EP1483544B1 - Module de tir - Google Patents

Module de tir Download PDF

Info

Publication number
EP1483544B1
EP1483544B1 EP03767411A EP03767411A EP1483544B1 EP 1483544 B1 EP1483544 B1 EP 1483544B1 EP 03767411 A EP03767411 A EP 03767411A EP 03767411 A EP03767411 A EP 03767411A EP 1483544 B1 EP1483544 B1 EP 1483544B1
Authority
EP
European Patent Office
Prior art keywords
propellant charge
shell
weapon
propellant
magazine
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.)
Expired - Lifetime
Application number
EP03767411A
Other languages
German (de)
English (en)
Other versions
EP1483544A1 (fr
Inventor
Heinrich Heldmann
Michael Kohlstedt
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.)
Krauss Maffei Wegmann GmbH and Co KG
Original Assignee
Krauss Maffei Wegmann GmbH and Co KG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP1483544A1 publication Critical patent/EP1483544A1/fr
Application granted granted Critical
Publication of EP1483544B1 publication Critical patent/EP1483544B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/61—Magazines
    • F41A9/64—Magazines for unbelted ammunition
    • 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
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/01—Feeding of unbelted ammunition
    • F41A9/06—Feeding of unbelted ammunition using cyclically moving conveyors, i.e. conveyors having ammunition pusher or carrier elements which are emptied or disengaged from the ammunition during the return stroke
    • F41A9/09—Movable ammunition carriers or loading trays, e.g. for feeding from magazines
    • F41A9/10—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging
    • F41A9/13—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging in a vertical plane
    • F41A9/16—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging in a vertical plane which is parallel to the barrel axis
    • 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
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/37—Feeding two or more kinds of ammunition to the same gun; Feeding from two sides
    • F41A9/375—Feeding propellant charges and projectiles as separate units
    • 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
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/61—Magazines
    • F41A9/64—Magazines for unbelted ammunition
    • F41A9/76—Magazines having an endless-chain conveyor

