EP2405227B1 - Dispositif de chargement et procédé de chargement d'une arme dotée d'une munition séparée et canon d'artillerie doté d'une arme et d'un dispositif de chargement - Google Patents

Dispositif de chargement et procédé de chargement d'une arme dotée d'une munition séparée et canon d'artillerie doté d'une arme et d'un dispositif de chargement Download PDF

Info

Publication number
EP2405227B1
EP2405227B1 EP11173097.4A EP11173097A EP2405227B1 EP 2405227 B1 EP2405227 B1 EP 2405227B1 EP 11173097 A EP11173097 A EP 11173097A EP 2405227 B1 EP2405227 B1 EP 2405227B1
Authority
EP
European Patent Office
Prior art keywords
weapon
loading device
loading
propellant charge
propellant
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
EP11173097.4A
Other languages
German (de)
English (en)
Other versions
EP2405227A3 (fr
EP2405227A2 (fr
Inventor
Matthias Raczek
Jens KÖSTER
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=44763677&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP2405227(B1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP2405227A2 publication Critical patent/EP2405227A2/fr
Publication of EP2405227A3 publication Critical patent/EP2405227A3/fr
Application granted granted Critical
Publication of EP2405227B1 publication Critical patent/EP2405227B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F41A9/37—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
    • F41A9/01—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
    • F41A9/38—Loading arrangements, i.e. for bringing the ammunition into the firing position
    • F41A9/39—Ramming arrangements
    • F41A9/42—Rammers separate from breech-block

