EP1096218A2 - Richtantrieb - Google Patents
Richtantrieb Download PDFInfo
- Publication number
- EP1096218A2 EP1096218A2 EP00122062A EP00122062A EP1096218A2 EP 1096218 A2 EP1096218 A2 EP 1096218A2 EP 00122062 A EP00122062 A EP 00122062A EP 00122062 A EP00122062 A EP 00122062A EP 1096218 A2 EP1096218 A2 EP 1096218A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- azimuth
- launcher
- substructure
- elevation
- support ring
- 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
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
- F41A27/28—Electrically-operated systems
Definitions
- the invention relates to directional drives according to the preambles of the main claims.
- Such directional drives are known from EP 0 149 639 B1 for the weapon turret known light military vehicle.
- the one that can be turned relative to the vehicle The tower is supported by a radial ball bearing on a plate, which in turn leads to the Cushioning of the recoil of the barrel weapon by means of elastic supports from the vehicle chassis will be carried.
- Tilting moments acting on the plate are from her about a hollow truncated cone-shaped cage against a central shaft in the azimuth axis of the tower rotation. For azimuth straightening, this is done Rotation of the tower around this shaft via a bearing mounted in the plate Pinion that is driven by a vehicle-mounted engine via a belt drive becomes.
- the central wave ends in front of the tower a linear rack, in which the pinion is mounted fixed to the vehicle Motor engages to move the shaft in the direction of the azimuth axis.
- the rack opposite is a fork on this shaft via a ball joint connected.
- Their free foreheads are quite far behind - approximated by the center of gravity of the gun - elevation axis to the gun articulated, whereby this is directed in height via the rack and pinion drive can be.
- the present invention is based on the object
- Directional drives for azimuth and elevation as well as for a combined azimuth and elevation alignment of the weapon - especially in the form of the mentioned Launcher - designed to meet such critical requirements are optimized, i.e. as fast and as free of play as possible, exactly alignment of the launching container to be observed according to azimuth and / or Elevation for targeted firing, especially against a defense grenade enable an attacking missile.
- the support ring for the fork-shaped swivel bracket is attached to the platform a rotating bearing of low axial height to accommodate both axial as well as radial loads are carried, preferably as such as such known cross roller bearing is designed.
- a rotating bearing of low axial height to accommodate both axial as well as radial loads are carried, preferably as such as such known cross roller bearing is designed.
- the fork-shaped swivel bracket mounted on the rotatable support ring preferably has about the geometry of a rigid unequal leg right-angled triangle, which with its longer Kathethe fixed on motion resting and opposite the support ring, in the area of the transition from the axially parallel shorter Kathethe to the hypotenuse, outside the course of the Azimuth axis with a swivel eye for tilting for elevation adjustment of the launching container suspended in the holder.
- this swivel axis passes across it with the azimuth axis of the support ring identical central axis of the substructure. It is preferably at medium elevation the launching container, its linkage to the support rod just on the azimuth axis.
- the launching container is supported on the coupling rod along the azimuth axis a translational output of the concentric to the support ring and thus coaxial also fixed to the azimuth axis in the housing of the substructure Elevator servomotor. Its output is about a telescope or preferably a conversion from a motor rotary movement into an output linear movement via a spindle nut on a threaded rod.
- the Elevation servomotor as a whole or in any case its output are relative to the Substructure rotatable, if not the support rod in itself or over at least one Ball joint is rotatable relative to the substructure, because the support ring for the azimuth aiming rotates around the azimuth axis and thereby the coupling of the fixed object Elevation motor takes to the rotatable launch container.
- no rotatable coupling is installed here, i.e.
- the directional drive designed according to the invention serves to protect a stationary or mobile object 11 against an approaching object fast steering projectile (not considered in the drawing) by counterfire at least one fragmentation grenade from one with several Grenades in interchangeable firing tubes can be loaded is carried by the object 11 to be protected via the directional drive 10 after sensing the direction of the threat, the direction of launch of those to be fired Defense grenade as quickly as possible in azimuth and elevation on the attacking missile to be able to align - as in the already cited US 5,661,254 A. described in more detail with regard to the mechanism of action of the splinter defense grenade, which is expressly referred to here to avoid repetitions becomes.
