EP1930685A1 - Launcher for self-defence of a mobile or stationary object - Google Patents
Launcher for self-defence of a mobile or stationary object Download PDFInfo
- Publication number
- EP1930685A1 EP1930685A1 EP07023110A EP07023110A EP1930685A1 EP 1930685 A1 EP1930685 A1 EP 1930685A1 EP 07023110 A EP07023110 A EP 07023110A EP 07023110 A EP07023110 A EP 07023110A EP 1930685 A1 EP1930685 A1 EP 1930685A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- elevation
- tubes
- container
- launcher
- launcher 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.)
- Granted
Links
- 239000000725 suspension Substances 0.000 claims abstract description 22
- 238000010304 firing Methods 0.000 claims abstract description 4
- 230000005484 gravity Effects 0.000 claims abstract description 3
- 239000003595 mist Substances 0.000 claims description 9
- 230000007123 defense Effects 0.000 claims description 7
- 239000002223 garnet Substances 0.000 claims description 7
- 230000010354 integration Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000004570 mortar (masonry) Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
Images
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
- F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
- F41A27/06—Mechanical systems
- F41A27/24—Elevating gear
-
- 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
- F41A27/22—Traversing gear
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/145—Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances
- F42B5/15—Cartridges, 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
- F42B5/155—Smoke-pot projectors, e.g. arranged on vehicles
Definitions
- the invention relates to a projector according to the preamble of the main claim.
- Such a launcher is from the DE 1 99 51 915 A1 with an interchangeable ammunitioned container with launching tubes for firing fragmentation grenades against missiles or of blast grenades against KE rods in the respective remaining phase of their approach to the attacked object to be defended.
- the object may be a vehicle (in particular an armored vehicle) or a property (in particular a military camp).
- the excellent suitability of the described there, fast and accurate directional drive with stationary in the launcher pedestal azimuth and elevation drives for the container was meanwhile convincingly demonstrated. Its great agility is essentially based on the fact that in the interest of reducing the masses to be moved during the straightening process, the motors for azimuth and elevation movements are stationary, and mechanically protected, built into the object-fixed gun socket.
- a disadvantage of that construction proves only the restriction to small elevation angles around a structurally predetermined average, in which a height-adjustable push rod for elevation straight in the azimuth axis.
- the articulation of the supported as a one-armed lever on the push rod container namely namely with the elevation a pivoting of the push rod from this axis out with the result that the leverage of the linkage are increasingly unfavorable and the push rod can be subjected to bending.
- an effective defense against all expected attack scenarios requires a mastery of the complete hemisphere; and if possible also, for example, from an elevated location on a vehicle, launch directions below the mounting level of the container.
- it would be desirable to the object In addition to the hard-core active protection provided by the defense grenades, it is also possible to provide flexible soft-kill passive protection.
- the present invention is based on the technical problem of providing a launcher of the generic type for such additional defense options.
- the elevation is no longer limited to a relatively small elevation around a predetermined angle, but the container can rotate virtually around its elevation axis and so far aligned in each spatial direction.
- This solution is of particular advantage in equipping the thrower also with launch tubes for fog pots for temporary camouflage of the object equipped with the launcher.
- additional Nebelwerfer tubes are provided parallel to the garnet tubes. But because they do not have to be as long as the launching tubes for the grenades, there is always a pair of mist thrower tubes installed coaxially in opposite directions. Nevertheless, two mist pots can be fired in succession in the same direction by turning the Nebelwerfer pipes 180 ° after the first firing and adjusting their elevation.
- the Nebelwerfer tube pairs can be conveniently integrated into the container with the grenade tubes or applied as interchangeable tubes to the launcher.
- the suspension of the elevation drive is not in the pedestal but above, in the suspension of the launcher next to the shaft for pivoting the container and arranged laterally offset so that the resulting center of mass of loaded with a loaded with defensive grenade container, including mists , Suspension in the interest of low mass moment of inertia for use of a small-scale azimuth drive as straight as possible in the azimuth axis.
- the functionality of the thrower for hard-core defense of a mobile or stationary object can be significantly expanded if it is equipped according to the invention in addition to the launch tubes for defensive grenades with Nebelwerfer tubes and designed for elevation angle of at least approximately 360 °.
