelt sich hier um einen Rüstsatz für militärische Kampffahrzeuge mit einer Kampfplattform, die als einfache Raketenbox ausgeführt sein kann und auf dem Dach eines Kampfpanzers hinter dem Turm angeordnet ist. Die Raketenbox kann zum Abschuss aus der horizontalen Lage bis zur senkrechten aufgerichtet werden.Such a combat vehicle is in EP 03 88 762 A2 described. It is a military combat vehicle upgrade kit with a combat platform that can be a simple rocket box and is located on the roof of a battle tank behind the tower. The rocket box can be erected to launch from the horizontal position to the vertical.

Kampffahrzeuge mit Flugabwehrsystem sind weiterhin in den Dokumenten DE 100 24 320 C2 und DE 34 10 467 A1 beschrieben.Combat vehicles with air defense system are still in the documents DE 100 24 320 C2 and DE 34 10 467 A1 described.

Bei der Einrichtung nach DE 100 24 320 C2 ist das erste am drehbaren Geräteträger angeordnete Wirkmittel als Abschussbehälter für schnelle Splittergranaten ausgebildet.When setting up DE 100 24 320 C2 is the first arranged on the rotatable device carrier active agent designed as a launching container for fast fragmentation grenades.

Bei der Einrichtung nach DE 34 10 467 A1 ist das erste Wirkmittel als auf einem Karapfpanzerturm angeordnetes Abschussgerät zum Abschießen von Wurfkörpern ausgebildet.When setting up DE 34 10 467 A1 is the first means of action as arranged on a carapace turret launcher designed for launching throwing bodies.

Es ist weiterhin aus DE 102 47 350 A1 eine Einrichtung zum Schutz von Objekten gegen als Lenkflugkörper ausgebildete Munitionen bekannt, die auch auf einem Kampffahrzeug angeordnet sein kann und bei der an einem gemeinsamen Geräteträger oberhalb einer Abschussvorrichtung für abschießbare Wirkmittel Warnsensoren angeordnet sind.It is still out DE 102 47 350 A1 a device for the protection of objects against ammunition designed as a missile, which may also be arranged on a combat vehicle and in which warning sensors are arranged on a common equipment carrier above a launching device for firing action means.

Schließlich ist es aus US 5 661 254 bekannt, an einem Kampffahrzeug eine in Azimut und Elevation verschwenkbare Abschussvorrichtung für Lenkflugkörper anzuordnen.Finally it is over US 5,661,254 known to arrange a launch vehicle for missile pivotable in azimuth and elevation on a combat vehicle.

Der Erfindung liegt die Aufgabe zugrunde, ein Kampffahrzeug mit Flugabwehrsystem, das die Merkmale aus dem Oberbegriff des Patentanspruchs 1 aufweist, so auszubilden, dass ein Flugabwehr-Hybridsystem entsteht, das die Verwendung sowohl von Rohrwaffen als auch von Lenkflugkörpern als Wirkmittel auf einem Waffensystem ermöglichtThe invention has the object of providing a combat vehicle with anti-aircraft system having the features of the preamble of claim 1, so as to form an anti-aircraft hybrid system that allows the use of both guns and missiles as a means of action on a weapon system

Die Lösung dieser Aufgabe geschieht erfindungsgemäß mit den Merkmalen aus dem kennzeichnenden Teil des Patentanspruchs 1. Vorteilhafte Weiterbildungen der Erfindung sind in den abhängigen Ansprüchen beschrieben.The solution of this object is achieved according to the invention with the features of the characterizing part of claim 1. Advantageous developments of the invention are described in the dependent claims.