Definitions

  • the present invention relates to a shooting module with a rotatably mounted in azimuth on a support structure housing in which a heavy weapon is pivotally mounted about a trunnion in elevation, wherein the weapon projectiles are fed by means of a fully automatic operating bullet feed device, which is pivotally mounted on a trunnion Geschoßübergabearm has, at its free end a provided with a loading tray bullet and is arranged from a raised position in which the loading tray is aligned with the Rohrselelenachse of the weapon, parallel to the elevation plane in a lowered position in which the charging tray is substantially vertical is aligned, as well as a Geschosentransporter with a transport arm having a gripping device at its free end, by means of each one In a bullet magazine, vertical and with the tip pointing upwards, the bullet is gripped and fed by the bullet transporter in the lowered position of the bullet transfer arm to the loading pallet.
  • Such a device is in a training as a tank howitzer in the European Patent EP 0 331 980 B1 described.
  • the housing is designed as a rotatable tower on which the heavy weapon is arranged.
  • the tower rests in azimuth rotatably on a support structure, which is designed as a tracked vehicle.
  • the projectile magazines are located in the known device below the pivot bearing in the vehicle pan of the carrier vehicle, and the projectiles are gripped by the Geschosentransporter and initially stored in a likewise arranged in the vehicle pan, initially horizontally aligned transport rail.
  • the transport rail moves the respective projectile linearly and rotates about the vertical axis to compensate for the different possible tower positions relative to the chassis.
  • the transport rail folds the lying floor in a vertical position and passes it into the charging tray of the piecing.
  • the bullet transfer arm is then swung up about the trunnion axis until the loading shell of the bullet attachment is aligned with the bore axis of the weapon.
  • the propellants are supplied in the known device by hand of the weapon.
  • the invention has the object of providing a shooting module of the type mentioned above in such a way that a considerable savings in space, especially height, and weight is achieved and further the bullet feed device is simplified in its construction.
  • the shooting operation should be fully automatic, so for example, from a command post outside the shooting module itself can be carried out, and the shooting module should be versatile, ie as a support structure should serve both a tracked vehicle and a wheeled vehicle for road or rail as well as a solid structure or even a ship.
  • the basic idea of the invention resides in arranging both the bullet magazines and the fully automatic bullet feed apparatus in the same housing above a rotary bearing, in which all the propellant charge magazines and also a fully automatic propellant charge supply apparatus are accommodated. In this case, there is a clear separation of the bullet magazines from the propellant charge magazines and the bullet feed device from the propellant charge supply device. This results in very short ways of transferring both the projectiles and the propellant charges to the weapon, which allows a high firing frequency.
  • the shooting module which is arranged above the pivot bearing.
  • the necessary in the known device transport rail is eliminated, whereby the bullet feed device is simplified and reduced in weight.
  • the bullet feed device has been supplemented by a fully automatic propellant charge supply device.
  • the inventive shooting module allows the separation of the gun operators of weapon, straightener, bullet feeder, propellant charge device and ammunition.
  • the existing in the known device ballistic protection structure can be limited to the protective volume of the staff and thus the command post.
  • the total weight of a gun consisting of a low-protection firing module and optimally protected command post can be brought to a weight while largely maintaining the other types of firing characteristics (firepower, range, cadence, automatic), allowing air transport with smaller and medium-sized transport aircraft.
  • the full automation also allows the reduction of operating personnel, which in turn leads to less risk to personnel in the case of operation and peacekeeping.
  • the number of personnel can be reduced to a minimum and the staff can be protected with an optimal ballistic protection structure. Furthermore, the total weight of the gun can be minimized.