- two nebulized pots ammunition mounted in a pair of oppositely-oriented mist thrower tubes can be sequentially fired in the same direction, if in between there is a 180 ° message in the azimuth axis correcting the elevation.
- the in Fig.1 sketched launcher 11 has a base 12 to be arranged fixed to the object and a rotatably mounted on it, asymmetrically fork-shaped suspension 13. Through this extends orthogonal to the vertical axis of azimuth 14, the horizontal elevation axis 15 for the spatial alignment of an interchangeable in the suspension 13 salaried container 16 with ridge and Nebetwerfer pipes. Its three garnet tubes 17 are loaded with one defense grenade each. In the interest of dense packing to gap, however, offset and parallel to the container 16 is additionally formed here with two Nebelwerfer tubes 18. These are equipped with mist pots.
- each of the Nebelwerfer tubes 18 is functionally pairwise divided so that it can ever fire a fog pot in opposite directions.
- the elevation orientation of the container 16 and thus its launch tubes 17, 18 by means of an elevation motor 19 The is as outlined in the axially wider of the two legs of the suspension 13 and arranged according to Fig.1 be flanged as a geared motor directly to a coaxial with the elevation axis 15 shaft; or the motor shaft is according to Fig.2 oriented transversely to the container, ie elevation shaft and connected via a deflection gear to the elevation shaft.
- the elevation motor 19 is rotatably connected to the container 16 via the elevation shaft.
- This container shaft is so high above the fork leg angle (ie above the ground) of the suspension 13, that the container 16 in principle can perform a full revolution over 360 °. This not only sweeps over the full hemisphere and the underlying space in the elevation, but it also ensures that two mist pots from the pair of coaxial pipe assembly sequentially (after pivoting the container 16 by 180 ° azimuth with adjustment of the elevation) in the same spatial direction can be shot down.
- the center of mass of the assembled suspension 13 is located to the elevation motor 19 offset in the container 16, to minimize the azimuth effective mass moments of inertia as accurately as possible on the azimuth axis 14.
- the elevation motor 19th from a multi-motor drive system 20 from the interior of the object-fixed base 12 out about the azimuth axis 14th twisted; as detailed in the DE 1 99 51 915 A1 is described, which is incorporated herein by reference in full to the present invention description.
- the pairs of the Nebelwerfer tubes 18 are not included in the ammunition with multiple anti-garnets 21 container 16 of the launcher 11, but applied separately replaceable to a separate bracket 22 on the suspension 13.
- This holder 22 is - preferably about a common to the garnet tubes 17 elevation axis 15 - HANnrichtbar by means of its own elevation motor 23, which is oriented transversely to the elevation shaft 24 in the axially narrower leg of the suspension 13 and connected thereto via a deflection gear 25.
- the center of gravity of the assembled suspension 13 is again as accurate as possible on the azimuth axis 14.
- the suspension 13 is again rotated together with its elevation motors 19, 23 by the azimuth drive system 20 about the azimuth axis 14.
- the container 16 is again designed both with garnet tubes as well as with Nebelwerfer tubes.
- the elevation motor 19 is oriented parallel to the azimuth axis 14 and thus oriented transversely to the elevation shaft 24 to the azimuth motors in the drive system 20 in the base 12 inside.
- a drive pinion 30 on the elevation shaft 24 meshes with the output of the elevation motor in the form of a rack or a worm, so that now only the mass of the container 16 together with its fork-shaped suspension 13 but no more elevation engine participates in the azimuth rotation.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
- Closures For Containers (AREA)
Abstract
Description
Die Erfindung betrifft einen Werfer gemäß dem Oberbegriff des Hauptanspruches.The invention relates to a projector according to the preamble of the main claim.
Ein derartiger Werfer ist aus der
In Erkenntnis dieser Gegebenheiten liegt vorliegender Erfindung die technische Problemstellung zugrunde, einen Werfer gattungsgemäßer Art für solche zusätzlichen Abwehrmöglichkeiten auszustatten.In recognition of these circumstances, the present invention is based on the technical problem of providing a launcher of the generic type for such additional defense options.
