EP3875882B1 - Vorrichtung zur sicherung einer munition oder treibladung sowie waffenanlage mit einer derartigen vorrichtung - Google Patents

Vorrichtung zur sicherung einer munition oder treibladung sowie waffenanlage mit einer derartigen vorrichtung Download PDF

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Publication number
EP3875882B1
EP3875882B1 EP21152302.2A EP21152302A EP3875882B1 EP 3875882 B1 EP3875882 B1 EP 3875882B1 EP 21152302 A EP21152302 A EP 21152302A EP 3875882 B1 EP3875882 B1 EP 3875882B1
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EP
European Patent Office
Prior art keywords
bracket
securing
propellant charge
bridge
charge
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.)
Active
Application number
EP21152302.2A
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German (de)
English (en)
French (fr)
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EP3875882A1 (de
Inventor
Jesko RABE
Klaus Lawitzke
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Waffe Munition GmbH
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Rheinmetall Waffe Munition GmbH
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Publication of EP3875882A1 publication Critical patent/EP3875882A1/de
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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
    • F41A9/37—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
    • F41A3/00—Breech mechanisms, e.g. locks
    • F41A3/02—Block action, i.e. the main breech opening movement being transverse to the barrel axis
    • F41A3/10—Block action, i.e. the main breech opening movement being transverse to the barrel axis with sliding breech-block, e.g. vertically
    • 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
    • F41A9/20—Movable ammunition carriers or loading trays, e.g. for feeding from magazines sliding, e.g. reciprocating
    • 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
    • F41A9/20—Movable ammunition carriers or loading trays, e.g. for feeding from magazines sliding, e.g. reciprocating
    • F41A9/22—Movable ammunition carriers or loading trays, e.g. for feeding from magazines sliding, e.g. reciprocating in a horizontal direction
    • 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
    • F41A9/38—Loading arrangements, i.e. for bringing the ammunition into the firing position
    • F41A9/39—Ramming arrangements
    • F41A9/42—Rammers separate from breech-block
    • 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
    • F42B5/38—Separately-loaded propellant charges, e.g. cartridge bags

Definitions

  • the invention relates to a device for securing or retaining, in particular, a propellant charge or a propellant charge module or propellant charge modules against falling out of a charge chamber of a weapon system.
  • the invention relates to a switchable device in particular, which can be used in the context of large-caliber guns in order to prevent the ammunition or parts thereof, such as a propellant charge or a propellant charge module or propellant charge modules, from accidentally falling out of the charge chamber when loading ammunition, in particular divided ammunition.
  • the invention also relates to a weapon system with the device.
  • Split ammunition is used in the field of large-caliber guns, especially artillery pieces.
  • This consists of a projectile and a row of propellant charge modules for variable acceleration of the projectile.
  • the projectile is placed in the transition between the charge chamber and the caliber part with a projectile rammer from behind through the charge chamber.
  • the required propellant charge modules are then fed into the charge chamber via a propellant charge rammer and deposited at a defined position. This position may be defined by a step at the rear of the cargo area.
  • the paragraph is intended to prevent the propellant charge from slipping backwards out of the not yet sealed charge space when the tube is raised positively.
  • a propellant charge delivery system which is part of a fully automatic firing module on a combat vehicle with a heavy weapon.
  • the basic idea here is to divide the process of moving the propellant charges into the propellant charge chamber into two sections by means of starting means and attachment means.
  • the disadvantage is that the propellant charges, which are sometimes introduced at high speed into the charge space, have problems with positioning, especially with large tube elevations, the problem being that the propellant charge(s) can fall out of the charge space to the rear after the application process and before the charge space is closed. Even a possible paragraph cannot always remedy this disadvantage.
  • the DE 10 2011 050 937 A1 relates to a loading device for loading a weapon with a feed slide movable in the direction of the bore axis of the weapon for conveying an ammunition body from a feed position into a firing position inside a charge chamber of the weapon.
  • the feed slide holding the ammunition body is designed to be movable in a second direction.