  • the separation of personnel and shooting module in the form described allows new loader concepts, as previously reserved for the gun operator rooms can be used. It can be used for the electric drives higher voltages and thus weight and cost reductions and / or performance increases can be achieved. Furthermore, the cost of air conditioning and ABC protection ventilation is lower, since only a relatively small command state volume must be estimated. An improvement in the protection of the personnel is achieved by the spatial separation and foreclosure of the ammunition carried and by gunning and loading movements.
  • the shooting operation can be carried out fully automatically, and it is from a location outside the housing, so for example, a set up in the field command post or from the cab of a host vehicle, operable.
  • the propellant charge magazines and the propellant charge supply device can be configured such that different sized propellant charges are freely selectable and deliverable. A particularly fast availability of the propellant charges is achieved if, as described below, two independent propellant charge magazines and two propellant charge supply devices are arranged in the housing.
  • That in the Fig. 1 to 6 shown shooting module has a housing 1, which is rotatably mounted on a rotary bearing 2 in azimuth on the chassis of a trained as a chain motor vehicle carrier vehicle T.
  • a heavy weapon W is pivotally suspended about a trunnion 3 in elevation.
  • two ammunition magazines 4.1 and 4.2 are arranged on both sides of the longitudinal center axis L of the housing, in which projectiles 4.11 and 4.21 are arranged in a vertical position with pointing upwards tip.
  • the bullets are conveyed by means of a fully automatic bullet feed device into the area behind the weapon W.
  • This bullet feed device has a pivotable mounted on the trunnion 3 Geschoßübergabearm 5, at the rear free end of a charging tray 5.1 of a bullet tappet, not shown, is arranged.
  • the projectile transfer arm 5 can be pivoted parallel to the elevation plane into a lowered position from a raised position, not shown, in which the loading tray 5.1 is aligned flush with the pipe axis axis R of the weapon W, in the Fig. 1 and 3 can be seen and in which the charging tray is oriented substantially vertically, ie perpendicular to the housing bottom 1.1.
  • the charger 5.1 is like the Fig. 1 and 2 can be pivoted about a in the lowered position of the projectile transfer arm 5 vertically aligned pivot axis 5.3 by 180 ° between an opening to the area in front of the trunnion 3 receiving position and an opening to the area behind the trunnion 3 Abgabewolfwolfwolfwolf.
  • the bullet feed device further has a bullet transporter 6, which is arranged in the region between the bullet magazines 4.1 and 4.2.
  • the Geschosentransporter 6 has in a conventional manner a transport arm 6.1, which has at its free end equipped with two grippers gripping device 6.2, by means of each stored in one of the bullet magazines 4.1 and 4.2 projectile 4.11 or 4.21 and grabbed by the Geuntertransporter in the lowered position of the floor transfer arm 5 of the charging tray 5.1 is supplied.
  • the charging tray 5.1 is then around the Axis 5.3 swiveled by 180 °.
  • the projectile transfer arm 5 is pivoted up into the raised position and the projectile is fed to the gun W by means of the bullet tappet.
  • Fig. 1 to 6 are located in the area behind the trunnion 3 two propellant magazines 7.1 and 7.2, which are designed to receive modular propellant charges.
  • the propellant charge modules are arranged vertically one above the other in shafts 7.11, 7.12, 7.13, 7.14, 7.15 and 7.16, from which they are conveyed by non-specifically shown conveyors cyclically upwards and delivered at the top.
  • the propellant charges are conveyed by means of a fully automatic propellant charge supply device from the magazines to the weapon and this supplied.
  • the propellant charge supply device has in the illustrated embodiment, two propellant charge transfer arms 8.1 and 8.2, on each of which a propellant charge feed tray 8.11 and 8.21 is arranged.
  • the propellant charge supply shells are attached to the propellant charge transfer arm 8.1 and 8.2 arranged pivot arms 8.12 and 8.22.
  • the propellant charge modules at the top of the propellant charge magazines are fed to the propellant charge magazine towards pivoted position of the swing arm 8.12 or 8.22 of the propellant charge supply shell 8.11 or 8.21.
  • the respective pivoting arm 8.12 or 8.22 is then pivoted inwardly about an axis, which is possibly after a corresponding pivoting of the propellant charge transfer arm 8.1 or 8.2 parallel to Rohrseelenachse R of the weapon until the respective propellant charge supply - Fig.