Diese Aufgabe ist durch die im Hauptanspruch angegebenen wesentlichen Merkmale gelöst. Danach ist die Elevation nicht mehr auf eine relativ kleine Elevation um einen vorgegebenen Winkel herum beschränkt, sondern der Container kann praktisch um seine Elevationsachse rotieren und insoweit in jede Raumrichtung ausgerichtet werden.This object is achieved by the essential features specified in the main claim. Thereafter, the elevation is no longer limited to a relatively small elevation around a predetermined angle, but the container can rotate virtually around its elevation axis and so far aligned in each spatial direction.
Diese Lösung ist von besonderem Vorteil bei Ausstattung des Werfers auch mit Abschussrohren für Nebeltöpfe zum vorübergehenden Tarnen des mit dem Werfer ausgestatteten Objektes. Um dafür denselben Richtantrieb wie für den Abschuss von Abwehrgranaten nutzen zu können, sind parallel zu den Granat-Rohren zusätzliche Nebelwerfer-Rohre vorgesehen. Weil die aber nicht so lang sein müssen, wie die Abschussrohre für die Granaten, ist immer ein Paar von Nebelwerfer-Rohren koaxial gegensinnig eingebaut. Zwei Nebeltöpfe können daraus dennoch - nacheinander - in derselben Richtung abgeschossen werden, indem die Nebelwerfer-Rohre nach dem ersten Abschuss um 180° verschwenkt und ihre Elevation angepasst werden.This solution is of particular advantage in equipping the thrower also with launch tubes for fog pots for temporary camouflage of the object equipped with the launcher. In order to be able to use the same directional drive as for the launch of defense grenades, additional Nebelwerfer tubes are provided parallel to the garnet tubes. But because they do not have to be as long as the launching tubes for the grenades, there is always a pair of mist thrower tubes installed coaxially in opposite directions. Nevertheless, two mist pots can be fired in succession in the same direction by turning the Nebelwerfer pipes 180 ° after the first firing and adjusting their elevation.
Die Nebelwerfer-Rohrpaare können zweckmäßigerweise in den Container mit den Granaten-Rohren integriert oder als austauschbare Einzelrohre an den Werfer appliziert werden. Für einen kleinbauenden Antrieb der Aufhängung ist der Elevationsantrieb nicht im Sockel sondern darüber, in der Aufhängung des Werfers neben der Welle für das Verschwenken des Containers und dabei derart seitlich versetzt angeordnet, dass der resultierende Masseschwerpunkt der, mit einem mit Abwehrgranaten geladenen Container samt Nebeltöpfen bestückten, Aufhängung im Interesse geringen Masseträgheitsmomentes für Einsatz eines kleinbauenden Azimut-Antriebes möglichst gerade in der Azimutachse liegt.The Nebelwerfer tube pairs can be conveniently integrated into the container with the grenade tubes or applied as interchangeable tubes to the launcher. For a small-sized drive the suspension of the elevation drive is not in the pedestal but above, in the suspension of the launcher next to the shaft for pivoting the container and arranged laterally offset so that the resulting center of mass of loaded with a loaded with defensive grenade container, including mists , Suspension in the interest of low mass moment of inertia for use of a small-scale azimuth drive as straight as possible in the azimuth axis.
Andererseits können für das Elevationsrichten zwei separate, - auch insgesamt - masseärmere Motore zum Einsatz gelangen und die Richtkinematiken dadurch separat wirkoptimiert werden, wenn für die Abwehrgranaten und für die Nebeltöpfe zwei unabhängig von einander anzusteuernde Elevations-Antriebe eingesetzt werden, die ebenfalls den Azimut-Richtvorgang mitdrehen.On the other hand, for the elevation two separate, - also total - lower-mass motors can be used and the directional kinematics are thus optimized separately, if for the defensive grenades and for the mist pots two be used independently of each other to be controlled elevation drives, which also rotate the azimuth straightening process.
