EP1549899B1 - Device for protecting objects against ammunition in the form of guided missiles - Google Patents
Device for protecting objects against ammunition in the form of guided missiles Download PDFInfo
- Publication number
- EP1549899B1 EP1549899B1 EP03773477A EP03773477A EP1549899B1 EP 1549899 B1 EP1549899 B1 EP 1549899B1 EP 03773477 A EP03773477 A EP 03773477A EP 03773477 A EP03773477 A EP 03773477A EP 1549899 B1 EP1549899 B1 EP 1549899B1
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- EP
- European Patent Office
- Prior art keywords
- active elements
- warning
- housing
- device carrier
- sensors
- Prior art date
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- Expired - Lifetime
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- 238000010304 firing Methods 0.000 claims description 10
- 238000009434 installation Methods 0.000 claims description 3
- 230000001846 repelling effect Effects 0.000 claims 2
- 238000001514 detection method Methods 0.000 abstract 1
- 239000013543 active substance Substances 0.000 description 7
- 239000003795 chemical substances by application Substances 0.000 description 3
- 230000010354 integration Effects 0.000 description 3
- 230000001419 dependent effect Effects 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005352 clarification Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
Images
Classifications
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- 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
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- 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
- F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
- F41A27/06—Mechanical systems
- F41A27/08—Bearings, e.g. trunnions; Brakes or blocking arrangements
- F41A27/14—Central-pivot bearings
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- 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
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
- F41F1/08—Multibarrel guns, e.g. twin guns
- F41F1/085—Multibarrel guns, e.g. twin guns with oscillating barrels; with barrels having variable relative orientation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
Definitions
- the invention relates to a device for protecting objects against munitions formed as steering missiles with the features of the preamble of patent claim 1.
- Suitable objects include both vehicles, in particular combat vehicles, as well as stationary facilities such as smaller buildings, portable shelters and the like. It is known to realize distance-effective protection systems by independent integration of warning sensors and active agents on the object to be protected. This leads in particular to vehicles to relatively complex retrofit solutions, since in the integration of the individual components each extensive adjustment and very precise mechanical processing must be performed on the vehicle surface.
- a device with the features of the preamble of claim 1 is in the document DE 3410467 A1 described.
- FR 2611259 A1 is a Werferiser for the protection of movable or stationary objects, in particular tanks, described with several modules, each of which consists of a base body and a plurality attached thereto, shooting cup receiving launcher tubes.
- the modules can be directed in azimuth.
- the invention has the object of providing a device of the type mentioned in such a way that an autarkic self-protection platform is created, which can be adapted to the objects and for all-round protection against trained as a steering missiles ammunition.
- a basic idea of the invention consists in arranging both the sensor system and the active means in a functionally optimized manner on a compact device carrier configured as a narrow towering unit. It has been found that in the device according to the invention the adaptation effort is low and thus a high flexibility with respect to mission-dependent use arises.
- the device it is possible to harmonize the axes of sensors and active agents, in particular the Abschuss wornen for active agents, taking into account parallax correction, attachment angle, etc. from the beginning so that a complex adjustment after the attachment of the device to the object omitted.
- the device can be designed and arranged so that a clarification of the threat and its control is possible regardless of the installation over an azimuthal angle to 360 °.
- the facility is so flexible that it can be used on combat vehicles as well as on stationary facilities.
- the interface to the intended carrier systems can be carried out uniformly, so that the "self-sufficient self-defense platform" does not have to be executed target-specific. Nevertheless, the equipment is with Sensors and active agents freely configurable.
- the device is designed to be remotely operated under armored protection.
- a unit for electronic / electro-optical active agents can be arranged on top of the equipment carrier in the area above the warning sensors.
- the arrangement in different horizontal planes ensures that sensors and active agents do not interfere.
- firing devices for firing action means approaching steering missiles can be disturbed by pyrotechnic means.
- a multispectral fog wall can be generated.
- electronic / electro-optical means of action for example, a tightly focused light beam from a uniformly operated or modulated light source, such as a laser, are emitted, through which the steering system of the steering missile is disturbed.
- the device carrier is arranged on a base plate via an articulated joint, such that at least part of the external equipment of the device can be pivoted up and down.