  • the propellant charge modules are supplied to the cargo space of the weapon W by means of a not specifically illustrated propellant charge applicator, which may be formed, for example, as a back-rigid chain.
  • a propellant charge applicator which may be formed, for example, as a back-rigid chain.
  • a maximum of six propellant charge modules can be removed from each magazine for each shot, which are pushed together in the propellant charge supply tray and fed together.
  • the arrangement of two independent propellant magazines 7.1 and 7.2 and two propellant charge supply devices, a rapid deployment of the propellant charges behind the weapon is possible.
  • propellant charges of different lengths can be promoted and supplied.
  • the two propellant charge magazines 7.1 and 7.2 are firmly connected to the housing 1, serve the propellant charge transfer arms 8.1 and 8.2 for safe delivery in different elevation positions of the weapon W.
  • the shooting module described is extremely variable in terms of the arrangement and design of the bullet magazines and the propellant charge magazines.
  • Fig. 7 shows an embodiment in which the propellant charge magazines 17.1 and 17.2 again firmly arranged in the housing 1, but not as a shaft magazines but as tape magazines are formed. Again, the propellant charge modules are supplied to propellant charge trays 18.11 and 18.21, the can be swung in the manner already described from the field of propellant magazines behind the weapon behind. Otherwise, the embodiment is after Fig. 7 designed as well as the embodiment of the Fig. 1 to 6 ,
  • the Fig. 8 to 10 show an embodiment of the shooting module, in which the propellant charge magazines 27.1 and 27.2, which are formed as a shaft magazines, are not fixed to the housing 1, but firmly connected to the weapon W and thus accompany the pivotal movement of the weapon in the elevation.
  • the propellant charge modules which are supplied from the propellant charge magazines 27.1 and 27.2 the propellant charge supply shells 28.1 and 28.2, already arranged at the correct elevation angle and only by means of a device that the pivot arms 8.12 and 8.22 from Fig. 3 corresponds to need to be swung in behind the weapon. Propellant transfer arms are not required in this embodiment.
  • the propellant charges are instead fed from the propellant charge magazines 27.1 and 27.2 first respectively a Portionierstation 27.11 and 27.21 and then passed to the propellant charge trays 28.1 and 28.2 and there after pivoting by means of a propellant charge 28.3 the cargo space of the weapon W supplied.
  • Fig. 9 can be fed, depending on the shot to be prepared a different number of propellant charge modules are supplied.
  • the propellant charge tray 28.1 includes six propellant modules, while the propellant charge tray 28.2 contains only four propellant modules.
  • the propellant magazines 27.1 and 27.2 are initially conveyed in the direction of the arrow T1 into the portioning stations 27.11 and 27.21, respectively.
  • the pushing together of the propellant charge modules and possibly the mating to a propellant charge unit can be carried out by means of a displacement device already in the portioning station. This is in Fig. 9 for the portioning 27.21 shown with the displacement device 27.22.
  • the portioning 27.11 is equipped in an analogous manner.
  • the shooting module is after the Fig. 8 to 10 built in the same way as the shooting module after the Fig. 1 to 6 ,
  • the Fig. 11 and 12 show a shooting module, in which on the one hand the propellant charge magazines are fixed to the weapon as tape magazines 37.1 and 37.2 and on the other hand, a special, star-shaped arrangement of the projectile magazines 14 is present.
  • the propellant charge modules are supplied from the propellant charge magazines 37.1 and 37.2 via the portioning 37.11 and 37.21 the propellant charge trays 38.1 and 38.2, and these are pivoted in the manner already described inwardly behind the weapon by means of the pivot arms 9.1 and 9.2, where the propellant charge trays 38.1 and 38.2 are attached.
  • Fig. 12 The swiveling in of the propellant modules behind the weapon is over Fig. 12 to recognize.
  • Fig. 12 the swivel arm 9.1 is shown with the propellant charge supply shell 38.1 in both positions and in a receiving position in the region of the upper end of the propellant charge magazine 37.1 and in a delivery position behind the weapon W.
  • the propellant charge supply tray 28.1 moves in the direction of arrow S from the receiving position to the delivery position.
  • the embodiment of the Fig. 11 and 12 constructed in the same way as the embodiment according to Fig. 1 to 6 ,