- the servomotors 13, 14 are not included the launcher 12 moves, but in the housing of a fixed substructure 15 of the directional drive 10 installed, as in the drawing by the in the object 11 recessed pot-shaped housing symbolically illustrates.
- This Pot-shaped base 15 for the stationary reception of the servomotors 13, 14 and for rotatably receiving a swivel bracket 19 for the launching container 12 carries on or in a (at least partially recessed into the supporting object) Housing covering, with ibs.
- At least one azimuthal servomotor 14 stationary in the substructure 15 and preferably arranged parallel to the azimuth axis 17.
- These teeth 25 on the torque bearing of the support ring 18 represents the only functional interface to be adjusted between stationary base 15 and rotating swivel bracket 19.
- the rotational engagement is radially opposite for its radial support, and preferably designed at the same time for its axial mounting, at least one Rolling bearings arranged in the base plate 16, which run as a ring as outlined, but basically also from individual peripherally offset bearings can exist. It is preferred that it rotates within the support ring 18 Torque bearing 26 designed, the on its mutually perpendicular roller tracks can absorb both axial and radial forces.
- At least two azimuthal servomotors 14 are e.g. equidistant distributed over the circumference of the support ring 18. For the azimuth straightening process if they are switched to synchronism, they drive the support ring 18 in the same direction of rotation on. When the azimuthal target position is reached, the azimuthal servomotors become 14 turned off per se, but at least a couple of them will switched to the same drive torque with opposite drive direction, see above that at least two motors 14 block each other via the toothing 25 and thereby the achieved azimuthal alignment of the launch container 12 without play fix.
- the elevation servomotor 13 also does not rotate in order to reduce rotating masses with the support ring 18. Rather, the elevation servomotor 13 is concentric with Azimuth axis 17 embedded under the support ring 18 in the base 15.
- the elevation servomotor 13 can have a translational output 23 in Form of a telescope or to convert the rotary into a translatory Output movement of the motor 13 in the form of a sliding nut on a motor shaft with a threaded spindle, for example in the manner of a roller screw drive or Trapezoidal spindle can be designed.
- This output 23 is also connected via a support rod 22 the launch container 12 connected to it already relative to the substructure 15 the azimuth setting and / or in the currently reached azimuth position to raise or lower.
- the distance between the pivot axis 20 for the elevation of the launcher 12 and the eye 21 for elevation support on the support rod 22 chosen as low as possible so that the deflection on both sides of a medium elevation the support rod 22 remains as small as possible out of the azimuth axis 17 and thereby a practically bending moment-free, i.e. ideal kinetic Pressure can be transmitted from the linear output 23 of the servomotor 13.
- the operative connection between the elevation servomotor 13 and the launching container 12 can be rotated here relative to the substructure 15 because the launching container 12 an azimuth setting relative in the interest of smaller masses to be rotated to the elevation servomotor 13 arranged in a stationary manner in the substructure 15.
- This Rotatability which affects the elevation during due to the Prevents azimuthal alignment, the translational output 23 can be relative have its servomotor 13, as symbolically in the sketch by a rotary bearing 29 illustrated to the articulations of the support rod 22 on the one hand Firing container 12 and opposite to the elevation servomotor 13 as to be able to train one-dimensional swivel joints.
- the rotatability can but also be ensured that at least one of these two coupling points 30 is designed as a ball joint, so that the rotation during the azimuth setting not on the output side directly on the elevation servomotor 13 takes place, but in at least one of these coupling points 30 so also function-critical linear plain bearings avoided.
- a directional drive 10 which can be integrated into an object 11 to be protected, for fast Alignment of the fork-shaped swivel bracket 19 of a launch container 12 for frag grenades to ward off an attacking missile the interpretation according to the invention thus by the possibility of more precise simultaneous Azimuth and elevation settings with particularly high dynamics of this Straightening process despite the heavy weight of the chip grenades Launching container 12 from.
- the servomotors 13, 14 are from the swivel bracket 19 continued and protected against splintering, for example parallel to Azimuth axis 17, relocated to a fixed substructure 15, where it with a Substructure 15, support ring 18 held rotatably by means of a torque bearing 26 are in rotary connection for the azimuth adjustment of the swivel bracket 19.
- Elevation servomotor 13 has a translatory output 23 equipped, which is essentially concentric to the azimuth axis 17 extending and rotatable about this support rod 22, the elevation of the launching container 12 determined.