- FIGS. 1 to 4 show a device for protecting objects against ammunition designed as guided missiles, hereinafter referred to as "self-sufficient self-defense platform", which is arranged on the surface O of an object (not shown in detail), for example a combat vehicle. It has a device carrier 5 designed as a narrow, protruding unit, which is connected via an articulated joint 5a to a base plate 5c, which is fixedly arranged on the surface O. By means of a drive device 5b, the device carrier 5 about the axis B of the articulated joint 5a from the pivoted position shown in Fig. 1 to 3 in solid lines by 90 ° in a tilted position shown in phantom pivotally.
- a housing 6 On the equipment rack 5, a housing 6 is arranged, are integrated into the side of one to four warning sensors 1 depending on the equipment.
- a unit 2 electronic / electro-optical agent 2 On the housing 6 a unit 2 electronic / electro-optical agent 2 is rotatable about the axis A of the device carrier 5 and arranged in elevation by the angle ⁇ ⁇ pivotally by means of a directional drive 2a in azimuth direction.
- the warning sensors 1 detect a viewing angle ⁇ .
- the arrangement of the electronic / electro-optical agent 2 above the warning sensors 1 allows an unrestricted directional range of these agents 2 in azimuth. There are no fades caused by other components of the self-defense platform.
- the field of view ⁇ of the warning sensors 1 is also limited in azimuth and elevation by no other components.
- the space in the area below the warning sensors 1 is used for the installation of the units 3 with launchers 3a for firing action means, which are formed in the illustrated embodiment as a throwing cup for firing throwing bodies.
- a unit 3 with a plurality of launchers 3 a is installed on each side of the equipment carrier 5.
- the individual launcher 3a, so the dome, can be directed by means of an adjusting device 7 in elevation.
- the units 3 are azimutely directionable by means of drive devices 3b (e.g., electric locking pin mechanism with springs).
- the trackability of the launcher in azimuth and elevation is in this arrangement, i. left and right next to the equipment carrier 5, not restricted.
- the directional range of the launcher 3a in elevation is designated in FIG. 4 by ⁇ .
- the directional range of the units 3 in azimuth is denoted by ⁇ in FIG.
- the device carrier 5 is designed so that directly below the housing 6 results in an enclosed, freely available space 4. This space 4 is protected by the equipment carrier against external influences and can be used for the integration of electrical and electronic components, ie for the electronics, power distribution, position sensor, cables.
- the arrangement of all components described on the common equipment carrier 5 accounts for extensive adjustments of warning sensors 1 and 2 active agents or 3a to each other.
- the mechanical and electrical interfaces are integrated in the foot of the articulated joint 5a.
- Fig. 5 and 6 a variant of the embodiment according to FIGS. 1 to 4 is shown, which differs from this embodiment in that the base plate, which is designated in Fig. 5 with 5c ', with the surface O of the object means a straightening drive 8 is connected in azimuth directionally.
- FIGS. 5 and 6 correspond exactly to the parts of the embodiments of FIGS. 1 to 4 and are designated by the same reference numerals.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
- Elimination Of Static Electricity (AREA)
- Catching Or Destruction (AREA)
- Details Of Aerials (AREA)
- Air Bags (AREA)
Abstract
Description
Die Erfindung betrifft eine Einrichtung zum Schutz von Objekten gegen als Lenk-Flugkörper ausgebildete Munitionen mit den Merkmalen aus dem Oberbegriff des Patentanspruchs 1.The invention relates to a device for protecting objects against munitions formed as steering missiles with the features of the preamble of
Als Objekte kommen dabei sowohl Fahrzeuge, insbesondere Kampffahrzeuge, als auch stationäre Einrichtungen wie kleinere Gebäude, transportable Shelter und dergleichen in Betracht. Es ist bekannt, abstandswirksame Schutzsysteme durch unabhängige Integration von Warn-Sensoren und Wirkmitteln auf dem zu schützenden Objekt zu realisieren. Dies führt insbesondere bei Fahrzeugen zu relativ aufwändigen Nachrüstlösungen, da bei der Integration der Einzelkomponenten jeweils umfangreiche Justierarbeiten und sehr präzise mechanische Bearbeitungen auf der Fahrzeugoberfläche durchgeführt werden müssen.Suitable objects include both vehicles, in particular combat vehicles, as well as stationary facilities such as smaller buildings, portable shelters and the like. It is known to realize distance-effective protection systems by independent integration of warning sensors and active agents on the object to be protected. This leads in particular to vehicles to relatively complex retrofit solutions, since in the integration of the individual components each extensive adjustment and very precise mechanical processing must be performed on the vehicle surface.