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Gyroscopes (AREA)
  • Furnace Charging Or Discharging (AREA)
  • Inorganic Insulating Materials (AREA)

Claims (10)

  1. Module de tir comprenant un boîtier pouvant être monté sur une construction porteuse de façon rotative en azimut, dans lequel une arme lourde est montée de façon pivotante en élévation autour d'un tourillon, des projectiles étant amenés à l'arme au moyen d'un dispositif d'alimentation en projectiles entièrement automatique, qui présente un bras de transfert de projectile monté pivotant sur le tourillon, bras sur l'extrémité libre duquel est disposé un introducteur de projectile doté d'un plateau de chargement et qui peut basculer d'une position surélevée, dans laquelle le plateau de chargement est orienté en alignement avec l'axe de l'âme de tube de l'arme, parallèlement au plan d'élévation dans une position abaissée dans laquelle le plateau de chargement est orienté sensiblement verticalement, ainsi qu'un transporteur de projectile avec un bras de transport de projectile qui présente sur son extrémité libre un dispositif de préhension au moyen duquel à chaque fois un projectile monté verticalement dans un chargeur de projectile et logé avec la pointe dirigée vers le haut et est saisi et est amené par le transport de projectile dans la position abaissée du bras de transfert de projectile au plateau de chargement, caractérisé par les caractéristiques suivantes :
    a) dans le boîtier (1) sont disposés dans la zone située devant le tourillon (3) au moins un chargeur de projectile (4.1, 4.2) et le transporteur de projectile (6) ;
    b) le plateau de chargement (5.1) sur le bras de transfert de projectile (5) peut basculer autour d'un axe de pivotement (5.3) orienté sensiblement verticalement dans la position abaissée du bras de transfert de projectile d'au moins 180° entre une position de logement s'ouvrant en direction de la zone située devant le tourillon (3) et une position de remise s'ouvrant en direction de la zone située derrière le tourillon (3) ;
    c) dans le boîtier (1) est disposé dans la zone située à côté ou derrière le tourillon (3) au moins un chargeur de charge propulsive (7.1, 7.2 ; 17.1, 17.2 ; 27.1, 27.2 ; 37.1, 37.2) ;
    d) à l'arme (W) sont amenées des charges propulsives au moyen d'un dispositif d'alimentation en charges propulsives entièrement automatique disposé dans le boîtier (1), qui présente un plateau d'alimentation en charges propulsives (8.11, 8.21 ; 18.11, 18.21 ; 28.1, 28.2, 38.1, 38.2) pouvant basculer dans la zone située derrière l'arme (W) et en alignement avec l'axe de l'âme du tube (R) de l'arme avec un introducteur de charge propulsive.
  2. Module de tir selon la revendication 1, caractérisé en ce que le chargeur de charge propulsive (7.1, 7.2 ; 17.1, 17.2) est disposé de façon solidaire du boîtier et le dispositif d'alimentation en charges propulsives présente au moins un bras de transfert de charge propulsive (8.1, 8.2) monté pivotant sur le tourillon (3), bras sur l'extrémité libre duquel sont disposés le plateau d'alimentation en charges propulsives (8.11, 8.21 ; 18.11, 18.21) et l'introducteur de charge propulsive et qui peut être basculé à partir d'une position de logement, dans laquelle les charges propulsives peuvent être amenées à un plateau d'alimentation en charges propulsives, parallèlement au point d'élévation dans une position de remise, dans laquelle le plateau d'alimentation en charges propulsives (8.11, 8.21 ; 18.11, 18.21) peut basculer au moyen d'un bras pivotant (8.12, 8.22) dans un plan perpendiculaire à l'axe de l'âme du tube (R) de l'arme dans une position en alignement avec l'axe de l'âme du tube (R) de l'arme.