Abstract
Description
Claims (7)
- Richtantrieb (10) für eine Abschußeinrichtung auf einem Objekt (11), der zum Ausrichten einer Schwenkhalterung (19) für die Abschußeinrichtung in einem objektfesten Unterbau (15) einen Azimut-Stellmotor (14) mit einem rotatorischen Abtrieb (Ritzel 24) zu einem Tragring (18) für die Schwenkhalterung (19) aufweist, dadurch gekennzeichnet, daß, insbesondere zur Abwehr eines das Objekt (11) angreifenden Flugkörpers mittels Splittergranaten aus der Abschußeinrichtung in Gestalt eines Abschußbehälters (12), zum schnellen Azimut-Ausrichten des Abschußbehälters (12) in seinem Unterbau (15) wenigstens zwei auf den Tragring (18) wirkende Azimut-Stellmotore (14) parallel zur Azimutachse (17) angeordnet sind, von denen wenigstens einer von gleichsinnigem Antrieb mit dem anderen zur Einnahme einer Azimutstellung auf gegensinnigen Antrieb zur Arretierung der erreichten Azimutstellung des Tragringes (18) umsteuerbar ist.
- Richtantrieb (10) für eine Abschußeinrichtung auf einem Objekt (11), der zum Ausrichten einer Schwenkhalterung (19) für die Abschußeinrichtung in einem objektfesten Unterbau (15) einen Elevations-Stellmotor (13) mit gegenüber dem Unterbau (15) verdrehbarer, über ein Gelenk und durch einen Tragring (18) für die Schwenkhalterung (19) hindurch verlaufender Abstützung (Stützstange 22) für die Elevation der Abschußeinrichtung aufweist, dadurch gekennzeichnet, daß, insbesondere zur Abwehr eines das Objekt (11) angreifenden Flugkörpers mittels Splittergranaten aus einer Abschußeinrichtung in Gestalt eines Abschußbehälters (12), zum schnellen Elevations-Ausrichten des Abschußbehälters (12) in seinem Unterbau (15) konzentrisch zur Azimutachse (17) der Elevations-Stellmotor (13) angeordnet ist, der mit einem translatorischen, relativ zum Stellmotor (13) um die Azimutachse (17) verdrehbaren Abtrieb (23) ausgestattet ist, an den eine Stützstange (22) angelenkt ist, auf welcher der Abschußbehälter (12) ruht.
- Richtantrieb nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß die Stellmotore (13, 14) stationär in einem topfförmigen Unterbau (15) angeordnet sind.
- Richtantrieb nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß der mit der Schwenkhalterung (19) verdrehbare Tragring (18) über ein Momentenlager (26) geringer axialer Bauhöhe am Unterbau (15) radial und axial gehalten ist.
- Richtantrieb nach einem der vorangehenden Ansprüche, dadurch gekennzeichnet, daß die Schwenkhalterung (19) die Geometrie eines ungleichschenkeligen rechtwinkligen Dreiecks aufweist, das mit seiner längeren Kathethe bewegungsstarr auf dem Tragring (18) ruht und gegenüberliegend mit einem Schwenkauge für die Schwenkachse (20) des Abschußbehälters (12) ausgestattet ist.
- Richtantrieb nach Anspruch 5, dadurch gekennzeichnet, daß der Abschußbehälter (12) dicht neben der Schwenkachse (20) mit einem Auge (21) an die Stützstange (22) angelenkt ist, die gegenüberliegend an den zur Azimutachse (17) koaxialen translatorischen Abtrieb (23) des Elevations-Stellmotors (13) angelenkt ist, mit beidseitig eindimensionalen Schwenkgelenken.