Ein Grundgedanke der Erfindung besteht darin, dass die Abschussvorrichtung für in vertikaler Richtung startende Lenklugkörper derart am Heck des Kampffahrzeugs angeordnet ist, dass sie in zwei Bewegungsschritten aus einer Transportstellung, in der sie vorzugsweise in die Fahrzeugkontur integriert und horizontal ausgerichtet ist, in eine Abschusstellung bewegbar ist, in der sie vertikal ausgerichtet ist und in einem vorgegebenen Abstand vom Fahrzeug angeordnet sein kann.A basic idea of the invention is that the launcher for launching in the vertical direction Lenklugkörper is arranged at the rear of the combat vehicle, that they in two movement steps from a transport position in which they are preferably in the vehicle contour is integrated and oriented horizontally, is movable into a Abschusstellung in which it is vertically aligned and can be arranged at a predetermined distance from the vehicle.

Im folgenden wird anhand der beigefügten Zeichnungen ein Ausführungsbeispiel für ein Kampffahrzeug mit Flugabwehrsystem nach der Erfindung näher erläutert.In the following an embodiment of a combat vehicle with anti-aircraft system according to the invention will be explained in more detail with reference to the accompanying drawings.

In den Zeichnungen zeigen:

Fig. 1
in Seitenansicht ein Kampffahrzeug mit einem Flugabwehrsystem;
Fig. 2
in Aufsicht das Kampffahrzeug nach Fig. 1;
Fig. 3
in perspektivischer Darstellung von vorne das Kampffahrzeug nach Fig. 1 und 2 mit einer Abschussvorrichtung für Lenkflugkörper in der Transportstellung;
Fig. 4
in perspektivischer Darstellung von hinten das Kampffahrzeug nach Fig. 1 und 2 mit der Abschussvorrichtung für Lenkflugkörper in der Abschusstellung.
In the drawings show:
Fig. 1
in side view a combat vehicle with an air defense system;
Fig. 2
in supervision the combat vehicle after Fig. 1 ;
Fig. 3
in perspective from the front of the combat vehicle after Fig. 1 and 2 with a launcher for guided missiles in the transport position;
Fig. 4
in perspective from behind the combat vehicle after Fig. 1 and 2 with the missile launcher in the launch position.

Das in den Zeichnungen dargestellte Kampffahrzeug besitzt eine Fahrzeugwanne 1, die von einem Kettenfahrwerk 1.1 getragen wird. Auf der Dachplatte 1.2 der Fahrzeugwanne 1 ist ein in Azimut verdrehbarer Turm 3 angeordnet, der mit einer als Zwillingsrohrwaffe ausgebildeten Maschinenwaffe 4 bestückt ist. Weiterhin ist am Turmheck ein Zielzuweisungs-Radargerät 5 angeordnet, das in der Arbeitsstellung oberhalb der Maschinenwaffe 4 liegt und - wie in Fig. 4 mit 5' angedeutet - einklappbar ausgebildet ist. Zwischen den Waffenrohren der Maschinenwaffe 4 ist an der Turmfront ein Zielverfolgungs-Sensor 6 angeordnet, und auf dem Turmdach ist ein zusätzlicher, unabhängig von anderen Sensoren richtbarer Rundumblicksensor 7 montiert, der der Besatzung die optronische Geländeüberwachung mittels CCD-Kamera oder Wärmebildgerät ermöglicht.The combat vehicle shown in the drawings has a vehicle trough 1, which is supported by a chain chassis 1.1. On the roof panel 1.2 of the vehicle pan 1, a rotatable in azimuth tower 3 is arranged, which is equipped with a designed as a twin-tube weapon machine gun 4. Furthermore, a target assignment radar device 5 is arranged at the turret rear, which is located in the working position above the machine gun 4 and - as in Fig. 4 with 5 'indicated - is formed foldable. Between the gun barrels of the machine gun 4, a target tracking sensor 6 is arranged on the tower front, and on the tower roof is an additional, regardless of mounted to other sensors directional all-round sensor 7, the crew allows the optronische terrain monitoring using a CCD camera or thermal imaging device.