  3. Module de tir selon la revendication 1, caractérisé en ce que le chargeur de charge propulsive (27.1, 27.2 ; 37.1, 37.2) est disposé de façon solidaire de l'arme et le dispositif d'alimentation en charges propulsives présente un bras d'alimentation en charges propulsives (9.1, 9.2) pouvant basculer autour d'un axe parallèle à l'axe de l'âme du tube (R) de l'arme (W), bras sur l'extrémité libre duquel sont disposés le plateau d'alimentation en charges propulsives (28.1, 28.2 ; 38.1, 38.2) et l'introducteur de charge propulsive et qui peut être basculé d'une position de logement, dans laquelle des charges propulsives peuvent être amenées au plateau de chargement en charges propulsives, dans un plan perpendiculaire à l'axe de l'âme du tube (R) de l'arme (W) dans une position de remise dans laquelle le plateau d'alimentation en charges propulsives est disposé en alignement avec l'axe de l'âme du tube de l'arme.
  4. Module de tir selon la revendication 2 ou 3, caractérisé en ce que les chargeurs de charge propulsive (7.1, 7.2 ; 17.1, 17.2 ; 27.1, 27.2 ; 37.1, 37.2) sont réalisés pour le logement de charges propulsives modulaires et sont dotés de dispositifs pour la remise d'un nombre prédéfini de modules de charge propulsive pouvant être disposés les uns derrière les autres dans le plateau de charge propulsive.
  5. Module de tir selon l'une quelconque des revendications 1 à 4, caractérisé en ce que deux chargeurs de charges propulsives sont présents et un dispositif d'alimentation en charges propulsives est attribué à chaque chargeur de charge propulsive.
  6. Module de tir selon l'une quelconque des revendications 1 à 5, caractérisé en ce que le chargeur de charge propulsive est réalisé sous forme de chargeur à compartiment (7.1, 7.2 ; 17.1, 17.2 ; 27.1, 27.2), dans lequel les modules de charge propulsive sont disposés les uns au-dessus les autres dans des compartiments individuels (7.11 à 7.16) et peuvent être délivrés de façon cyclique à partir de chaque compartiment individuel.
  7. Module de tir selon l'une quelconque des revendications 1 à 5, caractérisé en ce que le chargeur de charge propulsive est réalisé sous forme de chargeur à bande rotatif, dans lequel les modules de charge propulsive sont logés sur des bandes individuelles tournantes et peuvent être délivrées de façon cyclique à partir de chaque bande.
  8. Module de tir selon l'une quelconque des revendications 1 à 7, caractérisé en ce que sur chaque chargeur de charge propulsive (27.1, 27.2) est disposée une station de fractionnement (27.11, 27.21), dans laquelle le nombre souhaité de modules de charge propulsive est délivré à partir du chargeur de charge propulsive et les modules de charge propulsive sont transférés de la station de fractionnement au plateau d'alimentation en charges propulsives.
  9. Module de tir selon la revendication 8, caractérisé en ce que, si l'on utilise des modules de charge propulsive emboîtables les uns dans les autres, le regroupement des modules de charge propulsive s'effectue à la station de fractionnement (27.11, 27.21).
  10. Module de tir selon l'une quelconque des revendications 1 à 9, caractérisé en ce que le dispositif d'alimentation en projectiles ainsi que le ou les dispositifs d'alimentation en charges propulsives présentent des dispositifs d'entraînement et de commande pouvant être actionnés automatiquement, lesquels peuvent être activés à partir d'un poste de commande situé à l'extérieur du boîtier.
EP03767411A 2002-12-13 2003-11-08 Module de tir Expired - Lifetime EP1483544B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10258263A DE10258263B4 (de) 2002-12-13 2002-12-13 Schießmodul
DE10258263 2002-12-13
PCT/DE2003/003708 WO2004055464A1 (fr) 2002-12-13 2003-11-08 Module de tir