- Richtantrieb (10) für eine Abschußeinrichtung auf einem Objekt (11), der zum Ausrichten einer Schwenkhalterung (19) für die Abschußeinrichtung in einem objektfesten Unterbau (15) Stellmotore (13, 14) aufweist, dadurch gekennzeichnet, daß, insbesondere zur Abwehr eines das Objekt (11) angreifenden Flugkörpers mittels Splittergranaten aus der Abschußeinrichtung in Gestalt eines Abschußbehälters (12), Azimut-Stellmotore (14) nach Anspruch 1 und ein Elevations-Stellmotor (13) nach Anspruch 2 in einem topfförmigen Unterbau (15) angeordnet sind.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19951915A DE19951915A1 (de) | 1999-10-28 | 1999-10-28 | Richtantrieb |
DE19951915 | 1999-10-28 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1096218A2 true EP1096218A2 (de) | 2001-05-02 |
EP1096218A3 EP1096218A3 (de) | 2002-04-10 |
EP1096218B1 EP1096218B1 (de) | 2004-09-29 |
Family
ID=7927155
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00122062A Expired - Lifetime EP1096218B1 (de) | 1999-10-28 | 2000-10-11 | Richtantrieb |
Country Status (6)
Country | Link |
---|---|
US (2) | US6571678B1 (de) |
EP (1) | EP1096218B1 (de) |
AT (1) | ATE278172T1 (de) |
DE (2) | DE19951915A1 (de) |
ES (1) | ES2233267T3 (de) |
IL (1) | IL138978A (de) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001088564A1 (de) * | 2000-05-17 | 2001-11-22 | Diehl Munitionssysteme Gmbh & Co.Kg | Radareinrichtung für den objekt-selbstschutz |
FR2827950A1 (fr) * | 2001-07-20 | 2003-01-31 | Giat Ind Sa | Systeme de defense d'une cible comprenant un dispositif lanceur de projectiles |
WO2003064958A1 (de) * | 2002-02-01 | 2003-08-07 | Krauss-Maffei Wegmann Gmbh & Co.Kg | Richtanlage für einen raketenwerfer |
WO2004023058A1 (fr) * | 2002-09-05 | 2004-03-18 | Giat Industries | Systeme de defense d'une cible comprenant un dispositif lanceur de projectiles |
EP2157398A3 (de) * | 2008-08-21 | 2012-07-18 | Krauss-Maffei Wegmann GmbH & Co. KG | Gegenschussanlage |
ITTR20120010A1 (it) * | 2012-10-03 | 2014-04-04 | Lucci Ettore | Macchina per la movimentazione di armi di squadra e di reparto, da installare su veicoli militari e postazioni di controllo del territorio, elettronica e/o manuale |
US9891027B2 (en) | 2014-04-28 | 2018-02-13 | Rafael Advanced Defense Systems Ltd. | System and method for neutralizing shaped-charge threats |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6907812B1 (en) * | 2003-01-21 | 2005-06-21 | United Defense Lp | Pop-up weapon system |
DE10329861B3 (de) * | 2003-07-02 | 2005-01-13 | Moog Gmbh | Antriebsvorrichtung und Regelungsverfahren zum Ausrichten einer Waffe |
US7673552B2 (en) * | 2003-11-25 | 2010-03-09 | Kilgore Flares Company, Llc | Countermeasure system and method of using the same |
US6820531B1 (en) * | 2003-12-01 | 2004-11-23 | Textron Systems Corporation | Positioning system with continuous-range inclination and rotation angles |
DE102004017375B4 (de) * | 2004-04-08 | 2009-05-07 | Diehl Bgt Defence Gmbh & Co. Kg | System zum Schutze eines Zieles gegen angreifende Flugkörper |
US7555970B2 (en) * | 2004-09-22 | 2009-07-07 | Precision Remotes, Inc. | Rotating drive module with position locking mechanism |
DE102005059225B4 (de) * | 2005-12-12 | 2013-09-12 | Moog Gmbh | Waffe mit einem Waffenrohr, das außerhalb des Schwerpunkts auf einer bewegbaren Unterlage drehbar gelagert ist |
ITMI20060668A1 (it) * | 2006-04-05 | 2007-10-06 | Oto Melara Spa | Dispositivo ausiliario di puntamento |
DE102006050604B3 (de) * | 2006-10-26 | 2008-01-31 | Moog Gmbh | Richtantrieb für eine Waffe mit Differentialgetriebe |
DE102006057564B3 (de) | 2006-12-07 | 2008-08-14 | Diehl Bgt Defence Gmbh & Co. Kg | Werfer zur Selbstverteidigung eines mobilen oder stationären Objektes |
US7966763B1 (en) * | 2008-05-22 | 2011-06-28 | The United States Of America As Represented By The Secretary Of The Navy | Targeting system for a projectile launcher |
