EP1717541B2 - Launcher - Google Patents

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Publication number
EP1717541B2
EP1717541B2 EP06006342.7A EP06006342A EP1717541B2 EP 1717541 B2 EP1717541 B2 EP 1717541B2 EP 06006342 A EP06006342 A EP 06006342A EP 1717541 B2 EP1717541 B2 EP 1717541B2
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EP
European Patent Office
Prior art keywords
firing
launcher
drum
launcher according
abovementioned
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
EP06006342.7A
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German (de)
French (fr)
Other versions
EP1717541A1 (en
EP1717541B1 (en
Inventor
Berthold Dr. Baumann
Norbert Kohnen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Waffe Munition GmbH
Original Assignee
Rheinmetall Waffe Munition GmbH
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A9/00Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/61Magazines
    • F41A9/64Magazines for unbelted ammunition
    • F41A9/73Drum magazines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A9/00Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/01Feeding of unbelted ammunition
    • F41A9/24Feeding of unbelted ammunition using a movable magazine or clip as feeding element
    • F41A9/26Feeding of unbelted ammunition using a movable magazine or clip as feeding element using a revolving drum magazine
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A9/00Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/01Feeding of unbelted ammunition
    • F41A9/24Feeding of unbelted ammunition using a movable magazine or clip as feeding element
    • F41A9/26Feeding of unbelted ammunition using a movable magazine or clip as feeding element using a revolving drum magazine
    • F41A9/27Feeding of unbelted ammunition using a movable magazine or clip as feeding element using a revolving drum magazine in revolver-type guns
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41CSMALLARMS, e.g. PISTOLS, RIFLES; ACCESSORIES THEREFOR
    • F41C3/00Pistols, e.g. revolvers
    • F41C3/02Signal pistols, e.g. Very pistols
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/145Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances
    • F42B5/15Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances for creating a screening or decoy effect, e.g. using radar chaff or infrared material
    • F42B5/155Smoke-pot projectors, e.g. arranged on vehicles