Eine Einrichtung mit den Merkmalen aus dem Oberbegriff des Patentanspruchs 1 ist in dem Dokument
Es handelt sich dort um eine mehrrohrige Waffenanlage, die auf dem Turm eines Kampfpanzers montiert oder montierbar ist. Sie umfasst auf einem Kreisumfang gleichmäßig verteilt angeordnete Rohre, die in unterschiedlicher Elevation starr auf einer von der Drehbewegung des Turms unabhängig drehbaren Waffenplattform angeordnet sind. Aus den Rohren können zielsuchende Flugkörper abgefeuert werden. Die Rohre sind im Bereich unterhalb eines auf der Waffenplattform montierten Radargerätes angeordnet.It is a multi-tube weapon system that can be mounted or mounted on the turret of a main battle tank. It comprises on a circumference evenly distributed arranged tubes which are arranged in different elevations rigidly mounted on a rotating independently of the rotation of the tower weapon platform. From the pipes, homing missiles can be fired. The tubes are located in the area below a mounted on the weapon platform radar device.
In dem Dokument
Der Erfindung liegt die Aufgabe zugrunde, eine Einrichtung der eingangs erwähnten Art so auszugestalten, dass eine autarke Selbstschutz-Plattform entsteht, die auf den Objekten adaptiert werden kann und zum Rundumschutz gegen als Lenk-Flugkörper ausgebildete Munitionen dient.The invention has the object of providing a device of the type mentioned in such a way that an autarkic self-protection platform is created, which can be adapted to the objects and for all-round protection against trained as a steering missiles ammunition.
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 of this object is achieved according to the invention with the features of the characterizing part of
Ein Grundgedanke der Erfindung besteht darin, sowohl die Sensorik als auch die Wirkmittel funktionsoptimiert auf einer als schmal aufragende Einheit ausgebildeten kompakten Geräteträger anzuordnen. Es hat sich gezeigt, dass bei der erfindungsgemäßen Einrichtung der Adaptionsaufwand gering ist und somit eine hohe Flexibilität in bezug auf missionsabhängigen Einsatz entsteht.A basic idea of the invention consists in arranging both the sensor system and the active means in a functionally optimized manner on a compact device carrier configured as a narrow towering unit. It has been found that in the device according to the invention the adaptation effort is low and thus a high flexibility with respect to mission-dependent use arises.
Bei der erfindungsgemäßen Einrichtung ist es möglich, die Achsen von Sensoren und Wirkmitteln, insbesondere der Abschusseinrichtungen für Wirkmittel, unter Berücksichtigung von Parallaxenkorrektur, Aufsatzwinkel etc. von Anfang an so zu harmonisieren, dass eine aufwändige Justierung nach dem Anbau der Einrichtung an das Objekt entfällt. Die Einrichtung kann so ausgebildet und angeordnet werden, dass eine Aufklärung der Bedrohung und deren Bekämpfung unabhängig vom Einbauort über einen azimutalen Winkel bis 360° ermöglicht wird. Die Einrichtung ist so flexibel gestaltet, dass sie sowohl auf Kampffahrzeugen als auch auf stationären Einrichtungen eingesetzt werden kann. Die Schnittstelle zu den vorgesehenen Trägersystemen kann einheitlich ausgeführt werden, so dass die "autarke Selbstschutz-Plattform" nicht zielsystemspezifisch ausgeführt werden muss. Dennoch ist die Ausstattung mit Sensoren und Wirkmitteln frei konfigurierbar. Die Einrichtung ist so konzipiert, dass sie unter Panzerschutz fernbedient werden kann.In the device according to the invention, it is possible to harmonize the axes of sensors and active agents, in particular the Abschusseinrichtungen for active agents, taking into account parallax correction, attachment angle, etc. from the beginning so that a complex adjustment after the attachment of the device to the object omitted. The device can be designed and arranged so that a clarification of the threat and its control is possible regardless of the installation over an azimuthal angle to 360 °. The facility is so flexible that it can be used on combat vehicles as well as on stationary facilities. The interface to the intended carrier systems can be carried out uniformly, so that the "self-sufficient self-defense platform" does not have to be executed target-specific. Nevertheless, the equipment is with Sensors and active agents freely configurable. The device is designed to be remotely operated under armored protection.