  • the feed slide is moved to the side by a closure element without the ammunition body losing its secure hold within the charge space, until this holding function has been taken over by the closure element moved in front of the charge space.
  • the closure element moves from above in the direction of the feed slide.
  • the closure element comes into contact with the feed slide on the top side, as a result of which it is moved downwards transversely to the direction of the tube core axis against the force of a spring.
  • the feed slide automatically springs back to its upper starting position.
  • a movably arranged retainer is provided on a feed slide, via which the propellant charges can be secured in position in their attached position.
  • the retainer is hinged to the feeder so that it can pivot and can be transferred from a folded-in feed position to an upright retention position.
  • the retainer is prestressed in particular by a spring in the direction of the folded-in delivery position.
  • the retainer is articulated on the feed slide so that it can be pivoted through an angle of more than 90° for the transfer from the feed position to the retention position.
  • the raising movement of the retainer takes place automatically when the feed pusher reaches a release element.
  • the erection movement is initiated in the end area of the feed path.
  • a rope can be used as a coupling element on the retainer.
  • the moving rope can be caught and stretched over a pulley.
  • the restraint can be set up by tensioning the rope.
  • the object of the invention is, in particular, to securely hold a propellant charge of an ammunition or an ammunition itself or to safely catch the falling propellant charge so that it cannot slip out of a charge chamber of a weapon system when the closure element is open.
  • the device according to the invention comprises at least one base plate and has at least one means running or adjustable perpendicularly to the base plate or to the axis of the tube core.
  • the means for securing the ammunition or propellant charge should be designed in such a way that it can at least partially cover or cover a charge space of a weapon system in order to prevent the propellant charge or one or more propellant charge modules from slipping out.
  • the means may resemble an i-, u- or v-shaped fork.
  • the means should have at least one, preferably at least two, protruding fingers or overhangs. Another sensible number of projections is also conceivable.
  • the agent can be guided through a profile in the bottom plate of the device.
  • the means can be pretensioned by at least one spring element of the device, here in a direction perpendicular to a tube core axis of the cargo space as a function of the device.
  • Preferred two spring elements are used.
  • the use of two spring elements supports a better effect of the remedy.
  • the spring elements are flat springs that can be rolled up.
  • conventional tension springs or gas springs can also be used.
  • the means is limited within the base plate, preferably in the profile, above and below.
  • the means can be secured by at least one catching device of the device. Securing can be done using a contour functionally associated with the means. This contour can hook or snap into at least one catching device.
  • Two capture devices are preferably used. These can be attached to the right and left of the base plate within the device.
  • the securing of the means within the at least one capture device can be sensed by at least one sensor and the sensing can be forwarded to a system computer.
  • the sensor can be an inductive sensor, for example. Alternative sensors are known.
  • the means is connected to a bridge.
  • the bridge includes at least one pin that functionally interacts with the at least one capture device.
  • the contour for securing the means can be arranged, which can hook or latch the means into the at least one catching device.
  • Two pins are preferred for the preferred two capture devices.
  • each arresting device has at least one holding bracket which can be displaced orthogonally relative to the means or the base plate and is preferably spring-loaded.
  • This sliding bracket can be held by a bracket holder and guided linearly.
  • a spring force acting on the holding bracket preferably acts in the direction of, alternatively counter to, a weapon barrel muzzle.
  • the spring-loaded retaining brackets should in turn be displaceable parallel to the axis of the tube core depending on the function of the device.
  • a counter-contour for the contour of the pin of the bridge is introduced on a front inner side of the respective holding bracket. A positive locking is achieved by the contour and the counter-contour.
  • the counter-contour can also be provided on a rear inner side of the respective holding bracket, which can then interact with the contour of the pin of the bridge and thus with the means.
  • the holding brackets can then be moved parallel to the axis of the barrel core but counter to the muzzle of the weapon barrel.
  • the form-fitting detent can also be designed as a force-fit detent. Magnets, for example, which can be separated from one another when attached to the bridge and to the retaining bracket, are ideal here.