Die Maschinenwaffe 4 stellt ein erstes Wirkmittel zur Flugabwehr dar. Zur Verwirklichung eines Flugabwehr-Hybridsystems ist ein zweites Wirkmittel vorgesehen, das als Abschussvorrichtung 8 bzw. 8' für in vertikaler Richtung startende Lenkflugkörper ausgebildet ist. Die Abschussvorrichtung kann zwei Stellungen einnehmen, nämlich einmal eine Abschusstellung, in der sie vertikal ausgerichtet und in einer vorgegebenen Entfernung von der Fahrzeugwanne angeordnet ist und zum anderen eine Transportstellung, in der sie horizontal ausgerichtet und in die Fahrzeugkontur integriert ist. In den Figuren 1 bis 3 ist die Transportstellung jeweils mit Bezugsziffer 8' und in Fig. 4 die Abschussstellung jeweils mit Bezugsziffer 8 bezeichnet.The machine gun 4 represents a first means of action for air defense. To realize an anti-aircraft hybrid system, a second active means is provided, which is designed as a launching device 8 or 8 'for launching missile in the vertical direction. The launcher can take two positions, namely once a Abschusstellung in which it is vertically aligned and arranged at a predetermined distance from the vehicle pan and on the other hand, a transport position in which it is aligned horizontally and integrated into the vehicle contour. In the FIGS. 1 to 3 is the transport position with reference numeral 8 'and in Fig. 4 the firing position respectively denoted by reference numeral 8.

Im dargestellten Ausführungsbeispiel sind zwei derartige Abschussvorrichtungen 8 bzw. 8' vorhanden, die zu beiden Seiten der Fahrzeuglängsachse am Fahrzeugheck angeordnet sind. Die Integration der Abschussvorrichtungen in die Fahrzeugkontur geschieht bei dem als Kettenfahrzeug ausgebildeten Kampffahrzeug, indem die Abschussvorrichtungen 8' in der Transportstellung jeweils im Kettenkasten 1.3 parallel zur Fahrzeuglängsachse angeordnet sind.In the illustrated embodiment, two such launchers 8 and 8 'are provided, which are arranged on both sides of the vehicle longitudinal axis at the rear of the vehicle. The integration of the launcher in the vehicle contour is done in the trained as a tracked vehicle combat vehicle by the launcher 8 'are arranged in the transport position in each case in the chain case 1.3 parallel to the vehicle longitudinal axis.

Die Bewegung der Abschussvorrichtung aus der Transportstellung in die Abschusstellung geschieht in zwei Bewegungsschritten. In einem ersten Bewegungsschritt erfolgt eine Verschiebung der horizontal liegenden Abschussvorrichtung 8' in einer horizontalen Ebene senkrecht zur Fahrzeuglängsachse, bis die Abschussvorrichtung außerhalb der Fahrzeugkontur liegt. In einem zweiten Bewegungsschritt erfolgt dann eine Verschwenkung der Abschussvorrichtung aus der horizontalen in die vertikale Stellung, die mit Bezugsziffer 8 bezeichnet ist.The movement of the launcher from the transport position to the Abschusstellung done in two steps. In a first movement step, the horizontal launching device 8 'is displaced horizontally in a horizontal plane perpendicular to the vehicle longitudinal axis until the launching device lies outside the vehicle contour. In a second movement step then takes place a pivoting of the launching device from the horizontal to the vertical position, which is designated by reference numeral 8.

Um diese Bewegung zu ermöglichen, ist jeder Abschussvorrichtung eine am Heck des Kampffahrzeugs angeordnete Lager- und Antriebseinheit 9 zugeordnet. Diese dient u.a. zur Lagerung von quer über die Fahrzeugbreite reichenden linearen Führungsbahnen 9.2, an denen verschiebbare Halter geführt sind, an welchen nach außen weisende, in ihrer Längsrichtung in einer horizontalen Ebene senkrecht zur Fahrzeuglängsachse verschiebbare Tragarme 9.1 angeordnet sind. Durch in nicht eigens dargestellter Weise in den Lager- und Antriebseinheiten angeordnete elektrische Antriebsvorrichtungen können die Tragarme 9.1 nach außen verschoben werden. Am äußeren Ende der Tragarme 9.1 ist jeweils die Abschussvorrichtung 8' um eine horizontale, senkrecht zur Fahrzeuglängsachse liegende Schwenkachse schwenkbar angeordnet.In order to enable this movement, each launching device is associated with a bearing and drive unit 9 arranged at the rear of the combat vehicle. This serves u.a. for the storage of transversely across the vehicle width reaching linear guideways 9.2, on which slidable holders are guided, are arranged on which outwardly facing, in its longitudinal direction in a horizontal plane perpendicular to the vehicle longitudinal axis slidable support arms 9.1. By arranged in not specifically shown manner in the storage and drive units electrical drive devices, the support arms can be moved 9.1 to the outside. At the outer end of the support arms 9.1 each launcher 8 'is pivotally mounted about a horizontal, perpendicular to the vehicle longitudinal axis pivot axis.