Definitions

  • Throwing equipment in particular launcher, used for launching active bodies or active media, such as fog, explosive, noise and / or decoy and tear gas, pepper or the like. Throwing systems are usually mounted or used on vehicles such as land vehicles and ships and on buildings. Such litter cups with active body are in the DE 37 06 213 C2 disclosed. Magazine-like Nebelschitzanlagen are for example in the DE 43 38 650 C1 as well as the DE 100 08 198 A1 described. As a rule, the throwing cups are arranged side by side or one above the other and have only a small straightening possibility,
  • the US 4,112,818 describes a surveillance and weapon system for protection in an aircraft.
  • a weapon integrated in this system is designed as a drum weapon, whereby the drum is rotatable about its own axis. Shots are fired whenever the drum pins come into contact with the pins on the triggers as the drum rotates. A contact separation to continue to rotate the drum without a shot is not provided. Rather, with each rotation of the shot fired until no more shot is in the drum.
  • the weapon is mounted below the aircraft roof and can be pivoted in two directions, horizontal and vertical. The pivoting in height is structurally limited.
  • This unit consists of several modules, which consists of a main body and several attached launching tubes.
  • the modules are rotated by a drive motor around the shaft longitudinal axis, wherein the drive motor and the ignition systems are controlled by a microprocessor. This ensures that different modules can shoot in the same direction. It is not possible to judge unity as a whole.
  • US 5,415,152 describes a pressure-driven throwing unit, wherein the launching tube is brought into alignment with the compressed gas from which the projectile is to be fired.
  • the invention has as its object to show a throwing system, which preferably allows a Richtfflegzier in at least one straightening axis.
  • the invention is based on the idea of arranging the launching tubes for the projectiles in a circle around an axis of rotation. This results in a Abschusstrommel that rotatably makes it possible to fire the or the projectile from a certain position.
  • the firing direction can be determined rigidly or adjusted by straightening the drum. That is, in a preferred embodiment, the thrower has a straightening at least in a straightening axis.
  • a straightening in two to three axes is provided.
  • the launching is ideally done from the launch tube whose axis is cut from both the elevation directional axis and the azimuth directional axis. As a result, no torques are generated around the straightening during firing.
  • brakes and clutches can be omitted on the drives of the directional axis or adjustable lever supports.
  • the straightening drives can be made small.
  • the control of the throwing machine can be simplified.
  • the launcher components can be made symmetrical and small.
  • the Werfertrommel can be designed as a removable magazine. This has the advantage that completely ammunitioniere magazines can be changed.
  • a drum / magazine drive allows rotation to an index position for loading / unloading the launcher.
  • the contacts for firing are separated to create a high level of security in this position.
  • the firing in only one position has the advantage that the introduction of force and torque into the carrier vehicle can be optimized.
  • the launcher can also be attached to buildings etc.
  • a brake and reset system can be integrated in the launching position in continuation of the invention.
  • This allows the use of light carrier vehicles, such as the use of SUVs, motorcycles, helicopters, light aircraft and the like and, for example, as a mobile, portable systems.
  • Fig. 1 is a launcher 1 with several launch tubes 2, in which there are not shown here throwing body 3, shown.
  • the launch tubes 2 in their entirety form a Abschusstrommel or a drum magazine 4, which in azimuth A about a straightening axis R 1 by means of a drive 5 and elevation E about a straightening axis R 2 by means of another drive 6 (Fig. Fig. 3 ) is pivotable.
  • a video camera is provided.
  • the drum 4 itself is adjustable about its own drum axis / axis of rotation D (drive 13).
  • Figure 4 and stored in or on a carrier 8.
  • the litter installation 1 can be adapted to a carrier vehicle (not shown in more detail) by means of a bracket 9 adapted to the respective mounting situation and position.
  • Fig. 2 shows the throwing machine 1 with the launching tubes 2 and throwing bodies 3 in a front view.
  • Fig. 3 gives a side view of the throwing machine 1
  • Fig. 4 a sectional view of the throwing machine 1 in section AA Fig. 2 ,
  • the drum 4 is rotated about its axis D.
  • the throwing body 3 1 is in the firing position, d, h., From the launch tube 2, whose axis is cut both from the straightening axis R 2 for the elevation E and from the straightening axis R 1 for azimuth A. If this projectile has been ignited 3 1 , there is a further adjustment of the drum 4 until another projectile 3 is in the launching position. After firing all located in the launch tubes 2 throwing body 3, the magazine 4 can be changed. For straightening the discharge tubes 2, the drum 4 is adjusted in its entirety in azimuth and / or elevation. If a safety position is desired, the drum 4 is adjusted so that no throwing body 3 comes into contact (contacts 10 and 11 also separated from each other electrically).
  • the contacts 10, 11 ( Fig. 3 . 3a ) are used to power the throwing machine 1 and to transmit the firing signal. It is ensured that in the firing position only the projectile located in this position 3 is ignited.
  • an ammunition detection device 12 (FIG. Fig. 3 ).

Abstract

A throwing unit (1) for projectiles (3) comprises a tube (2) arranged around a rotational axis, and a firing drum which contains the projectiles. Only the projectiles are ignited, and the drum can be moved about the rotational axis using a drive. The drum and the throwing unit are in contact when in the firing position.

Description

Wurfanlagen, insbesondere Werfer, dienen zum Abschuss von Wirkkörpern bzw. Wirkmedien, wie beispielsweise Nebel-, Spreng-, Stör- und / oder Täuschkörper sowie Tränengas, Pfeffer oder dergleichen. Wurfanlagen werden in der Regel an Fahrzeugen wie Landfahrzeuge und Schiffe und an Gebäuden angebracht bzw. eingesetzt. Derartige Wurfbecher mit Wirkkörper sind in der DE 37 06 213 C2 offenbart. Magazinartige Nebelwurfanlagen sind beispielsweise in der DE 43 38 650C1 sowie der DE 100 08 198 A1 beschrieben. In der Regel sind die Wurfbecher nebeneinander oder übereinander angeordnet und besitzen nur eine geringe Richtmöglichkeit,Throwing equipment, in particular launcher, used for launching active bodies or active media, such as fog, explosive, noise and / or decoy and tear gas, pepper or the like. Throwing systems are usually mounted or used on vehicles such as land vehicles and ships and on buildings. Such litter cups with active body are in the DE 37 06 213 C2 disclosed. Magazine-like Nebelwurfanlagen are for example in the DE 43 38 650 C1 as well as the DE 100 08 198 A1 described. As a rule, the throwing cups are arranged side by side or one above the other and have only a small straightening possibility,

In der DE 101 11 714 C1 wird erwähnt, dass derartige Effektmunition meistens aus Kurzlaufwaffen bzw. aus kurzen Trommelmagazinen verschossen wird, wobei ausgeführt wird, dass in diesen Fällen das Magazin dann üblicherweise durch eine Scheibe abgedeckt ist. Weitere Ausführungen über die Trommel selbst werden nicht gemacht.In the DE 101 11 714 C1 It is mentioned that such effect ammunition is usually fired from short-barreled weapons or from short drum magazines, wherein it is stated that in these cases the magazine is then usually covered by a disk. Further details about the drum itself are not made.