Oben auf dem Geräteträger im Bereich oberhalb der Warn-Sensoren kann eine Einheit für elektronische/elektrooptische Wirkmittel angeordnet sein. Durch die Anordnung in verschiedenen horizontalen Ebenen wird erreicht, dass sich Sensoren und Wirkmittel nicht stören. Durch die Abschussvorrichtungen für abschießbare Wirkmittel können anfliegende Lenk-Flugkörper mit pyrotechnischen Mitteln gestört werden. So kann beispielsweise eine multispektrale Nebelwand erzeugt werden. Durch elektronische/elektrooptische Wirkmittel kann beispielsweise ein enggebündelter Lichtstrahl von einer gleichmäßig betriebenen oder modulierten Lichtquelle, beispielsweise einem Laser, ausgesendet werden, durch die das Lenksystem des Lenk-Flugkörpers gestört wird.A unit for electronic / electro-optical active agents can be arranged on top of the equipment carrier in the area above the warning sensors. The arrangement in different horizontal planes ensures that sensors and active agents do not interfere. By firing devices for firing action means approaching steering missiles can be disturbed by pyrotechnic means. For example, a multispectral fog wall can be generated. By electronic / electro-optical means of action, for example, a tightly focused light beam from a uniformly operated or modulated light source, such as a laser, are emitted, through which the steering system of the steering missile is disturbed.
Bei der erfindungsgemäßen Einrichtung, ist der Geräteträger über ein Knickgelenk auf einer Grundplatte angeordnet, derart, dass mindestens ein Teil der außenwirksamen Ausstattung der Einrichtung auf und ab geschwenkt werden kann.In the device according to the invention, the device carrier is arranged on a base plate via an articulated joint, such that at least part of the external equipment of the device can be pivoted up and down.
Durch das Aufschwenken erhält man unterschiedliche Höhenniveaus im operationellen Betrieb für Ausblick- und Wirkungsachsen, wodurch eine gegenseitige Beeinflussung der Baugruppen der "autarken Selbstschutz-Plattform" selbst über den gesamten azimutalen Bereich von 360° ausgeschlossen wird.By pivoting, different levels of elevation are obtained in operational mode for outlook and action axes, thereby precluding interference between the assemblies of the "self-sustaining self-defense platform" even over the entire azimuthal range of 360 °.
In der abgeschwenkten Position erhält man eine relativ kompakte, niedrigbauende Einheit. Dies ist besonders wichtig beim Transport von Kampffahrzeugen mit montierter "autarker Selbstschutz-Plattform" zur Sicherstellung der Einhaltung des Lademaßes.In the pivoted position to obtain a relatively compact, low-building unit. This is particularly important in the transport of combat vehicles with mounted "self-sufficient self-defense platform" to ensure compliance with the load gauge.
Im Folgenden wird anhand der beigefügten Zeichnungen ein Ausführungsbeispiel für eine Einrichtung nach der Erfindung näher erläutert.In the following an embodiment of a device according to the invention will be explained in more detail with reference to the accompanying drawings.
In den Zeichnungen zeigen:
- Fig. 1
- in einer Seitenansicht eine autarke Selbstschutz-Plattform nach der Erfindung;
- Fig. 2
- die Selbstschutz-Plattform nach Fig. 1 in einer teilweise geschnittenen Vorderansicht;
- Fig. 3
- die Selbstschutz-Plattform nach Fig. 1 und 2 in einer Draufsicht;
- Fig. 4
- den Bereich X aus Fig. 1 in einer Teilschnittdarstellung;
- Fig. 5
- in einer Darstellung analog Fig. 2 eine Variante der Ausführungsform nach Fig. 1 bis 4;
- Fig. 6
- einen Teilschnitt durch die Ausführungsform nach Fig. 5 nach der Linie VI-VI in Fig. 5.
- Fig. 1
- in a side view of a self-sufficient self-protection platform according to the invention;
- Fig. 2
- the self-protection platform of Figure 1 in a partially sectioned front view.
- Fig. 3
- the self-protection platform of Figure 1 and 2 in a plan view.
- Fig. 4
- the region X of Figure 1 in a partial sectional view.