GB2475888A (en) * | 2009-12-04 | 2011-06-08 | Meritor Heavy Vehicle Sys Ltd | Differential lock actuator |
DE102011010902A1 (de) | 2011-02-10 | 2012-08-16 | Diehl Bgt Defence Gmbh & Co. Kg | Schutzsystem |
US8413569B1 (en) | 2011-09-28 | 2013-04-09 | The United States Of America As Represented By The Secretary Of The Navy | Parallel actuator gun mount |
ITUB20151137A1 (it) * | 2015-05-28 | 2016-11-28 | Oto Melara Spa | Sistema di supporto per arma da fuoco, in particolare destinato ad essere montato appeso ad una superficie superiore. |
CN106500543B (zh) * | 2016-10-27 | 2018-05-04 | 福州大学 | 抛投器载台及其使用方法 |
CN112815792B (zh) * | 2021-01-18 | 2023-02-28 | 中国人民解放军空军工程大学 | 一种地空导弹武器系统坐标转换模型 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3341320A1 (de) | 1983-11-15 | 1985-05-23 | Hoesch Ag, 4600 Dortmund | Steuerbarer drehantrieb |
EP0149639B1 (de) | 1983-06-22 | 1988-10-05 | AM General Corporation | Turmanlage für leichte militärfahrzeuge |
US5661254A (en) | 1994-07-22 | 1997-08-26 | Diehl Gmbh & Co. | System for protecting a target from missiles |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2088600A (en) * | 1934-11-09 | 1937-08-03 | James C Karnes | Position comparator |
US2370585A (en) * | 1941-05-08 | 1945-02-27 | Rose Brothers Ltd | Gun turret |
US2405678A (en) * | 1943-08-06 | 1946-08-13 | Electrolux Corp | Remote control system |
US3310998A (en) * | 1964-06-24 | 1967-03-28 | Wayne A Harmening | Scheme for preloading power gear trains |
US3401599A (en) * | 1966-05-25 | 1968-09-17 | Licentia Gmbh | Stabilizer |
US3429222A (en) * | 1968-04-08 | 1969-02-25 | Vapor Corp | Drive means for cupola of tank vehicle |
FR2221981A5 (de) * | 1973-03-14 | 1974-10-11 | France Etat | |
SE408475B (sv) * | 1974-10-18 | 1979-06-11 | Bofors Ab | Stridsvagn utrustad med grovkalibrigt eldvapen |
US4144797A (en) * | 1975-09-12 | 1979-03-20 | Ab Bofors | Device for a turret applied to a tank |
US4305325A (en) * | 1979-10-31 | 1981-12-15 | The United States Of America As Represented By The Secretary Of The Navy | General purpose decoy launcher |
US4302666A (en) * | 1979-11-13 | 1981-11-24 | The Boeing Company | Position control system of the discontinuous feedback type |
DE3108368C2 (de) * | 1981-03-05 | 1983-01-05 | Pietzsch, Ludwig, Dr.-Ing., 7500 Karlsruhe | Stabilisierungs- und Richtantrieb für einen Drehturm eines Fahrzeuges |
US4574685A (en) * | 1983-06-22 | 1986-03-11 | Am General Corporation | Turret system for lightweight military vehicle |
US4686888A (en) * | 1983-06-22 | 1987-08-18 | Am General Corporation | Turret system for lightweight military vehicle |
DE3436081A1 (de) * | 1984-10-02 | 1986-04-10 | Rheinmetall GmbH, 4000 Düsseldorf | Einrichtung zum horizontieren einer drehbaren waffenplattform |
DE3631206A1 (de) * | 1986-04-10 | 1987-10-15 | Salgad Int Ltd | Drehlagerung des sattels mit einer ein gschuetzrohr, vornehmlich ein werferrohr, aufnehmenden wiege |
DE19751305A1 (de) * | 1997-12-02 | 1999-06-10 | Krauss Maffei Ag | Lafette und Vorrichtung zum Ausrichten einer Lafette |
-
1999
- 1999-10-28 DE DE19951915A patent/DE19951915A1/de not_active Withdrawn
-
2000
- 2000-10-11 ES ES00122062T patent/ES2233267T3/es not_active Expired - Lifetime
- 2000-10-11 DE DE50007974T patent/DE50007974D1/de not_active Expired - Lifetime
- 2000-10-11 EP EP00122062A patent/EP1096218B1/de not_active Expired - Lifetime
- 2000-10-11 AT AT00122062T patent/ATE278172T1/de not_active IP Right Cessation
- 2000-10-12 IL IL13897800A patent/IL138978A/en not_active IP Right Cessation
- 2000-10-26 US US09/696,846 patent/US6571678B1/en not_active Expired - Lifetime
-
2003
- 2003-03-19 US US10/392,267 patent/US6715397B2/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0149639B1 (de) | 1983-06-22 | 1988-10-05 | AM General Corporation | Turmanlage für leichte militärfahrzeuge |
DE3341320A1 (de) | 1983-11-15 | 1985-05-23 | Hoesch Ag, 4600 Dortmund | Steuerbarer drehantrieb |