Die US 4,112,818 beschreibt ein Überwachungs- und Waffensystem zum Schutz in einem Flugzeug. Eine in dieses System integrierte Waffe ist als Trommelwaffe ausgeführt, wobei die Trommel um die eigene Achse drehbar ist. Es werden immer dann Schüsse ausgelöst, wenn beim Drehen der Trommel die Pins der Trommel mit den Pins der Auslöser in Kontakt kommen. Eine Kontaktrennung, um die Trommel ohne Schuss weiter zu drehen, ist nicht vorgesehen. Vielmehr wird mit jeder Drehung der Schuss ausgelöst, bis kein Schuss mehr in der Trommel vorhanden ist. Die Waffe ist unterhalb des Flugzeugdaches angebracht und kann in zwei Richtungen verschwenkt werden, horizontal und vertikal. Das Verschwenken in der Höhe ist baulich begrenzt.The US 4,112,818 describes a surveillance and weapon system for protection in an aircraft. A weapon integrated in this system is designed as a drum weapon, whereby the drum is rotatable about its own axis. Shots are fired whenever the drum pins come into contact with the pins on the triggers as the drum rotates. A contact separation to continue to rotate the drum without a shot is not provided. Rather, with each rotation of the shot fired until no more shot is in the drum. The weapon is mounted below the aircraft roof and can be pivoted in two directions, horizontal and vertical. The pivoting in height is structurally limited.

Mit der DE 37 05 700 A1 wird eine Werfereinheit zum Schutz von beweglichen oder stationären Objekten offenbart. Diese Einheit besteht aus mehreren Modulen, welche aus einem Grundkörper und mehreren daran befestigten Abschussrohren besteht. Die Module werden durch einen Antriebsmotor um die Wellenlängsachse herum gedreht, wobei der Antriebsmotor und die Zündsysteme über einen Mikroprozessor ansteuerbar sind. Dadurch wird erreicht, dass mit unterschiedlichen Modulen in dieselbe Richtung geschossen werden kann. Ein Richten der Einheit in der Gesamtheit ist nicht möglich.With the DE 37 05 700 A1 discloses a thrower unit for protecting moving or stationary objects. This unit consists of several modules, which consists of a main body and several attached launching tubes. The modules are rotated by a drive motor around the shaft longitudinal axis, wherein the drive motor and the ignition systems are controlled by a microprocessor. This ensures that different modules can shoot in the same direction. It is not possible to judge unity as a whole.

US 5,415,152 beschreibt eine druckgetriebene Werfereinheit, wobei das Abschussrohr in Ausrichtung zum komprimierten Gas gebracht wird, aus welchem das Projektil verschossen werden soll. US 5,415,152 describes a pressure-driven throwing unit, wherein the launching tube is brought into alignment with the compressed gas from which the projectile is to be fired.

Die Erfindung stellt sich die Aufgabe, eine Wurfanlage aufzuzeigen, die bevorzugt eine Richtmäglichkeit in wenigstens eine Richtachse ermöglicht.The invention has as its object to show a throwing system, which preferably allows a Richtmäglichkeit in at least one straightening axis.

Gelöst wird die Aufgabe durch die Merkmale des Patentanspruchs 1. Vorteilhafte Ausgestaltungen sind in den Unteransprüchen enthalten.The object is achieved by the features of claim 1. Advantageous embodiments are contained in the subclaims.

