EP1930685B1 - Lanceur pour l'autodéfense d'un objet mobile ou stationnaire - Google Patents
Lanceur pour l'autodéfense d'un objet mobile ou stationnaire Download PDFInfo
- Publication number
- EP1930685B1 EP1930685B1 EP07023110A EP07023110A EP1930685B1 EP 1930685 B1 EP1930685 B1 EP 1930685B1 EP 07023110 A EP07023110 A EP 07023110A EP 07023110 A EP07023110 A EP 07023110A EP 1930685 B1 EP1930685 B1 EP 1930685B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- launcher
- elevation
- container
- smoke
- suspension
- 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
Links
- 239000000725 suspension Substances 0.000 claims abstract description 23
- 238000010304 firing Methods 0.000 claims abstract description 16
- 230000005484 gravity Effects 0.000 claims abstract description 4
- 230000005540 biological transmission Effects 0.000 claims description 3
- 239000000779 smoke Substances 0.000 claims 8
- 230000007123 defense Effects 0.000 description 6
- 239000002223 garnet Substances 0.000 description 6
- 239000003595 mist Substances 0.000 description 6
- 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
- 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.
- a launcher is from the FR 2 832 792 A known.
- a similar launcher with a replaceable ammunitioned container with launching tubes for firing fragmentation grenades against missiles or from blast grenades against KE rods in the respective remaining phase of their approach to the attacked and defended object is from the DE 199 51 915 A1 known.
- 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 extended if, in addition to the launching tubes for defensive grenades, it is also equipped with Nebelwerfer tubes and designed for elevation angles of at least approximately 360 °.
- Nebelwerfer tubes and designed for elevation angles 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 a replaceable in the suspension 13 salaried container 16 with garnet and Nebetwerfer tubes. 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 gravity 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)
Claims (10)
- Dispositif de lancement (11) avec entraînement directionnel pour l'autodéfense d'un objet mobile ou fixe en tirant des grenades défensives (21) depuis les tubes lance-grenades (17) d'un conteneur (16) qui peut effectuer une rotation autour d'un axe d'azimut (14) avec sa suspension (13) sur un socle (12) fixe de l'objet et qui peut être élevé autour d'un axe d'élévation (15), au moins un tube lance-grenades fumigènes (18) étant en plus prévu pour des engins fumigènes,
caractérisé par
un centre de gravité des masses résultant de la suspension (13) ainsi équipée qui se trouve dans l'axe d'azimut (14),
l'axe d'élévation (15) se trouvant à une hauteur telle au-dessus du sol de la suspension (13) que le conteneur (16) peut exécuter une rotation complète sur 360°. - Dispositif de lancement selon la revendication 1, caractérisé en ce que les tubes lance-grenades fumigènes (18) sont orientés opposés les uns aux autres de manière coaxiale par paire.
- Dispositif de lancement selon la revendication 1 ou 2, caractérisé en ce que les tubes lance-grenades fumigènes (18) sont disposés dans le conteneur (16) décalés dans des espaces à côté des tubes lance-grenades (17).
- Dispositif de lancement selon la revendication 1 ou 2, caractérisé en ce que les tubes lance-grenades fumigènes (18) sont disposés sur un support (22) à l'extérieur du conteneur (16) de manière à pouvoir être remplacés individuellement.
- Dispositif de lancement selon la revendication 4, caractérisé en ce qu'il est prévu un axe d'élévation (15) commun pour les tubes lance-grenades (17) et les tubes lance-grenades fumigènes (18).
- Dispositif de lancement selon l'une des revendications 1 à 5, caractérisé en ce qu'il est prévu un moteur d'élévation (19) commun pour les tubes lance-grenades (17) et les tubes lance-grenades fumigènes (18).
- Dispositif de lancement selon l'une des revendications 1 à 6, caractérisé en ce qu'au moins un moteur d'élévation (19, 23) est disposé dans une branche de la suspension (13) en forme de fourche.
- Dispositif de lancement selon la revendication 7, caractérisé en ce qu'un moteur d'élévation (19, 23) est disposé transversalement à l'axe d'élévation (15) dans chacune des deux branches de la suspension (13) en forme de fourche pour les tubes lance-grenades (17) ou pour les tubes lance-grenades fumigènes (18) et il est en liaison active avec les arbres d'élévation (24) par le biais d'un engrenage de renvoi (25).