Geringste zu beherrschende Trägheitsmomente treten auf, wenn das Elevations- und das Azimut-Richten wieder durch gehäusefest in den Werfer-Sockel eingebaute Antriebe entkoppelt werden. Statt der Schubstange für die Container-Elevation ist dann wenigstens eine Spindel mit Kegelradgetriebe zweckmäßig, die von einem zugeordneten Getriebemotor zur Voruntersetzung verdreht wird, um den Container praktisch rundum zu schwenken. Stattdessen kann aber auch wenigstens ein Linerantrieb zum Längsverschieben einer Zahnstange vorgesehen sein, die mit einem Ritzel auf einer Elevationswelle kämmt.The lowest moments of inertia to be controlled occur when the elevation and azimuth straightening are decoupled again by drives built into the launcher base fixed to the housing. Instead of the push rod for the container elevation then at least one spindle with bevel gear is appropriate, which is rotated by an associated gear motor for Voruntersetzung to pivot the container virtually all around. Instead, however, at least one liner drive for longitudinal displacement of a rack may be provided, which meshes with a pinion on an elevation shaft.
Jedenfalls kann die Funktionalität des Werfers für Hardkill-Verteidigung eines mobilen oder stationären Objektes wesentlich erweitert werden, wenn er erfindungsgemäß zusätzlich zu den Abschussrohren für Abwehrgranaten auch mit Nebelwerfer-Rohren ausgestattet und für Elevationswinkel von wenigstens annähernd 360° ausgelegt wird. Dadurch können zwei in einem Paar von gegensinnig orientierten Nebelwerfer-Rohren munitionierte Nebeltöpfe nacheinander in dieselbe Richtung abgefeuert werden, wenn zwischendurch ein Nachrichten um 180° in der Azimutachse unter Korrektur der Elevation erfolgt.In any case, the functionality of the thrower for hard-core defense of a mobile or stationary object can be significantly expanded if it is equipped according to the invention in addition to the launch tubes for defensive grenades with Nebelwerfer tubes and designed for elevation angle of at least approximately 360 °. As a result, two nebulized pots ammunition mounted in a pair of oppositely-oriented mist thrower tubes can be sequentially fired in the same direction, if in between there is a 180 ° message in the azimuth axis correcting the elevation.
Zusätzliche Abwandlungen und Weiterbildungen zur erfindungsgemäßen Lösung ergeben sich aus den weiteren Ansprüchen und, auch hinsichtlich deren Vorteilen, aus nachstehender Beschreibung von in der Zeichnung nicht ganz maßstabsgerecht auf das Funktionswesentliche abstrahiert skizzierten bevorzugten Ausführungsbespielen zur Erfindung. In der Zeichnung zeigen:
- Fig.1
- in Ansicht einen Werfer mit Integration der Abschussrohre für Nebeltöpfe in den Container mit den Abschussrohren für Abwehrgranaten,
- Fig.2
- im Längsschnitt einen Werfer mit getrennten Elevationsantrieben für Hardkill- und für Softkill-Abschussrohre und
- Fig.3
- eine Antriebs-Entkopplung für Elevation und Azimut bei einem Werfer nach
Fig.1 .
- Fig.1
- in view a launcher with integration of pothole launching tubes into the container with the mortar launching tubes,
- Fig.2
- in longitudinal section a launcher with separate elevation drives for Hardkill- and for Softkill launch tubes and
- Figure 3
- a drive decoupling for elevation and azimuth in a launcher after
Fig.1 ,
Der in
Die Elevationsausrichtung des Containers 16 und damit seiner Abschuss-Rohre 17, 18 erfolgt mittels eines Elevationsmotors 19. Der ist wie skizziert im axial breiteren der beiden Schenkel der Aufhängung 13 angeordnet und kann gemäß