Der Erfindung liegt die Idee zugrunde, die Abschussrohre für die Wurfkörper kreisförmig um eine Drehachse anzuordnen. Hieraus ergibt sich eine Abschusstrommel, die drehbar es ermöglicht, die bzw. den Wurfkörper aus einer bestimmten Position abzufeuern. Dabei kann die Abschussrichtung starr bestimmt oder aber durch Richten der Trommel eingestellt werden. D.h., der Werfer weist in einer bevorzugten Ausführung eine Richtbarkeit zumindest in einer Richtachse auf. In Weiterführung der Erfindung ist ein Richten in zwei bis drei Achsen vorgesehen.The invention is based on the idea of arranging the launching tubes for the projectiles in a circle around an axis of rotation. This results in a Abschusstrommel that rotatably makes it possible to fire the or the projectile from a certain position. In this case, the firing direction can be determined rigidly or adjusted by straightening the drum. That is, in a preferred embodiment, the thrower has a straightening at least in a straightening axis. In continuation of the invention, a straightening in two to three axes is provided.

Der Abschuss erfolgt idealer Weise aus dem Abschussrohr, dessen Achse sowohl von der Richtachse für die Elevation als auch von der Richtachse für Azimut geschnitten wird. Hierdurch werden beim Abschuss keine Drehmomente um die Richtachse erzeugt. Durch die momentfreie Ausführung können beispielsweise Bremsen und Kupplungen an den Antrieben der Richtachse oder verstellbare Hebelabstützungen entfallen. Des Weiteren können der / die Richtantriebe klein dimensioniert werden. Die Steuerung der Wurfanlage kann vereinfacht werden. Die Werferbauteile können symmetrisch und klein ausgeführt werden.The launching is ideally done from the launch tube whose axis is cut from both the elevation directional axis and the azimuth directional axis. As a result, no torques are generated around the straightening during firing. By torque-free design, for example, brakes and clutches can be omitted on the drives of the directional axis or adjustable lever supports. Furthermore, the straightening drives can be made small. The control of the throwing machine can be simplified. The launcher components can be made symmetrical and small.

In Weiterführung der Lösung, wird zur Erhöhung der Sicherheit nur der in Abfeuerposition befindliche Wirkkörper zumindest elektrisch kontaktiert. So wird sichergestellt, dass nur in der vorgegebenen Magazinstellung abgefeuert werden kann. Bei einer Zwischenstellung der Trommel besitzt der Wurfkörper keinen Kontakt zur Abfeuerung. Zur weiteren Erhöhung der Sicherheit ist vorgesehen, dass die Trommel in der Schussstellung mechanisch verriegelt wird, beispielsweise mittels Bolzen.In continuation of the solution, only the active body located in firing position is contacted at least electrically to increase safety. This ensures that it can only be fired in the specified magazine position. In an intermediate position of the drum of the throwing body has no contact for firing. To further increase the security is provided that the drum is mechanically locked in the firing position, for example by means of bolts.

Bei einer Adaption weiterer Bewegungsachsen (rotatorisch, translatorisch) sind unterschiedliche Ausführungen der Werferanlage erreichbar. So kann diese aus einer verdeckten Parkposition in die Schussposition bewegt werden. Dieses Signaturverhalten ist bei vielen Fahrzeugen erwünscht.In an adaptation of other axes of motion (rotational, translational) different versions of the launcher can be achieved. So this can be moved from a hidden parking position in the firing position. This signature behavior is desirable in many vehicles.

Auch kann die Werfertrommel als Wechselmagazin ausgeführt sein. Dies bringt den Vorteil mit sich, dass vollständig aufmunitionierte Magazine gewechselt werden können. Ein Trommel- / Magazinantrieb ermöglicht die Drehung in eine Indexstellung zum Laden / Entladen des Werfers. Bevorzugt sind zur Schaffung einer hohen Sicherheit in dieser Position die Kontakte zur Abfeuerung getrennt.Also, the Werfertrommel can be designed as a removable magazine. This has the advantage that completely ammunitionierte magazines can be changed. A drum / magazine drive allows rotation to an index position for loading / unloading the launcher. Preferably, the contacts for firing are separated to create a high level of security in this position.

Durch das Verschießen in nur einer Position kann ein bauraumkleiner Werfer geschaffen werden, der Störkanten, Abschattungen etc. durch die Trägerfahrzeugkontur oder dergleichen überschießen kann. Die Integration des Werfers am Trägerfahrzeug ist dadurch nicht örtlich gebunden. Des Weiteren hat das Verschießen in nur einer Position den Vorteil, dass die Kraft- und Momenteinleitung in das Trägerfahrzeug optimiert werden kann.By shooting in only one position, a small space launcher can be created, the interference edges, shadowing, etc. can overshoot by the carrier vehicle contour or the like. The integration of the launcher on the carrier vehicle is thus not locally bound. Furthermore, the firing in only one position has the advantage that the introduction of force and torque into the carrier vehicle can be optimized.