US5661254A (en) | 1994-07-22 | 1997-08-26 | Diehl Gmbh & Co. | System for protecting a target from missiles |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001088564A1 (de) * | 2000-05-17 | 2001-11-22 | Diehl Munitionssysteme Gmbh & Co.Kg | Radareinrichtung für den objekt-selbstschutz |
FR2827950A1 (fr) * | 2001-07-20 | 2003-01-31 | Giat Ind Sa | Systeme de defense d'une cible comprenant un dispositif lanceur de projectiles |
WO2003064958A1 (de) * | 2002-02-01 | 2003-08-07 | Krauss-Maffei Wegmann Gmbh & Co.Kg | Richtanlage für einen raketenwerfer |
WO2004023058A1 (fr) * | 2002-09-05 | 2004-03-18 | Giat Industries | Systeme de defense d'une cible comprenant un dispositif lanceur de projectiles |
US7150218B2 (en) | 2002-09-05 | 2006-12-19 | Giat Industries | Target defense system comprising a projectile launcher device |
EP2157398A3 (de) * | 2008-08-21 | 2012-07-18 | Krauss-Maffei Wegmann GmbH & Co. KG | Gegenschussanlage |
DE102008038603C5 (de) * | 2008-08-21 | 2018-04-19 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Gegenschussanlage |
ITTR20120010A1 (it) * | 2012-10-03 | 2014-04-04 | Lucci Ettore | Macchina per la movimentazione di armi di squadra e di reparto, da installare su veicoli militari e postazioni di controllo del territorio, elettronica e/o manuale |
US9891027B2 (en) | 2014-04-28 | 2018-02-13 | Rafael Advanced Defense Systems Ltd. | System and method for neutralizing shaped-charge threats |
Also Published As
Publication number | Publication date |
---|---|
IL138978A (en) | 2004-12-15 |
DE19951915A1 (de) | 2001-05-10 |
EP1096218A3 (de) | 2002-04-10 |
US6571678B1 (en) | 2003-06-03 |
ES2233267T3 (es) | 2005-06-16 |
US20030177897A1 (en) | 2003-09-25 |
US6715397B2 (en) | 2004-04-06 |
IL138978A0 (en) | 2001-11-25 |
EP1096218B1 (de) | 2004-09-29 |
ATE278172T1 (de) | 2004-10-15 |
DE50007974D1 (de) | 2004-11-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1096218B1 (de) | Richtantrieb | |
DE102006050604B3 (de) | Richtantrieb für eine Waffe mit Differentialgetriebe | |
DE2336040C3 (de) | Abwehrsystem mit mehreren Geschossen | |
EP1128152A2 (de) | An einem Kampffahrzeug angeordnete Wurfanlage für Nebelkerzen, Sprengkörper und dergleichen | |
DE102008038603C5 (de) | Gegenschussanlage | |
WO2011131183A1 (de) | Fahrzeug mit turmlafette, zusatzlafette und an zusatzlafette angeordnetem sichtgerät | |
DE60225047T3 (de) | Waffenvisier | |
EP0040871A2 (de) | Schiffsgeschütz zur Bekämpfung von Zielen in der Luft | |
EP1930685B1 (de) | Werfer zur Selbstverteidigung eines mobilen oder stationären Objektes | |
DE3342958C2 (de) | ||
DE102011106489B4 (de) | Lastträger für ein Fluggerät | |
DE2725414C2 (de) | Fliehkraftversteller zur Änderung des Zünd- bzw. Einspritzzeitpunktes bei Brennkraftmaschinen | |
DE102012002043C5 (de) | Waffenbasierte Schutzeinrichtung für Fahrzeuge | |
EP0387676B1 (de) | Elevationslagerung für eine in einem Panzerturm angeordnete grosskalibrige Rohrwaffe | |
DE1800330C3 (de) | Panzerfahrzeug mit Fliegerabwehrbewaffnung | |
DE2257679B2 (de) | Ladehilfe für Panzerkanonen | |
DE102004017375B4 (de) | System zum Schutze eines Zieles gegen angreifende Flugkörper | |
EP0392086B1 (de) | Flügelstabilisiertes Geschoss | |
AT396990B (de) | Richteinrichtung für einen granatwerfer | |
DE102022114729B3 (de) | Waffensystem | |
DE2446027A1 (de) | Selbstfahrlafette fuer artilleriegeschuetze | |
EP1739381B1 (de) | Lafettierung für ein Geschütz | |
EP0651223B1 (de) | Militärisches Fahrzeug | |
EP4227634A1 (de) | Lenkung drallender geschosse durch zyklischen stellflächenausschlag | |
DE102012001537B4 (de) | Anordnung eines Antriebs zur Kompensation von Rückstoßeffekten |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE Kind code of ref document: A2 Designated state(s): DE FR GB |
|
AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
RIC1 | Information provided on ipc code assigned before grant |
Free format text: 7F 41A 27/12 A, 7F 41A 27/22 B, 7F 41A 27/24 B, 7F 41A 27/28 B |
|
17P | Request for examination filed |