- Dispositif de lancement selon l'une des revendications 1 à 6, caractérisé en ce qu'au moins un moteur d'élévation (19) est disposé dans le socle (12).
- Dispositif de lancement selon la revendication 9, caractérisé en ce que le moteur d'élévation (19) est en liaison active parallèlement à l'axe d'azimut (14) avec un pignon d'entraînement (30) sur l'arbre d'élévation (24) au moyen d'un engrenage comme une crémaillère ou par le biais d'une denture conique ou encore par le biais d'une vis sans fin.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006057564A DE102006057564B3 (de) | 2006-12-07 | 2006-12-07 | Werfer zur Selbstverteidigung eines mobilen oder stationären Objektes |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1930685A1 EP1930685A1 (fr) | 2008-06-11 |
EP1930685B1 true EP1930685B1 (fr) | 2010-06-09 |
Family
ID=39153906
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07023110A Not-in-force EP1930685B1 (fr) | 2006-12-07 | 2007-11-29 | Lanceur pour l'autodéfense d'un objet mobile ou stationnaire |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1930685B1 (fr) |
AT (1) | ATE470830T1 (fr) |
DE (2) | DE102006057564B3 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008038603C5 (de) * | 2008-08-21 | 2018-04-19 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Gegenschussanlage |
DE102010025801A1 (de) | 2010-07-01 | 2012-01-05 | Diehl Bgt Defence Gmbh & Co. Kg | Aktives Abwehrsystem für leichte Kampffahrzeuge |
DE102011009154A1 (de) | 2011-01-22 | 2012-07-26 | Diehl Bgt Defence Gmbh & Co. Kg | Verfahren zur Abwehr einer Bedrohung durch Ausbringen von Tarnnebel und Einrichtung zum Ausüben des Abwehr-Verfahrens |
EP2746712B1 (fr) * | 2012-12-20 | 2017-04-12 | Curtiss-Wright Antriebstechnik GmbH | Dispositif d'entraînement pour un lanceur |
EP3306259A1 (fr) | 2016-10-10 | 2018-04-11 | CMI Defence S.A. | Structure standard et interchangeable pour un véhicule blindé |
FR3105391B1 (fr) | 2019-12-24 | 2022-12-02 | Nexter Systems | Dispositif lanceur de munitions |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3018692A (en) * | 1959-08-25 | 1962-01-30 | Andrew G Bilek | Rotatable rocket launcher |
DE3843164C1 (fr) * | 1988-12-22 | 1990-05-10 | Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De | |
DE19951915A1 (de) * | 1999-10-28 | 2001-05-10 | Diehl Munitionssysteme Gmbh | Richtantrieb |
FR2827667B1 (fr) * | 2001-07-17 | 2003-10-03 | Giat Ind Sa | Systeme de pointage en gisement d'une arme |
FR2832792B1 (fr) | 2001-11-29 | 2004-07-16 | Giat Ind Sa | Systeme d'obsersation et/ou de tir |
DE102004017375B4 (de) * | 2004-04-08 | 2009-05-07 | Diehl Bgt Defence Gmbh & Co. Kg | System zum Schutze eines Zieles gegen angreifende Flugkörper |
FR2873194B1 (fr) * | 2004-07-16 | 2007-11-23 | Giat Ind Sa | Dispositif de tir de projectiles |
-
2006
- 2006-12-07 DE DE102006057564A patent/DE102006057564B3/de not_active Expired - Fee Related
-
2007
- 2007-11-29 EP EP07023110A patent/EP1930685B1/fr not_active Not-in-force
- 2007-11-29 DE DE502007004065T patent/DE502007004065D1/de active Active
- 2007-11-29 AT AT07023110T patent/ATE470830T1/de active
Also Published As
Publication number | Publication date |
---|---|
ATE470830T1 (de) | 2010-06-15 |
DE502007004065D1 (de) | 2010-07-22 |
DE102006057564B3 (de) | 2008-08-14 |
EP1930685A1 (fr) | 2008-06-11 |
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