Sowohl die Verschiebebewegung als auch die Schwenkbewegung der Abschussvorrichtungen werden von in den Lager- und Antriebseinheiten 9 angeordneten, nicht dargestellten elektrischen Antriebsvorrichtungen bewirkt.Both the sliding movement and the pivotal movement of the launcher are arranged by arranged in the storage and drive units 9, not shown electrical drive devices.

Im dargestellten Ausführungsbeispiel ist die Antriebsvorrichtung für die Schwenkbewegung der Abschusseinrichtung durch einen Seilzug 10 realisiert, der in den Fig. 1, 3 und 4 in seinen nach außen sichtbaren Elementen angedeutet ist. In der jeweiligen Lager- und Antriebseinheit 9 befindet sich eine von einem Antriebsmotor angetriebene, nicht dargestellte Seiltrommel, auf der das Zugseil 10 aufgewickelt wird. Das Zugseil 10 ist über Seilführungen oder -rollen zur Abschussvorrichtung 8 bzw. 8' geführt, wobei das Ende 10.1 des Zugseils 10 im Bereich des von der Schwenkachse abgewandten Endes der Abschussvorrichtung 8 bzw. 8' befestigt ist. Bei dieser Ausführung erfolgt das Herabschwenken der Abschussvorrichtung 8' unter der Wirkung des Eigengewichtes der Abschussvorrichtung, während das Heraufschwenken über das Zugseil 10 erfolgt.In the illustrated embodiment, the drive device for the pivoting movement of the Abschusseinrichtung is realized by a cable 10, which in the Fig. 1 . 3 and 4 is indicated in its visible to the outside elements. In the respective storage and drive unit 9 is a driven by a drive motor, not shown, cable drum on which the pull cable 10 is wound. The traction cable 10 is guided via cable guides or rollers to the launcher 8 or 8 ', the end 10.1 of the traction cable 10 being fastened in the region of the end of the launcher 8 or 8' facing away from the pivot axis. In this embodiment, the launcher 8 'is pivoted down under the effect of the dead weight of the launcher, while the swinging up takes place via the pull cable 10.

Die Endpositionen der Bewegungen werden durch nicht dargestellte Sperrvorrichtungen gesichert.The end positions of the movements are secured by locking devices, not shown.

Claims (10)