- Fig. 5
- in a representation analogous to Figure 2 is a variant of the embodiment of Figures 1 to 4 ..;
- Fig. 6
- a partial section through the embodiment of FIG. 5 along the line VI-VI in Fig. 5th
In den Fig. 1 bis 4 ist eine Einrichtung zum Schutz von Objekten gegen als Lenkflugkörper ausgebildete Munitionen, im Folgenden "autarke Selbstschutz-Plattform" genannt, dargestellt, die auf der Oberfläche O eines nicht näher dargestellten Objektes, beispielsweise eines Kampffahrzeugs, angeordnet ist. Sie besitzt einen als schmal auf- ragende Einheit ausgebildeten Geräteträger 5, der über ein Knickgelenk 5a mit einer Grundplatte 5c verbunden ist, die fest auf der Oberfläche O angeordnet ist. Mittels einer Antriebsvorrichtung 5b ist der Geräteträger 5 um die Achse B des Knickgelenks 5a aus der in den Fig. 1 bis 3 mit ausgezogenen Linien dargestellten aufgeschwenkten Position um 90° in eine gestrichelt dargestellte abgeschwenkte Position schwenkbar. Auf dem Geräteträger 5 ist ein Gehäuse 6 angeordnet, in das seitlich je nach Ausstattung einer bis vier Warn-Sensoren 1 integriert sind. Auf dem Gehäuse 6 ist mittels eines Richtantriebs 2a in Azimut richtbar eine Einheit 2 elektronischer/elektrooptischer Wirkmittel 2 um die Achse A des Geräteträgers 5 drehbar und in Elevation um den Winkel ± δ schwenkbar angeordnet. Die Warn-Sensoren 1 erfassen einen Ausblickwinkel α. Es entsteht somit auf dem Geräteträger 5 eine kompakte Einheit aus Warn-Sensoren 1 und elektronischen/elektro-optischen Wirkmitteln 2, die in dem Gehäuse 6 zusammengefasst wird.FIGS. 1 to 4 show a device for protecting objects against ammunition designed as guided missiles, hereinafter referred to as "self-sufficient self-defense platform", which is arranged on the surface O of an object (not shown in detail), for example a combat vehicle. It has a device carrier 5 designed as a narrow, protruding unit, which is connected via an articulated
Die Anordnung der elektronischen/elektrooptischen Wirkmittel 2 oberhalb der Warn-Sensoren 1 ermöglicht einen uneingeschränkten Richtbereich dieser Wirkmittel 2 in Azimut. Es finden keine Ausblendungen durch andere Komponenten der Selbstschutz-Plattform statt.The arrangement of the electronic / electro-
Auch das Blickfeld α der Warn-Sensoren 1 wird in Azimut und Elevation durch keine anderen Komponenten eingeschränkt.The field of view α of the
Der Platz im Bereich unterhalb der Warn-Sensoren 1 wird für den Einbau der Einheiten 3 mit Abschussvorrichtungen 3a für abschießbare Wirkmittel genutzt, die im dargestellten Ausführungsbeispiel als Wurfbecher zum Abschießen von Wurfkörpern ausgebildet sind. Im dargestellten Ausführungsbeispiel ist zu beiden Seiten des Geräteträgers 5 je eine Einheit 3 mit mehreren Abschussvorrichtungen 3a installiert. Die einzelnen Abschussvorrichtungen 3a, also die Wurfbecher, können mittels einer Stelleinrichtung 7 in Elevation gerichtet werden. Die Einheiten 3 sind mittels Antriebsvorrichtungen 3b (z.B. elektrische Sperrbolzenmechanik mit Federn) in Azimut richtbar. Die Richtbarkeit der Abschussvorrichtungen in Azimut und Elevation ist bei dieser Anordnung, d.h. links und rechts neben dem Geräteträger 5, nicht eingeschränkt. Der Richtbereich der Abschussvorrichtungen 3a in Elevation ist in Fig. 4 mit γ bezeichnet. Der Richtbereich der Einheiten 3 in Azimut ist in Fig. 3 mit β bezeichnet.The space in the area below the
Der Geräteträger 5 ist so ausgestaltet, dass sich direkt unterhalb des Gehäuses 6 ein umschlossener, frei verfügbarer Bauraum 4 ergibt. Dieser Bauraum 4 ist durch den Geräteträger gegen äußere Einwirkungen geschützt und kann für die Integration von elektrischen und elektronischen Bauelementen, also für die Elektronik, Energieverteiler, Lagesensor, Kabel usw. genutzt werden.The device carrier 5 is designed so that directly below the
Durch die Anordnung aller beschriebenen Komponenten auf dem gemeinsamen Geräteträger 5 entfallen umfangreiche Justierarbeiten von Warn-Sensoren 1 und Wirkmitteln 2 bzw. 3a zueinander.The arrangement of all components described on the common equipment carrier 5 accounts for extensive adjustments of
Bei der Adaption der autarken Selbstschutz-Plattform auf Fahrzeugen ermöglicht die um die Achse B des Knickgelenks 5a abgeschwenkte Position des Geräteträgers 5 die Einhaltung von Verlademaßen. Die Funktionsfähigkeit der richtbaren Einheiten 3 für die Abschussvorrichtungen 3a, die derart angeordnet sind, dass sie das Einklappen des Geräteträgers 5 nicht behindern, bleibt auch bei eingeklappter Stellung des Geräteträgers 5 erhalten.When adapting the autarkic self-protection platform on vehicles pivoted about the axis B of the articulated joint 5a position of the equipment carrier 5 allows compliance with Verlademaßen. The functionality of the directional units 3 for the
Im Fuß des Knickgelenks 5a sind die mechanischen und elektrischen Schnittstellen integriert.The mechanical and electrical interfaces are integrated in the foot of the articulated joint 5a.