Der Werfer kann des Weiteren an Gebäuden etc. Angebracht werden.The launcher can also be attached to buildings etc.

Um Rückstosskräfte bei Bedarf verringern zu können, kann in Weiterführung der Erfindung an der Abschussposition ein Brems- und Rückstellsystem eingebunden werden. Dies ermöglicht die Nutzung an leichten Trägerfahrzeugen, beispielsweise die Nutzung von Geländewagen, Motorräder, Helikopter, Leichtflugzeuge und dergleichen sowie beispielsweise als mobile, tragbare Systeme.In order to be able to reduce recoil forces when needed, a brake and reset system can be integrated in the launching position in continuation of the invention. This allows the use of light carrier vehicles, such as the use of SUVs, motorcycles, helicopters, light aircraft and the like and, for example, as a mobile, portable systems.

Anhand eines Ausführungsbeispieles mit Zeichnung soll die Erfindung näher erläutert werden.Reference to an embodiment with drawing, the invention will be explained in more detail.

Es zeigt:

Fig. 1
in einer perspektivischen Darstellung eine adaptierbare Wurfanlage,
Fig. 2
eine Vorderansicht der Wurfanlage aus Fig. 1,
Fig. 3
eine Seitendarstellung der Wurfanlage,
Fig. 3a
eine vergrößerte Darstellung B aus Fig. 3,
Fig. 4
eine Schnittdarstellung im Schnitt A-A aus Fig. 2.
It shows:
Fig. 1
in a perspective view an adaptable throwing machine,
Fig. 2
a front view of the throwing machine Fig. 1 .
Fig. 3
a page presentation of the throwing machine,
Fig. 3a
an enlarged view B from Fig. 3 .
Fig. 4
a sectional view in section AA Fig. 2 ,

In Fig. 1 ist eine Wurfanlage 1 mit mehreren Abschussrohren 2, in denen sich hier nicht näher dargestellte Wurfkörper 3 befinden, aufgezeigt. Die Abschussrohre 2 bilden in ihrer Gesamtheit eine Abschusstrommel bzw. ein Trommelmagazin 4, welches in Azimut A um eine Richtachse R1 mittels eines Antriebes 5 und Elevation E um eine Richtachse R2 mittels eines weiteren Antriebes 6 (Fig. 3) verschwenkbar ist. Als Richthilfe bzw. Richtmittel 7 ist eine Videokamera vorgesehen. Die Trommel 4 selbst ist um eigene Trommelachse / Drehachse D verstellbar (Antrieb 13 - Fig.4) und in bzw. an einem Träger 8 gelagert.
Die Wurfanlage 1 kann über einen, an die jeweilige Montagesituation und -position angepassten Ausleger 9 an einem Trägerfahrzeug (nicht näher dargestellt) adaptiert werden.
In Fig. 1 is a launcher 1 with several launch tubes 2, in which there are not shown here throwing body 3, shown. The launch tubes 2 in their entirety form a Abschusstrommel or a drum magazine 4, which in azimuth A about a straightening axis R 1 by means of a drive 5 and elevation E about a straightening axis R 2 by means of another drive 6 (Fig. Fig. 3 ) is pivotable. As a directional aid or directing means 7, a video camera is provided. The drum 4 itself is adjustable about its own drum axis / axis of rotation D (drive 13). Figure 4 ) and stored in or on a carrier 8.
The litter installation 1 can be adapted to a carrier vehicle (not shown in more detail) by means of a bracket 9 adapted to the respective mounting situation and position.

Fig. 2 zeigt die Wurfanlage 1 mit den Abschussrohren 2 und Wurfkörpern 3 in einer Vorderansicht. Fig. 2 shows the throwing machine 1 with the launching tubes 2 and throwing bodies 3 in a front view.