  • the at least one capture device can be triggered at a specific point in time.
  • the triggering can be done by a triggering device.
  • the arrangement of the triggering device on the device is such that the displaceable retaining bracket is displaced by the triggering device to such an extent that the contour of the pin can emerge from the counter-contour (front inner side, rear inner side) and the detent to the center is canceled.
  • This allows the means, for example by the spring force of the at least one spring element in the base plate, to be moved from the lower starting position to a defined stop in the base plate or the profile in the direction of the core axis. In this defined end position, the means blocks the rear area of a cargo space. Any propellant charges that may slip back are caught by the means of the device. But a projectile can be secured with the inventive device.
  • the triggering device can be a cable, for example, which can move the retaining bracket or brackets against a spring force in the direction of the gun barrel muzzle or counter to this direction.
  • the expert can, for example, on the EP 2 898 281 B1 To fall back on.
  • a remotely controllable triggering device can also be used, as will be described below.
  • the inventive device can be embodied as a stand-alone construction.
  • a combination with a type of feed slide is also conceivable.
  • the triggering unit is to be brought into operation with the device in such a way that it can trigger the device and in particular the at least one catching device.
  • the means of the device can be reset by a type of spring element, which guides the means evenly downwards again, thus bringing the means into the defined starting position and thereby reestablishing the detent.
  • the spring element can then be relaxed again.
  • the device is in turn ready to be triggered again.
  • the device is intended to secure ammunition or a propellant charge in a charge space of a weapon system.
  • the above-described inventive device can also be permanently integrated into a weapon system in an advantageous manner.
  • the device is preferably located in the area of a tube base on the base piece of the weapon system.
  • the arrangement of the device can be provided depending on the type of closure element. In the case of a closure element in a base piece and a closure element falling linearly vertically downwards, the device should preferably be provided below the tube base, ie opposite the closure element.
  • Components of the device for partially closing a charge space of a gun barrel containing a propellant charge or propellant charge modules are preferably connected to the returning base piece.
  • a part that triggers the device can be connected to the (fixed) cradle.
  • the base plate of the device can in turn be firmly connected to the base piece of the weapon system.
  • the means is secured by at least one catching device.
  • the at least one catching device can be arranged under the floor piece. Two air-termination systems are also preferred here. These should be attached next to the base plate, for example on the right and left under the base piece.
  • each arresting device has a preferably spring-loaded holding bracket which can be displaced parallel to the axis of the tube core and which can be held and linearly guided by the bracket holder which can be mounted on the base piece.
  • a counter-contour for the contour of the pin of the bridge is introduced on a front inner side of the respective holding bracket. A positive locking is achieved by the contour and the counter-contour.
  • the counter-contour can also be provided on a rear inner side of the respective holding bracket, which can then interact with the contour of the pin of the bridge and thus with the means.
  • the holding brackets can be moved parallel to the axis of the barrel core but counter to the muzzle of the weapon barrel.
  • the form-fitting detent can also be designed as a force-fit detent.
  • Magnets that can be attached to the bridge and the retaining bracket(s) and separated from one another can be used here, for example.
  • the at least one capture device can be triggered at a specific point in time.
  • the device can be triggered by a triggering unit.
  • a controllable actuator which is itself preferably electrically controllable is preferred.
  • the actuator can be an electromechanical actuator, for example.
  • the actuator of the triggering device can preferably be fastened to a holding plate.
  • the retaining plate is preferably located below the base piece, preferably in front of the base plate.
  • the retaining plate can in turn be fixed to the cradle.
  • Functionally connected to the holding plate is an opening bracket which can engage the holding bracket of the at least one catching device and move it.
  • the opening bracket is limited and secured in its initial position by a mechanically movable connection to the actuator.
  • the opening clip is preferably pushed or displaced by the triggering device in the direction of the at least one retaining clip. This is not to be considered limiting. Rather, with an alternative triggering device, the opening clip can also be pulled by the triggering device, while retaining its function of moving the retaining clip(s).