In Fig. 5 und 6 ist eine Variante der Ausführungsform nach den Fig. 1 bis 4 dargestellt, die sich von dieser Ausführungsform dadurch unterscheidet, dass die Grundplatte, die in Fig. 5 mit 5c' bezeichnet ist, mit der Oberfläche O des Objekts mittels eines Richtantriebs 8 in Azimut richtbar verbunden ist.In Fig. 5 and 6 a variant of the embodiment according to FIGS. 1 to 4 is shown, which differs from this embodiment in that the base plate, which is designated in Fig. 5 with 5c ', with the surface O of the object means a straightening
Die übrigen Teile der Ausführungsform nach Fig. 5 und 6 entsprechen genau den Teilen der Ausführungsformen nach Fig. 1 bis 4 und sind mit den gleichen Bezugsziffern bezeichnet. Bei der Ausführungsform nach Fig. 5 und 6 ist es möglich, die gesamte Selbstschutz-Plattform in Richtung der erwarteten Hauptbedrohung zu richten. Dies ist dann erforderlich, wenn infolge einer Teilausstattung mit Warn-Sensoren 1 nicht der volle Bereich in Azimut sensiert werden kann.The remaining parts of the embodiment of FIGS. 5 and 6 correspond exactly to the parts of the embodiments of FIGS. 1 to 4 and are designated by the same reference numerals. In the embodiment of Figures 5 and 6, it is possible to direct the entire self-protection platform towards the expected major threat. This is necessary if, due to a partial equipment with
Claims (7)
- Device for protecting objects against ammunition in the form of guided missiles, comprising warning sensors (1) for detecting an incoming guided missile and active elements (2, 3a) for repelling the guided missile, in which all warning sensors (1) required for detecting and all active elements (2, 3a) required for repelling are arranged on a common device carrier (5) which is arranged on the object (O) that is to be protected, or can be mounted thereon, wherein at least one warning sensor (1) is arranged on the device carrier (5) and in the region below the warning sensor or warning sensors (1), firing devices (3a) for active elements that can be fired are arranged in such a way that the field of viewing of the warning sensor or warning sensors (1) is not limited in azimuth and elevation, characterised in that the device carrier (5) is constructed as a narrow, upwardly directed unit on which a housing (6) is mounted, wherein the warning sensors (1) are integrated in the sides of the housing (6) and in the upper part of the device carrier (5) below the housing (6) is arranged an installation space (4) for receiving electrical and electronic components and on both sides of the lower part of the device carrier (5) the units (3) with the firing devices (3a) for active elements that can be fired are arranged which are adjustable at least in elevation, and in that the device carrier (5) is arranged on a base plate (5c) via a universal joint (5a), on the base plate in the direction of axis (B) of the universal joint (5a), the units (3) having the firing devices (3a) for active elements that can be fired are arranged in such a way that the device carrier (5), together with the housing (6) and the warning sensors (1) are tiltable, via a drive mechanism (5d), out of the upright position, about 90°, into a pivoted-out position.
- Device according to claim 1, characterised in that the firing devices (3a) for active elements that can be fired are embodied as launchers for firing projectiles.
- Device according to claim 1 or 2, characterised in that respective units (3) comprising a plurality of firing devices (3a) for active elements that can be fired are arranged on a plurality of sides of the device carrier (5)
- Device according to any one of claims 1 to 3, characterised in that a unit (2) of electronic/electro-optical active elements that is adjustable at least in azimuth is arranged on the device carrier (5) in a region above the warning sensor or warning sensors (1).