Publications (2)

Publication Number Publication Date
EP1483544A1 EP1483544A1 (fr) 2004-12-08
EP1483544B1 true EP1483544B1 (fr) 2008-04-16

Family

ID=32477608

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03767411A Expired - Lifetime EP1483544B1 (fr) 2002-12-13 2003-11-08 Module de tir

Country Status (7)

Country Link
US (1) US7159504B2 (fr)
EP (1) EP1483544B1 (fr)
AT (1) ATE392596T1 (fr)
DE (2) DE10258263B4 (fr)
ES (1) ES2304533T3 (fr)
WO (1) WO2004055464A1 (fr)
ZA (1) ZA200408183B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012108832A1 (de) 2012-09-19 2014-03-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Treibladungsansetzer, Waffe und Verfahren zum Ansetzen von Treibladungen

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004024302B4 (de) * 2004-05-15 2008-04-10 Kraus-Maffei Wegmann Gmbh & Co. Kg Gurtkasten für eine lafettierte Granatmaschinenwaffe
DE102004025742A1 (de) 2004-05-26 2005-12-22 Krauss-Maffei Wegmann Gmbh & Co. Kg Einrichtung zur Zuführung von Treibladungen zu einer schweren Waffe
DE102004025743A1 (de) * 2004-05-26 2005-12-15 Krauss-Maffei Wegmann Gmbh & Co. Kg Schießmodul
DE102005029413A1 (de) * 2005-06-24 2006-12-28 Kraus-Maffei Wegmann Gmbh & Co. Kg Treibladungszuführungssystem
DE102006021135B4 (de) * 2006-05-04 2008-02-28 Krauss-Maffei Wegmann Gmbh & Co. Kg Kampfeinrichtung mit einem auf einer mit Rädern versehenen Trägerkonstruktion angeordneten Geschütz
DE102006041602B8 (de) * 2006-09-05 2008-05-29 Krauss-Maffei Wegmann Gmbh & Co. Kg In ein militärisches Schiff integriertes, großkalibriges Geschütz
IT1404036B1 (it) * 2010-12-17 2013-11-08 Oto Melara Spa Veicolo armato con struttura migliorata.
DE102011050537B3 (de) 2011-05-20 2012-10-25 Krauss-Maffei Wegmann Gmbh & Co. Kg Geschütz und militärisches Fahrzeug
KR101974079B1 (ko) 2014-10-28 2019-04-30 한화디펜스 주식회사 장약 공급 장치
DE102018109154A1 (de) * 2018-04-17 2019-10-17 Rheinmetall Waffe Munition Gmbh Autolader sowie Fahrzeug mit einem Autolader
RU2707476C1 (ru) * 2018-11-06 2019-11-26 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Система питания автоматической пушки
WO2022162684A1 (fr) * 2021-01-28 2022-08-04 Chairman, Defence Research And Development Organisation (DRDO) Chargeur de projectiles automatisé et procédé de chargement de projectiles pour véhicule
DE102022101219A1 (de) * 2022-01-19 2023-07-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren zur Handhabung von Treibladungsmodulen
EP4215865A1 (fr) * 2022-01-19 2023-07-26 Krauss-Maffei Wegmann GmbH & Co. KG Magasin
DE102022101213B3 (de) * 2022-01-19 2023-06-15 Krauss-Maffei Wegmann Gmbh & Co. Kg Magazin

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3437588A1 (de) * 1984-10-13 1986-04-24 Rheinmetall GmbH, 4000 Düsseldorf Ladeeinrichtung fuer geschuetze
DE3627042A1 (de) * 1986-08-09 1988-02-11 Kuka Wehrtechnik Gmbh Vorrichtung zum laden von geschuetzen, insbesondere panzerhaubitzen
DE3725762A1 (de) * 1987-08-04 1989-02-16 Rheinmetall Gmbh Gepanzertes kampfgeraet und versorgungswagen hierfuer
DE3807474A1 (de) * 1988-03-08 1989-09-21 Wegmann & Co Kampffahrzeug, insbesondere panzerhaubitze
DE4007425A1 (de) * 1990-03-09 1991-09-12 Kuka Wehrtechnik Gmbh Vorrichtung zum laden von geschuetzen, insbesondere panzerhaubitzen
SE9900152L (sv) * 1999-01-20 2000-06-19 Bofors Weapon Sys Ab Sätt och anordning för att hantera artillerigranater vid laddning av artilleripjäser
SE520361C2 (sv) * 2001-12-05 2003-07-01 Alvis Haegglunds Ab Anordning för överföring av grovkalibrig ammunition från ett ammunitionsmagasin till ett laddläge vid ett grovkalibrigt vapen
US6752063B2 (en) * 2002-10-31 2004-06-22 United Defense, L.P. Multiple cell ammunition cradle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012108832A1 (de) 2012-09-19 2014-03-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Treibladungsansetzer, Waffe und Verfahren zum Ansetzen von Treibladungen
WO2014044255A1 (fr) 2012-09-19 2014-03-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Refouloir pour charges propulsives, arme et procédé de mise en place de charges propulsives

Also Published As

Publication number Publication date
WO2004055464A1 (fr) 2004-07-01
WO2004055464A9 (fr) 2004-11-25
DE10258263B4 (de) 2006-01-19
ES2304533T3 (es) 2008-10-16
US20060162541A1 (en) 2006-07-27
US7159504B2 (en) 2007-01-09
DE50309631D1 (de) 2008-05-29
EP1483544A1 (fr) 2004-12-08
DE10258263A1 (de) 2004-07-08
ZA200408183B (en) 2005-11-30
ATE392596T1 (de) 2008-05-15