  • the means By triggering the device via the at least one catching device, the means can be moved from the lower starting position to a defined stop in the direction of the inner tube axis, for example by the spring force of the at least one spring element within the at least one pocket of the base plate. In this defined end position, the means blocks the rear area of the cargo space. If an attachment is present, the blocking occurs beyond the attachment of the floor piece of the cargo hold. Any ammunition or propellant charge(s) that may slip back are caught by the means of the device.
  • the device can be (electrically) triggered again by the triggering device.
  • the triggering of the device in particular that of the at least one arresting device, can also take place in a different manner instead of an actuator.
  • a mechanism which is dependent on a movement of the weapon system and which activates the device and here in particular the at least one capture device would be possible.
  • the device is designed in such a way that the locking element can be moved without interference and can completely close the charge space with the ammunition or propellant charge contained therein.
  • the means can be pushed back into the lower starting position by the closing element moving downwards and secured in the position by the at least one catching device.
  • the at least one sensor can detect this position and the securing can be confirmed.
  • the advantage of such a device is that the ammunition or propellant charge is prevented from falling out after the loading process.
  • safe and trouble-free operation can be created.
  • a further advantage lies in the fact that the device can be triggered remotely.
  • the remote triggering of the arresting device(s) makes it possible to be able to set the triggering time of the device and in particular the arresting device(s) via the triggering device.
  • the loading of the weapon system and the triggering of the device can be precisely coordinated.
  • the construction of the device allows for a simple way of working.
  • the triggered device is brought back into the lower starting position by the locking wedge moving downwards.
  • the device is tensioned again and the agent is guided downwards evenly with the movement of the closure element.
  • the cargo space is permanently secured against propellant charges falling out.
  • the device also provides a sensor that confirms the secured lower starting position of the means and forwards it to a system control of the weapon system.
  • the device works independently of the elevation or an elevation angle of the weapon or weapon system.
  • a device for securing or retaining a propellant charge or ammunition in particular against falling out of a charge chamber of a weapon system is proposed and relates in particular to a switchable device which can be used in the context of large-calibre barrel weapons.
  • a weapon system with the device is also proposed.
  • the device is characterized by a base plate with a profile for guiding a medium, the base plate having upper and lower end stops. These define a travel path of the means.
  • the means can be connected to a bridge in such a way that the means can be displaced along the profile via the bridge.
  • the device On the underside of the bridge, the device has at least one pocket for receiving a spring element.
  • the spring element can be rolled up flat, be a tension spring or a gas spring.
  • At least one catching device is designed in such a way that the means can be secured in a lower position.
  • the bridge has at least one peg, with a contour or a magnet being able to be integrated or attached to the lower end of the peg.
  • the at least one catching device comprises a spring-loaded retaining bracket that can be displaced parallel to the axis of the pipe core, the retaining bracket being held by a bracket holder and guided linearly.
  • a counter-contour or a magnet is integrated or attached in a front inner side of the holding bracket.
  • a triggering unit of the device can be operated remotely, in particular electromechanically.
  • the device can be integrated into a weapon system.
  • the base plate of the device can be attached to the base part of the weapon system.
  • Other parts of the device, such as the safety catch, retaining bracket, bracket holder and the triggering device are also included in housed in the weapon system.
  • a remote-controlled triggering of the device within the weapon system is achieved.
  • a device is explained, preferably in combination with a weapon system.
  • the device can also be regarded as an independent assembly.
  • the functionality is the same as explained below.
  • a large-calibre weapon system 100 is shown in simplified form with a base piece 2, a locking element 3, here a locking wedge, a charge chamber 4 and a cradle 5.
  • the base piece 2 is connected to a rear end of a gun barrel 16.
  • the breech block 3, which is movable in the direction of the bore axis 9, is located in the bottom piece 2 to seal the charge chamber 4.
  • the gun barrel 16 is mounted radially in the cradle 5. When a shot is fired, the gun barrel 16 and thus also the base piece 2 can be displaced along the bore axis 9 up to a defined end position.