Fig. 3 gibt eine Seitendarstellung der Wurfanlage 1 wieder, Fig. 4 eine Schnittdarstellung der Wurfanlage 1 im Schnitt A-A aus Fig. 2. Fig. 3 gives a side view of the throwing machine 1, Fig. 4 a sectional view of the throwing machine 1 in section AA Fig. 2 ,

Um den jeweiligen Wurfkörper 3 in die Abschussposition zu bringen, wird die Trommel 4 um ihre Achse D verdreht. In der aufgezeigten Darstellung befindet sich der Wurfkörper 31 in der Abschussposition, d,h., aus dem Abschussrohr 2, dessen Achse sowohl von der Richtachse R2 für die Elevation E als auch von der Richtachse R1 für Azimut A geschnitten wird. Ist dieser Wurfkörper 31 gezündet worden, erfolgt eine weitere Verstellung der Trommel 4, bis ein weiterer Wurfkörper 3 in der Abschussposition liegt. Nach Verschuss aller in den Abschussrohren 2 befindlichen Wurfkörper 3 kann das Magazin 4 gewechselt werden. Für das Richten der Abschussrohre 2 wird die Trommel 4 in ihrer Gesamtheit in Azimut und / oder Elevation verstellt. Wird eine Sicherheitsstellung erwünscht, wird die Trommel 4 derart verstellt, dass kein Wurfkörper 3 in Kontakt gelangt (Kontakte 10 und 11 voneinander auch elektrisch getrennt).In order to bring the respective projecting body 3 in the firing position, the drum 4 is rotated about its axis D. In the illustration shown, the throwing body 3 1 is in the firing position, d, h., From the launch tube 2, whose axis is cut both from the straightening axis R 2 for the elevation E and from the straightening axis R 1 for azimuth A. If this projectile has been ignited 3 1 , there is a further adjustment of the drum 4 until another projectile 3 is in the launching position. After firing all located in the launch tubes 2 throwing body 3, the magazine 4 can be changed. For straightening the discharge tubes 2, the drum 4 is adjusted in its entirety in azimuth and / or elevation. If a safety position is desired, the drum 4 is adjusted so that no throwing body 3 comes into contact (contacts 10 and 11 also separated from each other electrically).

Die Kontakte 10, 11 (Fig. 3, 3a) dienen zur Spannungsversorgung der Wurfanlage 1 sowie zur Übertragung des Abfeuersignals. Dabei wird gewährleistet, dass in der Abschussposition nur der sich in dieser Position befindliche Wurfkörper 3 gezündet wird. Bevorzugt kann zudem in der Wurfanlage 1 eine Munitionserkennungseinrichtung 12 (Fig. 3) eingebunden werden.The contacts 10, 11 ( Fig. 3 . 3a ) are used to power the throwing machine 1 and to transmit the firing signal. It is ensured that in the firing position only the projectile located in this position 3 is ignited. In addition, in the litter installation 1, an ammunition detection device 12 (FIG. Fig. 3 ).

Nicht weiter dargestellt ist die Wurfanlage 1 in einer Be-/ Entladeposition. Hierbei ist jedoch zu gewährleisten, dass die Kontakte 11 zur Abfeuerung voneinander getrennt sind bzw. bleiben.Not shown further is the throwing machine 1 in a loading / unloading position. In this case, however, it must be ensured that the contacts 11 for firing are or remain separated from one another.

Claims (12)