Similar Documents

Publication Publication Date Title
EP1483544B1 (fr) Module de tir
EP0331980B1 (fr) Véhicule de combat, en particulier canon blindé
EP1421327B1 (fr) Canon d'artillerie comprenant une arme lourde montee sur un vehicule de soutien
EP0178484B1 (fr) Chargeur pour canons
EP1061323A2 (fr) Véhicule blindé pour le transport de soldats
EP0141900B1 (fr) Dispositif de chargement automatique pour engin blindé avec tourelle rotative blindée
EP1898172B1 (fr) Canon naval à gros calibre
DE3642920C2 (de) Ladevorrichtung für ein Kampffahrzeug, insbesondere eine Panzerhaubitze
DE3702603C2 (fr)
EP0557751B1 (fr) Obusier blindé comportant un bras de chargement pivotant et un magasin pour munitions du type à chaîne sans fin
EP0042166B1 (fr) Char comportant un système d'échange de container à munitions
DE69206698T2 (de) Automatische Munitionszuführvorrichtung für Panzerkanonen
DE102004025743A1 (de) Schießmodul
DE102004063882B4 (de) Vorrichtung zur Halterung einer Waffenstation
DE19717734A1 (de) Kampffahrzeug
DE1578069C3 (de) Zubringvorrichtung in Form einer im Inneren eines gepanzerten Fahrzeuges drehbar angeordneten Magazintrommel für eine Abschußvorrichtung für Flugkörper mit Rückstoßantrieb
DE10160207B4 (de) Munitionsmagazin
EP0635695B1 (fr) Véhicule de combat, en particulier obusier, comportant des magasins de munitions
EP3267141A1 (fr) Arme
DE2852699C1 (de) Einrichtung fuer die Munitionszufuhr aus einem unterhalb einer drehbaren Plattform befindlichen Magazin zu einem auf der Plattform angeordneten scheitellafettierten Geschuetz
DE4123338A1 (de) Kampfpanzerturm
DE4134603B4 (de) Geschützturm
DE3341875A1 (de) Vorrichtung zum laden von munition
EP1273869B1 (fr) Véhicule blindé
EP0710812B1 (fr) Dispositif d'alimentation en munitions pour obusiers blindés

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

17P Request for examination filed

Effective date: 20041004

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

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 BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REF Corresponds to:

Ref document number: 50309631

Country of ref document: DE

Date of ref document: 20080529

Kind code of ref document: P

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: BOHEST AG

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

ET Fr: translation filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

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: 20080416

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2304533

Country of ref document: ES

Kind code of ref document: T3

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

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: 20080716

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: 20080416

Ref country code: NL

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: 20080416

Ref country code: PT

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: 20080916

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CZ

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: 20080416

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: 20080416

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: 20080416

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

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

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: 20080416

Ref country code: SK

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: 20080416

26N No opposition filed

Effective date: 20090119

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

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: 20080416

BERE Be: lapsed

Owner name: KRAUSS-MAFFEI WEGMANN G.M.B.H. & CO. KG

Effective date: 20081130

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: 20081130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20081130

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: 20080416

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: 20081108

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20081108

Ref country code: HU

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: 20081017

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

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: 20080416

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: 20080717

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)

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 13

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 14

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

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: 20211130

Year of fee payment: 19

Ref country code: SE

Payment date: 20211123

Year of fee payment: 19

Ref country code: GB

Payment date: 20211123

Year of fee payment: 19

Ref country code: ES

Payment date: 20211216

Year of fee payment: 19

Ref country code: FR

Payment date: 20211119

Year of fee payment: 19

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20211130

Year of fee payment: 19

Ref country code: CH

Payment date: 20211123

Year of fee payment: 19

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 50309631

Country of ref document: DE

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20221108

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221130

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221130

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: 20221109

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221108

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221108

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230601

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221130

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20231228

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: 20221109

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: 20221109