  • the gun barrel 16 has a shoulder 8 at the rear end.
  • the cradle 5 is pivotally connected through an elevation angle to a surrounding system, such as a turret.
  • the core of the invention is a device 1. Parts of the device 1 are partly connected to the returning base piece 2 and partly to the cradle 5.
  • a triggering device 31 for triggering the device 1 is arranged on the cradle 5 in a preferred embodiment.
  • the device 1 comprises at least one base plate 21, which has a linear profile 11 as a guide track(s) of a means 10.
  • the means 10 is connected to a bridge 20 in such a way that the means 10 can be displaced along the linear profile 11 via the bridge 20 .
  • the bridge 20 has at least one pin 24 . This can be integrated in the middle. This pin 24 interacts with at least one catching device 13 .
  • a contour 25 is introduced, which creates a form-fitting detent with a counter-contour of the catching device 13.
  • the catching device 13 has a parallel to the tube core axis 9 displaceable and preferably spring-loaded retaining clip 27, which is aligned with the pin 24 by a clip holder 28 mounted on the base piece 2 and can be guided linearly.
  • the spring force 30 acting on the retaining clip 27 acts in the direction of the muzzle of the weapon barrel.
  • a counter-contour to the contour 25 is introduced on the front inner side of the holding bracket 27 .
  • the two catching devices 13, 26 have spring-loaded retaining brackets 27 that can be displaced parallel to the tube core axis 9 and are held and linearly guided by two bracket holders 28, 29 mounted on the base piece 2.
  • the spring forces 30 acting on the retaining bracket 27 act in the direction of the muzzle of the weapon barrel.
  • the spring-loaded means 10 is held in the lower initial position with the aid of the contour 25 and the catch device(s) 13, 26 fitted under the base piece 2.
  • torsion spring-loaded rocker switch 19 pivotable about the axis 38 on the right bracket holder 29.
  • the rocker switch 19 is pressed by a front tip of the right bracket pin 24 in the upwardly pivoted position.
  • the right side of the rocker switch 19 is in the detection range of the sensor 15 mounted on the cradle 5, as a result of which a corresponding signal is passed on to a system controller, for example the weapon system 100.
  • the sensor 15 can be inductive in nature.
  • An electromechanical triggering unit 31 is located below the base piece 2 to trigger the displaceable retaining bracket(s) 27, a displacement counter to the direction of the gun barrel muzzle.
  • the task of the holding plate 18 is to receive an actuator 14 and to guide and hold an opener bracket 17, which can be displaced along the axis of the tube core, in its path.
  • the opening bracket 17 is loaded by the spring elements 38 prestressed in the direction of the gun barrel muzzle and is limited and secured in its initial position by a mechanically movable connection 32 to the actuator 14 .
  • FIG. 1 and 2 show the state of the weapon system 100 and the device 1 during the loading process after the projectile 6 has been placed in the caliber part of the gun barrel 16 and the propellant charge or the propellant charge modules 7 have been introduced into the charge chamber 4 by a propellant charge rammer (not shown in detail) and this has been moved out of the charge chamber 4 again.
  • the means 10, the bracket 27, the rocker switch 19 and the opening bracket 17 are in their prestressed and secured starting position.
  • the inductive sensor 15 is also actuated by the upwardly pivoted position of the switching rocker 19 and confirms to the system the lower initial position of the device 1.
  • the actuator 14 of the triggering unit 31 can now be controlled in order to generate a tensile force 33 directed parallel to the bore axis 9 and counter to the muzzle.
  • the tensile force 33 is passed on via the mechanically movable connection 32 to the opening bracket 17 that can be displaced along the axis 9 of the tube core. As a result, this is pressed in the direction of the two movable brackets 27, whereby these also move against their spring forces 30 up to the end stops of the two bracket holders 28, 29 after a certain distance ( 3 ).
  • the actuator 14 is deactivated again, as a result of which the tensile force 33 is eliminated and the spring force 38 moves the opening bracket 17 into its initial position.