  1. Launcher (1) for deploying launch bodies (3), with
    - the launch bodies (3) being active bodies with active media such as smoke, explosive, jamming and/or decoy bodies as well as ammunition,
    - firing tubes (2) being arranged in a circular shape about a rotation axis (D) and forming a firing drum (4) in which the launch bodies (3) are located,
    - the only launch body (3) which is fired being that which is located in a firing position, for which purpose
    - the firing drum (4) can be moved about its own rotation axis (D) by means of a drive (13) and
    - can be swivelled in azimuth (A) about an aiming axis (R1) by means of a drive (5) and
    - in elevation (E) about an aiming axis (R2) by means of a further drive (6),
    - in the firing position, electrical contacts (10, 11) between the firing drum (4) and the launcher (1) being closed in order to fire the launch bodies, and
    - at least one electrical disconnection being provided for the contacts (10, 11) in an intermediate position, a safe position and
    - when the firing drum (4) is in the form of an interchangeable magazine, when the firing drum (4) is changed.
  2. Launcher according to Claim 1, characterized in that firing takes place from the firing tube (2) whose axis is intersected both by the aiming axis (R2) for elevation (E) and by the aiming axis (R1) for azimuth (A).
  3. Launcher according to Claim 1 or 2, characterized in that the firing drum (4) is mechanically locked in the firing position.
  4. Launcher according to one of Claims 1 to 3, characterized in that an aiming aid or aiming means (7) is included.
  5. Launcher according to Claim 4, characterized in that the aiming means (7) is a video camera.
  6. Launcher according to one of the abovementioned Claims 1 to 5, characterized in that the firing drum (4) is mounted in or on a mount (8).
  7. Launcher according to one of the abovementioned Claims 1 to 6, characterized in that the launcher (1) can be selectively adapted via a cantilver arm (9), which is matched to the respective mounting situation and position, on a carrier vehicle.
  8. Launcher according to one of the abovementioned Claims 1 to 7, characterized in that the carrier vehicles may be all-terrain vehicles, motorcycles, helicopters, light aircraft and the like.
  9. Launcher according to one of the abovementioned Claims 1 to 7, characterized in that the launcher (1) can be adapted to a building, fence, marine vessel or the like.
  10. Launcher according to one of the abovementioned Claims 1 to 7, characterized in that the launcher (1) is in the form of a mobile and/or portable system.
  11. Launcher according to one of Claims 1 to 9, characterized in that the launcher (1) can be moved from a parked position to a firing position.
  12. Launcher according to one of the abovementioned Claims 1 to 11, characterized in that a braking and reset system is included at the firing position.
EP06006342.7A 2005-04-28 2006-03-28 Launcher Not-in-force EP1717541B2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005020177A DE102005020177A1 (en) 2005-04-28 2005-04-28 Launch system

Publications (3)

Publication Number Publication Date
EP1717541A1 EP1717541A1 (en) 2006-11-02
EP1717541B1 EP1717541B1 (en) 2009-08-12
EP1717541B2 true EP1717541B2 (en) 2015-11-18

Family

ID=36782580

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06006342.7A Not-in-force EP1717541B2 (en) 2005-04-28 2006-03-28 Launcher

Country Status (4)

Country Link
EP (1) EP1717541B2 (en)
AT (1) ATE439565T1 (en)
DE (2) DE102005020177A1 (en)
DK (1) DK1717541T4 (en)

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RU2718179C2 (en) * 2017-12-04 2020-03-31 Габлия Юрий Александрович Electric-shock directional attack mine

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WO2008099352A1 (en) * 2007-02-14 2008-08-21 Rippel Effect Weapon Systems (Proprietary) Limited Recoil advance mechanism for a multi-shot projectile launcher
DE102007029623A1 (en) 2007-06-26 2009-02-26 Rheinmetall Waffe Munition Gmbh Throwing machine with magazine
DE102007032112A1 (en) 2007-07-09 2009-01-15 Rheinmetall Waffe Munition Gmbh Method and launcher for protecting an object from a threat, in particular a missile, and ammunition
DE102009009082A1 (en) * 2009-02-14 2010-08-19 Krauss-Maffei Wegmann Gmbh & Co. Kg Agent dispensing system for firing non-lethal agents from a vehicle, especially a police or military vehicle
DE102010016542C5 (en) * 2010-04-20 2017-08-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Apparatus and method for straightening a launching container
DE202011101266U1 (en) 2011-05-23 2011-12-20 Rheinmetall Waffe Munition Gmbh Fastening device for a throwing unit
DE202011101269U1 (en) 2011-05-23 2012-02-13 Rheinmetall Waffe Munition Gmbh Fastening device for a throwing unit
DE102012010378A1 (en) 2012-05-29 2013-12-05 Rheinmetall Waffe Munition Gmbh Ammunition with active agents
DE102012010377A1 (en) 2012-05-29 2013-12-05 Rheinmetall Waffe Munition Gmbh Ammunition with active agents
DE102012106746C5 (en) 2012-07-25 2019-08-29 Krauss-Maffei Wegmann Gmbh & Co. Kg Protective equipment, vehicle and method for protecting an object

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Also Published As

Publication number Publication date
ATE439565T1 (en) 2009-08-15
EP1717541A1 (en) 2006-11-02
DE102005020177A1 (en) 2006-11-02
DK1717541T4 (en) 2016-02-15
DK1717541T3 (en) 2009-11-30
DE502006004483D1 (en) 2009-09-24
EP1717541B1 (en) 2009-08-12

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