  1. Combat vehicle with anti-aircraft system, there being arranged on the combat vehicle (1), having a tracked running gear (1.1), a turret (3) which is pivotable in azimuth and carries an automatic weapon (4) which is pivotable in elevation and also a target designation radar apparatus (5), there being arranged at the rear of the combat vehicle a firing device (8) for guided missiles launched in the vertical direction, which is movable from a transporting position oriented horizontally and parallel to the longitudinal axis of the vehicle into a vertically oriented firing position and in the transporting position is integrated into the vehicle contour and in the firing position is arranged at a predetermined distance from the combat vehicle, characterised in that the movement of the firing device (8, 8'), which in the transporting position lies within the vehicle contour, from the transporting position into the firing position takes place in two movement steps, in a first movement step a displacement in a horizontal plane perpendicular to the longitudinal axis of the vehicle taking place until the firing device lies outside the vehicle contour, and in a second movement step a pivoting of the firing device from the horizontal into the vertical position taking place.
  2. Combat vehicle according to Claim 1, characterised in that the firing device (8') is arranged in the track guard (1.3) in the transporting position.
  3. Combat vehicle according to Claim 2, characterised by at least two firing devices (8', 8) arranged on both sides of the longitudinal axis of the vehicle.
  4. Combat vehicle according to one of Claims 1 to 3, characterised in that there is assigned to each firing device (8', 8) a supporting and driving unit (9) which is arranged at the rear of the combat vehicle (1) and has guides (9.2), in which a carrying arm (9.1) is guided in a horizontal plane perpendicular to the longitudinal axis of the vehicle and is displaceable in its longitudinal direction, and the firing device (8', 8) is arranged at the outer end of the carrying arm (9.1) in a manner pivotable about a horizontal pivot axis lying perpendicular to the longitudinal axis of the vehicle.
  5. Combat vehicle according to Claim 4, characterised in that the displacing and pivoting movements of the firing device (8', 8) are effected by electrical driving devices arranged in the supporting and driving unit (9).
  6. Combat vehicle according to Claim 5, characterised in that the driving device has a cable pull (10), a cable drum, driven by a drive motor, being arranged in the supporting and driving unit (9) and the pull cable being guided via cable guides to the firing device (8, 8'), the end (10.1) of the pull cable being fastened in the region of that end of the firing device (8, 8') remote from the pivot axis.
  7. Combat vehicle according to one of Claims 1 to 6, characterised in that the automatic weapon (4) pivotable in elevation is designed as a twin-barrel automatic weapon.
  8. Combat vehicle according to Claim 7, characterised in that the target designation radar apparatus is arranged above the twin-barrel automatic weapon (4) retractably on the rear of the turret.
  9. Combat vehicle according to Claim 7 or 8, characterised in that a target-tracking sensor (6) is arranged on the front of the turret, between the weapon barrels of the twin-barrel automatic weapon (4).
  10. Combat vehicle according to one of Claims 7 to 9, characterised in that an additionally directable panoramic sensor (7) is arranged on the top of the turret (3).
EP05849522A 2004-12-17 2005-12-12 Combat vehicle with anti-aircraft system Not-in-force EP1825211B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL05849522T PL1825211T3 (en) 2004-12-17 2005-12-12 Combat vehicle with anti-aircraft system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004060779A DE102004060779A1 (en) 2004-12-17 2004-12-17 Combat vehicle with anti-aircraft system
PCT/DE2005/002241 WO2006063570A1 (en) 2004-12-17 2005-12-12 Combat vehicle with anti-aircraft system

Publications (2)

Publication Number Publication Date
EP1825211A1 EP1825211A1 (en) 2007-08-29
EP1825211B1 true EP1825211B1 (en) 2008-07-23

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EP05849522A Not-in-force EP1825211B1 (en) 2004-12-17 2005-12-12 Combat vehicle with anti-aircraft system

Country Status (6)

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EP (1) EP1825211B1 (en)
AT (1) ATE402387T1 (en)
DE (2) DE102004060779A1 (en)
ES (1) ES2309829T3 (en)
PL (1) PL1825211T3 (en)
WO (1) WO2006063570A1 (en)

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DE102010016542C5 (en) * 2010-04-20 2017-08-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Apparatus and method for straightening a launching container

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DE10160216C1 (en) * 2001-12-07 2003-06-12 Rheinmetall Landsysteme Gmbh Independently adjustable secondary armament
DE10247350A1 (en) * 2002-10-10 2004-04-22 Krauss-Maffei Wegmann Gmbh & Co. Kg Device for protection against munitions designed as guided missiles e.g. for protection of military vehicles and buildings, has all warning sensors for detection and acquisition and active defence devices arranged on common carrier

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PL1825211T3 (en) 2009-01-30
ES2309829T3 (en) 2008-12-16
DE102004060779A1 (en) 2006-06-29
DE502005004845D1 (en) 2008-09-04
EP1825211A1 (en) 2007-08-29
WO2006063570A1 (en) 2006-06-22
ATE402387T1 (en) 2008-08-15

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