  • This also has the effect that the front part of the opening clip 17 no longer presses against the two retaining clips 27 and the spring force 30 thus also moves the retaining clips 27 back into their starting positions.
  • the wedge 3 closes and moves back to its down position, closing the cargo space 4 by the wedge.
  • the two undersides 39 of the locking wedge 3 hit the two contact surfaces 36 on the left and right of the bridge 20, as a result of which these and thus also the connected means 10 are moved downwards ( Fig.4 ).
  • the two front contours 25 of the bridge pins 24 meet the matching counter-contour of the front inner sides of the holding bracket 27 .
  • the retaining brackets 27 are pushed a short distance against the spring force 30 until the two matching contours 25 of the bridge pins 24 and the counter-contours of the retaining brackets 27 engage and the retaining brackets 27 slip back in the direction of the spring force 30 in order to secure the means 10 in the lower initial position.
  • the weapon When a shot is fired, the weapon recoils, which accelerates the receding parts backwards.
  • these parts are the base plate 21 components attached to the base piece, together with means 10 and bridge 20, as well as the two arresting devices 13, 26 with the associated rocker switch 19.
  • the components of device 1 attached to the base piece 2 are arranged in such a way that they do not move when the shot is fired.
  • the components mounted on the cradle side, which include the entire triggering unit 31 with the opening bracket 17, the retaining plate 18 and the inductive sensor 15, are not accelerated by the weapon recoil.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
EP21152302.2A 2020-03-06 2021-01-19 Vorrichtung zur sicherung einer munition oder treibladung sowie waffenanlage mit einer derartigen vorrichtung Active EP3875882B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102020106157.9A DE102020106157B4 (de) 2020-03-06 2020-03-06 Vorrichtung zur Sicherung einer Munition oder Treibladung sowie Waffenanlage mit einer derartigen Vorrichtung

Publications (2)

Publication Number Publication Date
EP3875882A1 EP3875882A1 (de) 2021-09-08
EP3875882B1 true EP3875882B1 (de) 2023-07-26

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EP (1) EP3875882B1 (es)
DE (1) DE102020106157B4 (es)
DK (1) DK3875882T3 (es)
ES (1) ES2961317T3 (es)
HU (1) HUE064000T2 (es)
PL (1) PL3875882T3 (es)

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CH667719A5 (en) * 1985-10-23 1988-10-31 Oerlikon Buehrle Ag Weapon with wedge action breech block - uses pin sensing extraction groove on cartridge to release insertion arm and breech block
DE102005029413A1 (de) 2005-06-24 2006-12-28 Kraus-Maffei Wegmann Gmbh & Co. Kg Treibladungszuführungssystem
DE102010017809A1 (de) 2010-07-08 2012-01-12 Krauss-Maffei Wegmann Gmbh & Co. Kg Ladevorrichtung und Verfahren zum Laden einer Waffe mit geteilter Munition sowie Geschütz mit einer Waffe und einer Ladevorrichtung
DE102010038233A1 (de) 2010-10-15 2012-04-19 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren und Vorrichtung zum Ansetzen eines Geschosses und einer vom Geschoss getrennten Treibladung in den Ladungsraum einer Waffe
DE102011050637B4 (de) 2011-05-26 2019-10-31 Krauss-Maffei Wegmann Gmbh & Co. Kg Ladevorrichtung zum Laden einer Waffe, Waffe und Verfahren zum Betrieb einer Waffe
DE102011050937A1 (de) 2011-06-08 2012-12-13 ThyssenKrupp Fördertechnik GmbH Fördergurtanlage
DE102012108834A1 (de) 2012-09-19 2014-03-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Treibladungsansetzer, Waffe und Verfahren zum Ansetzen von Treibladungen

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DE102020106157A1 (de) 2021-09-09
ES2961317T3 (es) 2024-03-11
DK3875882T3 (da) 2023-10-23
EP3875882A1 (de) 2021-09-08
PL3875882T3 (pl) 2024-01-15
HUE064000T2 (hu) 2024-02-28

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