- Device according to claim 4, characterised in that the unit (2) of electronic/electro-optical active elements is arranged above the housing (6), the housing containing a directional drive (2a) for this unit (2) and together with the housing (6) can be tilted into the pivoted-out position.
- Device according to any one of claims 1 to 5, characterised in that mechanical and electrical interfaces are integrated into a base of the universal joint (5a).
- Device according to any one of claims 1 to 6, characterised in that the base plate (5c') is connected to the object (0) via a directional drive (8) so as to be adjustable in azimuth.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10247350A DE10247350A1 (en) | 2002-10-10 | 2002-10-10 | 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 |
| DE10247350 | 2002-10-10 | ||
| PCT/DE2003/003271 WO2004036138A1 (en) | 2002-10-10 | 2003-10-01 | Device for protecting objects against ammunition in the form of guided missiles |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1549899A1 EP1549899A1 (en) | 2005-07-06 |
| EP1549899B1 true EP1549899B1 (en) | 2007-09-05 |
Family
ID=32038480
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03773477A Expired - Lifetime EP1549899B1 (en) | 2002-10-10 | 2003-10-01 | Device for protecting objects against ammunition in the form of guided missiles |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US20050285771A1 (en) |
| EP (1) | EP1549899B1 (en) |
| AT (1) | ATE372497T1 (en) |
| CA (1) | CA2501374A1 (en) |
| DE (2) | DE10247350A1 (en) |
| ES (1) | ES2291706T3 (en) |
| IL (1) | IL167846A (en) |
| NO (1) | NO330449B1 (en) |
| WO (1) | WO2004036138A1 (en) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1605225A1 (en) * | 2004-06-07 | 2005-12-14 | Honeywell Aerospatiale Inc. | Active armour protection system for armoured vehicles |
| DE102004060779A1 (en) * | 2004-12-17 | 2006-06-29 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Combat vehicle with anti-aircraft system |
| FR2884601B1 (en) * | 2005-04-19 | 2010-10-29 | Giat Ind Sa | COMPACT WEAPON MOUNTING |
| IL173221A0 (en) * | 2006-01-18 | 2007-07-04 | Rafael Advanced Defense Sys | Devics |
| DE102007018507B4 (en) * | 2007-04-19 | 2012-05-03 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method and apparatus for controlling an assault ammunition launcher |
| DE102008038603C5 (en) | 2008-08-21 | 2018-04-19 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Gegenschuss conditioning |
| FR2935789B1 (en) * | 2008-09-11 | 2010-09-10 | Nexter Systems | RETRACTABLE TURRET |
| US8146479B2 (en) | 2009-09-10 | 2012-04-03 | Nexter Systems | Retractable light turret |
| FR2950962B1 (en) * | 2009-10-01 | 2011-10-14 | Nexter Systems | TURRET FOR MOUNTING AN EQUIPMENT, SUCH AS A SECONDARY ARMOR |
| DE102010025801A1 (en) * | 2010-07-01 | 2012-01-05 | Diehl Bgt Defence Gmbh & Co. Kg | Active defense system for light combat vehicles |
| DE102012002043C5 (en) * | 2012-02-02 | 2016-05-12 | Diehl Bgt Defence Gmbh & Co. Kg | Weapon-based protection device for vehicles |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2968997A (en) * | 1947-05-09 | 1961-01-24 | Sperry Rand Corp | Cross connected servo mechanism for a turret gun directing system |
| US3102451A (en) * | 1955-07-29 | 1963-09-03 | Ernest F Campbell | Weapon mount |
| US3019711A (en) * | 1956-12-26 | 1962-02-06 | Figure | |
| CH552784A (en) * | 1972-12-04 | 1974-08-15 | Contraves Ag | FLAB COMBAT VEHICLE. |
| US4020407A (en) * | 1973-03-02 | 1977-04-26 | Etat Francais | Control system for tracking a moving target |
| DE2336040C3 (en) * | 1973-07-14 | 1980-06-19 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Defense system with several floors |