Effective date: 20020405 |
|
AKX | Designation fees paid |
Free format text: DE FR GB |
|
RBV | Designated contracting states (corrected) |
Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20040929 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20040929 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20040929 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20041011 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20041011 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20041031 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20041031 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: GERMAN |
|
REF | Corresponds to: |
Ref document number: 50007974 Country of ref document: DE Date of ref document: 20041104 Kind code of ref document: P |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20041229 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20041229 |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20050115 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: A. BRAUN, BRAUN, HERITIER, ESCHMANN AG PATENTANWAE Ref country code: CH Ref legal event code: PFA Owner name: DIEHL BGT DEFENCE GMBH & CO. KG Free format text: DIEHL MUNITIONSSYSTEME GMBH & CO. KG#FISCHBACHSTRASSE 16#90552 ROETHENBACH (DE) -TRANSFER TO- DIEHL BGT DEFENCE GMBH & CO. KG#FISCHBACHSTRASSE 16#90552 ROETHENBACH (DE) |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
BERE | Be: lapsed |
Owner name: DIEHL MUNITIONSSYSTEME G.M.B.H. & CO. KG Effective date: 20041031 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: PC2A |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2233267 Country of ref document: ES Kind code of ref document: T3 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
ET | Fr: translation filed | ||
26N | No opposition filed |
Effective date: 20050630 |
|
BERE | Be: lapsed |
Owner name: *DIEHL MUNITIONSSYSTEME G.M.B.H. & CO. K.G. Effective date: 20041031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20050228 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PFA Owner name: DIEHL BGT DEFENCE GMBH & CO. KG Free format text: DIEHL BGT DEFENCE GMBH & CO. KG#FISCHBACHSTRASSE 16#90552 ROETHENBACH (DE) -TRANSFER TO- DIEHL BGT DEFENCE GMBH & CO. KG#FISCHBACHSTRASSE 16#90552 ROETHENBACH (DE) |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PCAR Free format text: NEW ADDRESS: HOLBEINSTRASSE 36-38, 4051 BASEL (CH) |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20141021 Year of fee payment: 15 Ref country code: FR Payment date: 20141022 Year of fee payment: 15 Ref country code: CH Payment date: 20141021 Year of fee payment: 15 Ref country code: SE Payment date: 20141021 Year of fee payment: 15 Ref country code: ES Payment date: 20141028 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20141021 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20141028 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20141217 Year of fee payment: 15 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 50007974 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: EUG Ref country code: CH Ref legal event code: PL |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20151011 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MM Effective date: 20151101 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20160503 Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151011 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151031 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151011 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151031 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20160630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151012 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151102 Ref country code: NL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151101 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20161128 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151012 |