Diese Containerwelle liegt so hoch über dem Gabelschenkelwinkel (also über dem Boden) der Aufhängung 13, dass der Container 16 im Prinzip eine volle Umdrehung über 360° ausführen kann. Dadurch wird nicht nur die volle Hemisphäre sowie der darunter gelegene Raum in der Elevation überstrichen, sondern es ist auch sichergestellt, dass zwei Nebeltöpfe aus dem Paar einer koaxialen Rohranordnung nacheinander (nach Verschwenken des Containers 16 um 180° Azimut unter Anpassung der Elevation) in die selbe Raumrichtung abgeschossen werden können.This container shaft is so high above the fork leg angle (ie above the ground) of the
Der Masseschwerpunkt der so bestückten Aufhängung 13 liegt zu dem Elevationsmotor 19 hin versetzt in dem Container 16, zum Minimieren der beim Azimutrichten wirksamen Masseträgheitsmomente möglichst genau auf der Azimutachse 14. Für den Azimut-Richtvorgang wird die Aufhängung 13 mit dem Container 16 samt dem Elevationsmotor 19 von einem mehrmotorigen Antriebssystem 20 aus dem Innern des objektfesten Sockels 12 heraus um die Azimutachse 14 verdreht; wie es detailliert in der
Im Beispielsfalle der
Die Aufhängung 13 wird wieder mitsamt ihren Elevationsmotoren 19, 23 vom Azimut-Antriebssystem 20 um die Azimutachse 14 gedreht. Dafür arbeiten wieder zwei Azimutmotore 26 über ihre Abtriebsritzel 27 gemeinsam auf eine Verzahnung 28 an einem Lagerring 29, der die Aufhängung 13 drehfest trägt. Bei Gleichlauf der Azimutmotore 26-26 wird der Lagerring 29 um die Azimutachse 14 verdreht, bei gegensinniger Ansteuerung in der dann gerade erreichten Winkelstellung mechanisch spielfrei arretiert.The
Beim Ausführungsbeispiel gemäß
Andererseits ist auch eine Kegelrad-Übertragung denkbar, deren Horizontal-Achse sich mit der Vertikal-Achse schneidet. Verringert werden dadurch die Trägheitsmomente.On the other hand, a bevel gear transmission is conceivable whose horizontal axis intersects with the vertical axis. This reduces the moments of inertia.
- 1111
- Werferthrower
- 1212
- Sockelbase
- 1313
- Aufhängungsuspension
- 1414
- Azimutachseazimuth axis
- 1515
- Elevationsachseelevation axis
- 1616
- ContainerContainer
- 1717
- Granat-RohreGarnet tubes
- 1818
- Nebelwerfer-RohreNebelwerfer pipes
- 1919
- Elevationsmotor (für 16)Elevation motor (for 16)
- 2020
- Azimut-AntriebssystemAzimuth drive system
- 2121
- AbwehrgranateAnti-tank grenade
- 2222
- Halterungbracket
- 2323
- Elevationsmotor (für 22)Elevation motor (for 22)
- 2424
- Elevationswellenelevation waves
- 2525
- Umlenkgetriebedeflecting
- 2626
- AzimutmotoreAzimut motors
- 2727
- Abtriebsritzel (von 26)Output pinion (from 26)
- 2828
- Verzahnunggearing
- 2929
- Lagerringbearing ring
- 3030
- Antriebsritzelpinion
Claims (10)
dadurch gekennzeichnet,
dass die Elevation des Containers (16) sich über wenigstens annähernd 360° erstreckt und dass zusätzlich wenigstens ein Abschussrohr (Nebelwerfer-Rohr 18) für Nebeltöpfe vorgesehen ist, bei einem in der Azimutachse (14) liegenden resultierenden Masseschwerpunkt der so bestückten Aufhängung (13).Thrower 11 with directional drive for self-defense of a mobile or stationary object by firing of defense grenades (21) from launching tubes (garnet tubes 17) one with its suspension (13) on an object-fixed base (12) about an azimuth axis (14) rotatable and elevierbaren container (16)
characterized,
that the elevation of the container (16) extends over at least approximately 360 ° and that in addition at least one launcher (Nebelwerfer tube 18) is provided for mist pots, at a in the azimuth axis (14) lying resulting center of gravity of the so equipped suspension (13) ,
dadurch gekennzeichnet,
dass die Nebelwerfer-Rohre (18) koaxial paarweise einander entgegengesetzt orientiert sind.Launcher according to the preceding claim,
characterized,
that the Nebelwerfer tubes (18) coaxially oriented in pairs opposite to each other.
dadurch gekennzeichnet,
dass die Nebelwerfer-Rohre (18) auf Lücke versetzt neben den Granat-Rohren (17) im Container (16) angeordnet sind.Launcher according to one of the preceding claims,
characterized,
in that the mist thrower tubes (18) are arranged in a gap next to the garnet tubes (17) in the container (16).