| DE2411790C3 (en) * | 1974-03-12 | 1978-06-29 | Precitronic Gesellschaft Fuer Feinmechanik Und Electronic Mbh, 2000 Hamburg | Method and weapon system for combating surface targets |
| DE2750776C3 (en) * | 1977-11-14 | 1980-06-04 | Precitronic Gesellschaft Fuer Feinmechanik Und Electronic Mbh, 2000 Hamburg | Azimuthally directional launcher |
| US4302666A (en) * | 1979-11-13 | 1981-11-24 | The Boeing Company | Position control system of the discontinuous feedback type |
| NL8204706A (en) * | 1982-12-06 | 1984-07-02 | Hollandse Signaalapparaten Bv | INTEGRATED WEAPON FIRE CONTROL SYSTEM. |
| NL8300178A (en) * | 1983-01-18 | 1984-08-16 | Hollandse Signaalapparaten Bv | PULSE RADAR DEVICE. |
| DE3410467A1 (en) * | 1984-03-22 | 1985-09-26 | Rheinmetall GmbH, 4000 Düsseldorf | Multi-barrel weapon system |
| SE459993B (en) * | 1985-01-25 | 1989-08-28 | Philips Norden Ab | DEVICE FOR POWER SUPPLY BY A CANON INCLUDING A FOLLOWING UNIT WITH RADAR TRANSMITTER / RECEIVER AND ANTENNA ORGAN |
| DE3705700A1 (en) * | 1987-02-23 | 1988-09-01 | Buck Chem Tech Werke | Launcher unit |
| FR2711806B1 (en) * | 1990-07-23 | 1995-12-29 | Aerospatiale | Detection and response system to an air threat. |
| JPH0772680B2 (en) * | 1992-02-05 | 1995-08-02 | 防衛庁技術研究本部長 | Proximity protection device |
| IL107707A (en) * | 1993-11-22 | 1997-01-10 | Israel State | Means for upgrading existing missile control systems |
| DE4426014B4 (en) * | 1994-07-22 | 2004-09-30 | Diehl Stiftung & Co.Kg | System for protecting a target against missiles |
| FR2751761B1 (en) * | 1996-07-24 | 1998-10-23 | Sfim Ind | OBSERVATION OR FOCUSING SYSTEM |
| FR2780774B1 (en) * | 1998-07-03 | 2001-03-09 | Alkan Sa | PASSIVE SELF-PROTECTION DEVICE FOR MOBILE MACHINE SUCH AS A HELICOPTER |
| DE29922470U1 (en) * | 1999-12-22 | 2001-05-03 | Krauss Maffei Wegmann Gmbh & C | Military system module, in particular air defense system module |
| DE10024320C2 (en) * | 2000-05-17 | 2002-09-05 | Diehl Munitionssysteme Gmbh | Radar device for object self-protection |
| DE10050479A1 (en) * | 2000-10-12 | 2002-04-18 | Bodenseewerk Geraetetech | System used for protecting objects, especially combat tanks, comprises an image-producing infra-red sensor attached to a missile launching device |
| DE10117007A1 (en) * | 2001-04-04 | 2002-10-17 | Buck Neue Technologien Gmbh | Method and device for protecting mobile military equipment |
-
2002
- 2002-10-10 DE DE10247350A patent/DE10247350A1/en not_active Withdrawn
-
2003
- 2003-10-01 CA CA002501374A patent/CA2501374A1/en not_active Abandoned
- 2003-10-01 US US10/530,940 patent/US20050285771A1/en not_active Abandoned
- 2003-10-01 ES ES03773477T patent/ES2291706T3/en not_active Expired - Lifetime
- 2003-10-01 WO PCT/DE2003/003271 patent/WO2004036138A1/en active IP Right Grant
- 2003-10-01 AT AT03773477T patent/ATE372497T1/en not_active IP Right Cessation
- 2003-10-01 DE DE50308132T patent/DE50308132D1/en not_active Expired - Lifetime
- 2003-10-01 EP EP03773477A patent/EP1549899B1/en not_active Expired - Lifetime
-
2005
- 2005-04-04 IL IL167846A patent/IL167846A/en active IP Right Grant
- 2005-05-09 NO NO20052256A patent/NO330449B1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| NO330449B1 (en) | 2011-04-18 |
| CA2501374A1 (en) | 2004-04-29 |
| ES2291706T3 (en) | 2008-03-01 |
| US20050285771A1 (en) | 2005-12-29 |
| ATE372497T1 (en) | 2007-09-15 |
| IL167846A (en) | 2010-04-15 |
| EP1549899A1 (en) | 2005-07-06 |
| WO2004036138A1 (en) | 2004-04-29 |
| DE50308132D1 (en) | 2007-10-18 |
| DE10247350A1 (en) | 2004-04-22 |
| NO20052256L (en) | 2005-05-09 |
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