dadurch gekennzeichnet,
dass die Nebelwerfer-Rohre (18) einzeln austauschbar an einer Halterung (22) außerhalb des Containers (16) angeordnet sind.A launcher according to any one of the preceding claims without the immediately preceding claim,
characterized,
in that the mist thrower tubes (18) are arranged individually exchangeably on a mount (22) outside the container (16).
dadurch gekennzeichnet,
dass eine gemeinsame Elevationsachse (15) für die Rohre (17, 18) vorgesehen ist.Launcher according to the preceding claim,
characterized,
that a common elevation axis (15) for the tubes (17, 18) is provided.
dadurch gekennzeichnet,
dass ein gemeinsamer Elevationsmotor (19) für die Rohre (17, 18) vorgesehen ist.Launcher according to one of the preceding claims,
characterized,
that a common elevation motor (19) for the tubes (17, 18) is provided.
dadurch gekennzeichnet,
dass wenigstens ein Elevationsmotor (19; 23) in einem Schenkel der gabelförmigen Aufhängung (13) angeordnet ist.Launcher according to one of the preceding claims,
characterized,
in that at least one elevation motor (19; 23) is arranged in one leg of the fork-shaped suspension (13).
dadurch gekennzeichnet,
dass in jedem beider Schenkel der gabelförmigen Aufhängung (13) ein Elevationsmotor (19, 23) quer zur Elevationsachse (15) für die Granat-Rohre (17) bzw. für die Nebelwerfer-Rohre (18) angeordnet und über ein Umlenkgetriebe mit den Elevationswellen (24) wirkverbunden ist.Launcher according to the preceding claim,
characterized,
that in each of both legs of the fork-shaped suspension (13) arranged one elevation motor (19, 23) transversely to the elevation axis (15) for the garnet-tubes (17) or for the rocket launcher tubes (18) and via a deflection gear to the elevation shafts (24) is operatively connected.
dadurch gekennzeichnet,
dass wenigstens ein Elevationsmotor (19) im Sockel (12) angeordnet ist.A launcher according to any one of the preceding claims without the two immediately preceding claims,
characterized,
in that at least one elevation motor (19) is arranged in the base (12).
dadurch gekennzeichnet,
dass der Elevationsmotor (19) parallel zur Azimutachse (14) mittels eines Getriebes, wie einer Zahnstange oder über eine Kegelverzahnung oder über ein Schneckenrad mit einem Antriebsritzel (30) auf der Elevationswelle (24) wirkverbunden ist.Launcher according to the preceding claim,
characterized,
in that the elevation motor (19) is operatively connected to the azimuth axis (14) by means of a gear, such as a toothed rack or via a conical toothing or via a worm wheel with a drive pinion (30) on the elevation shaft (24).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006057564A DE102006057564B3 (en) | 2006-12-07 | 2006-12-07 | Thrower for self-defense of a mobile or stationary object |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1930685A1 true EP1930685A1 (en) | 2008-06-11 |
EP1930685B1 EP1930685B1 (en) | 2010-06-09 |
Family
ID=39153906
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07023110A Not-in-force EP1930685B1 (en) | 2006-12-07 | 2007-11-29 | Launcher for self-defence of a mobile or stationary object |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1930685B1 (en) |
AT (1) | ATE470830T1 (en) |
DE (2) | DE102006057564B3 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2157398A3 (en) * | 2008-08-21 | 2012-07-18 | Krauss-Maffei Wegmann GmbH & Co. KG | Countermeasure launcher |
DE102011009154A1 (en) | 2011-01-22 | 2012-07-26 | Diehl Bgt Defence Gmbh & Co. Kg | Method for defensive threat by dispending of camouflage smoke, involves utilizing movement grenades for discharging visual camouflage smoke effective masses before attacking unit |
EP2746712A1 (en) | 2012-12-20 | 2014-06-25 | Curtiss-Wright Antriebstechnik GmbH | Actuation device for a launcher |
WO2017211911A1 (en) * | 2016-06-10 | 2017-12-14 | Cmi Defence S.A. | Modular turret |
FR3105391A1 (en) | 2019-12-24 | 2021-06-25 | Nexter Systems | AMMUNITION LAUNCHING DEVICE |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102010025801A1 (en) | 2010-07-01 | 2012-01-05 | Diehl Bgt Defence Gmbh & Co. Kg | Active defense system for light combat vehicles |
Citations (5)
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US3018692A (en) * | 1959-08-25 | 1962-01-30 | Andrew G Bilek | Rotatable rocket launcher |
EP0374409A1 (en) * | 1988-12-22 | 1990-06-27 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Container for scatter ammunition |
DE19951915A1 (en) | 1999-10-28 | 2001-05-10 | Diehl Munitionssysteme Gmbh | Directional drive |
WO2003008894A1 (en) * | 2001-07-17 | 2003-01-30 | Giat Industries | System for directional angle aiming of a weapon |
FR2832792A1 (en) | 2001-11-29 | 2003-05-30 | Giat Ind Sa | Military vehicle observation/firing system having observation unit interfacing vehicle and elevation unit with interface allowing observation unit raising |
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---|---|---|---|---|
DE102004017375B4 (en) * | 2004-04-08 | 2009-05-07 | Diehl Bgt Defence Gmbh & Co. Kg | System for protecting a target against attacking missiles |
FR2873194B1 (en) * | 2004-07-16 | 2007-11-23 | Giat Ind Sa | DEVICE FOR SHOOTING PROJECTILES |
-
2006
- 2006-12-07 DE DE102006057564A patent/DE102006057564B3/en not_active Expired - Fee Related
-
2007
- 2007-11-29 EP EP07023110A patent/EP1930685B1/en not_active Not-in-force
- 2007-11-29 AT AT07023110T patent/ATE470830T1/en active
- 2007-11-29 DE DE502007004065T patent/DE502007004065D1/en active Active
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US3018692A (en) * | 1959-08-25 | 1962-01-30 | Andrew G Bilek | Rotatable rocket launcher |
EP0374409A1 (en) * | 1988-12-22 | 1990-06-27 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Container for scatter ammunition |
DE19951915A1 (en) | 1999-10-28 | 2001-05-10 | Diehl Munitionssysteme Gmbh | Directional drive |
WO2003008894A1 (en) * | 2001-07-17 | 2003-01-30 | Giat Industries | System for directional angle aiming of a weapon |
FR2832792A1 (en) | 2001-11-29 | 2003-05-30 | Giat Ind Sa | Military vehicle observation/firing system having observation unit interfacing vehicle and elevation unit with interface allowing observation unit raising |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2157398A3 (en) * | 2008-08-21 | 2012-07-18 | Krauss-Maffei Wegmann GmbH & Co. KG | Countermeasure launcher |
DE102008038603C5 (en) * | 2008-08-21 | 2018-04-19 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Gegenschuss conditioning |
DE102011009154A1 (en) | 2011-01-22 | 2012-07-26 | Diehl Bgt Defence Gmbh & Co. Kg | Method for defensive threat by dispending of camouflage smoke, involves utilizing movement grenades for discharging visual camouflage smoke effective masses before attacking unit |
EP2746712A1 (en) | 2012-12-20 | 2014-06-25 | Curtiss-Wright Antriebstechnik GmbH | Actuation device for a launcher |
WO2017211911A1 (en) * | 2016-06-10 | 2017-12-14 | Cmi Defence S.A. | Modular turret |
EP3469299B1 (en) | 2016-06-10 | 2020-05-27 | CMI Defence S.A. | Modular turret |
US10712115B2 (en) | 2016-06-10 | 2020-07-14 | Cmi Defence S.A. | Modular turret |
EP3306259A1 (en) * | 2016-10-10 | 2018-04-11 | CMI Defence S.A. | Standard, interchangeable structure for an armoured vehicle |
FR3105391A1 (en) | 2019-12-24 | 2021-06-25 | Nexter Systems | AMMUNITION LAUNCHING DEVICE |
WO2021130605A1 (en) | 2019-12-24 | 2021-07-01 | Nexter Systems | Ammunition launching device |
US11719500B2 (en) | 2019-12-24 | 2023-08-08 | Nexter Systems | Ammunition launching device |
Also Published As
Publication number | Publication date |
---|---|
DE102006057564B3 (en) | 2008-08-14 |
DE502007004065D1 (en) | 2010-07-22 |
EP1930685B1 (en) | 2010-06-09 |
ATE470830T1 (en) | 2010-06-15 |
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