Definitions

  • the invention relates to a loading device for loading a weapon with divided ammunition, with a Ansetz structure for attaching a projectile in its Ansetzwolf in the cargo space of the weapon. Further objects of the invention form a gun with a cargo space having weapon and a loading device for loading the weapon and a method for loading a weapon with a loading device.
  • Guns with larger caliber weapons such as artillery pieces, howitzers, etc.
  • split ammunition consisting of the actual projectile and the propellant charges ignitable to accelerate the projectile.
  • the projectile and the propellant charges are introduced separately into the cargo space of the weapon, so that the amount of propellant charge can be varied depending on the situation by the number of propellant charges used.
  • GB 2 065 841 A describes a loading device for such a weapon, which makes it possible to introduce projectile and propellant simultaneously in the cargo space of the weapon.
  • the projectile is first conveyed via a charging device, often referred to as a piecing device, into an attachment position in the cargo space of the weapon.
  • a charging device often referred to as a piecing device
  • the projectile is first moved to a position behind the weapon and then transported via a mounting surface of the piecing in the cargo space of the weapon.
  • the piecing is withdrawn from the cargo space and then arranged in a further step, the propellant charges behind the bullet.
  • the object of the invention is to improve a loading device, a gun and a method of the type mentioned in terms of robustness.
  • propellant charge recording By provided on the loader propellant charge recording, it is possible to simultaneously promote the propellant charges in the cargo space of the weapon when preparing a projectile.
  • propellant charge recording several propellant charges can be arranged, which are introduced when attaching the projectile in one step together with the projectile in the cargo space of the weapon, which can quickly alsmunition Schl the weapon and an increased cadence or fast shot sequence can be realized.
  • the attachment surface is arranged on an end face of the propellant charge receptacle.
  • the front side of the propellant charge receptacle can be aligned substantially transversely to the axis of the tube axis of the weapon and form a pressure surface for attaching the projectile.
  • the attachment surface is arranged on the front end side of the propellant charge receptacle viewed in the attachment direction.
  • the propellant charges are in a position close to that of the floor of the storey.
  • the attachment surface can also be designed such that it can be introduced for attachment of the projectile in its Ansetzwolf in the cargo space of the weapon. With a arranged on the front end of the propellant charge receiving surface, the introduction of the projectile into the cargo space of the weapon can be done in the manner of a plunger.
  • a further embodiment of the invention provides that the propellant charge receptacle is formed cup-shaped.
  • the propellant charges can be used from above into the propellant charge recording. Due to the shell shape, a defined position of the propellant charges in the propellant charge uptake can be achieved. In a receiving space extending along the inside of the propellant charge receptacle, the propellant charges can be absorbed.
  • the outer contour of the propellant charge receptacle has the shape of a circular arc.
  • the circular arc contour can be adapted to the inner contour of the cargo space of the weapon.
  • the adaptation may be selected such that substantially uniform gaps result between the outer contour and the inner contour in the end position of the charger device over its length.
  • the propellant charge can be configured as a part-cylindrical shell or partially cylindrical tube.
  • the inner contour of the propellant charge receptacle is preferably adapted to the outer contour of the propellant charge.
  • the adaptation can be selected such that the propellant charge lies flat against the inner contour of the propellant charge receptacle, resulting in a defined position of the propellant charge.
  • the inner contour of the propellant charge receptacle has the shape of a circular arc.
  • the radius of this circular arc can essentially correspond to the radius of the propellant charges.
  • the attachment surface is at least partially formed by a Ansetzriegel.
  • a movably hinged Ansetzriegel the frontal attachment surface can be increased.
  • the propellant charge can be opened by moving the Ansetzriegels to the cargo space of the weapon, so that the propellant charges can be transported from the propellant charge in the cargo space.
  • the Ansetzriegel can be used for attaching a projectile in its Ansetz too.
  • the one end of the Ansetzriegels pivotally connected via a hinge, in particular articulated on an end face of the propellant charge receptacle.
  • the hinge is arranged on the broad side of the crescent-shaped propellant charge recording.
  • the propellant charge receptacle comprises an abutment for pressure-resistant support of the other end of the Ansetzriegels.
  • the anvil is arranged on the narrow side of the crescent-shaped propellant charge recording.
  • the abutment on the propellant charge receptacle is arranged diametrically opposite the hinge. This results in a two-point bearing formed of hinge and abutment.
  • the loading device be configured in such a way that it can be inserted into the cargo space of the weapon for loading the weapon.
  • the propellant charges in the cargo space of the weapon By insertable into the cargo space of the weapon loading device, it is possible to promote the attachment of a projectile in one step, the propellant charges in the cargo space of the weapon.
  • the propellant charges For introducing the propellant charges, it is not necessary to first remove the charging device from the cargo space. Both the projectile and the propellant charges can be introduced almost simultaneously into the cargo space of the weapon, whereby an increased cadence can be realized.
  • the outer contour of the loading device is adapted to the inner contour of the cargo space.
  • the adjacent surfaces can slide along each other, whereby a guide of the charging device can be achieved within the cargo space, which ultimately results in improved reproducibility when preparing the projectile.
  • Such adapted to the inner contour of the cargo space loading device can by exploiting the have available space thicker outer walls, whereby the charging device can be made more stable and stiffer.
  • the gun has a retainer which is movable behind the receiving space of the propellant charge receptacle.
  • a retainer can be brought into the area behind the propellant charges, so that the propellant charges are kept within the cargo space of the weapon upon retraction of the loader from the cargo space via the retainer.
  • the retainer may be insertable into the cargo space of the weapon.
  • the retainer may also be movable in front of the loading-side end of the cargo space.
  • the retainer can also be formed by a closure wedge of the weapon, which is at least partially moved in front of the loading side end of the barrel.
  • the propellant charges are introduced into the cargo space together with the projectile during insertion of the charging device, an improved cadence can be achieved with such a method. It is not necessary to first remove a piecing from the cargo space of the weapon, only then to bring the propellant charges can. Rather, the propellants and the projectile can be introduced in one step.
  • the projectile and the propellant charges can be brought into the cargo space of the weapon virtually at the same time in one movement.
  • Particularly advantageous is a method in which the propellant charges are held on the retraction of the charging device from the cargo space on the retainer in the cargo space. Since the retainer holds only the propellant charges, but not the charging device, the propellant charges can be kept in the cargo space during retraction of the charging device from the cargo space. This results in a relative displacement of the propellant charges relative to the charger device.
  • the loading device can be pulled out of the charge space of the weapon under the propellant charges, while the propellant charges on the retainer rest snugly in the cargo space of the weapon.
  • the Ansetzriegel opens during retraction of the charging device from the cargo space by the held on the retainer propellant charges.
  • pulling out of the loading device from the cargo space of Ansetzriegel can be opened so that it rests flat against the wall of the cargo space of the weapon and can be pulled past the fixed on the retainer propellant charges.
  • the Ansetzriegel can automatically open during retraction of the loader from the cargo space of the weapon, it is further proposed that in the cargo space between the bottom of the projectile and the Ansetz constitutional the loading device, a free space is available, in which the Ansetzriegel can swing. In a further embodiment, it is proposed that the axial length of this clearance is at least equal to the length of the Ansetzriegels.
  • Fig. 1 shows a perspective view of a loading device 2 according to the invention for loading a weapon with divided ammunition consisting of a projectile 1 and a number of a total of six propellant charges 4 in the embodiment.
  • the loading device 2 consists of an attachment surface 3 for attachment of the projectile 1 and a building unit behind it arranged propellant charge recording 8, which will be discussed in detail below.
  • the attachment surface 3 is arranged on the front side of the propellant charge receptacle 8 and serves in the manner of a plunger for attaching the projectile 1 in its Ansetzwolf in the cargo space 10 of a weapon 11, see. also Fig. 8 , About the Ansetz constitutional 3 a Ansetz strig is applied to the bottom of the projectile 1 and the projectile 1 is transported in this way in its Ansetzwolf within the cargo space 10.
  • the Ansetz structure 3 is formed as a flat Ansetzriegel 9, which is hinged via a hinge 7 pivotally mounted on the end face of the propellant charge receptacle 8.
  • the propellant charge receiving 8 which has a receiving space for receiving one or more propellant charges 4 extends.
  • the receiving space of the propellant charge receptacle 8 is shown in the illustration Fig. 2 closed at the front over the Ansetzriegel 9. The rear end of the recording room is open.
  • the propellant charge receptacle 8 is designed in the manner of an upwardly open, partially cylindrical support shell, on the upper side of which the propellant charges 4 rest slidably in the axial direction.
  • the radius R of the outer contour of the propellant charge recording 8 is greater than the radius r of the inner contour or the bearing surface of the propellant charge receiving 8.
  • the circle centers of the outer contour and the inner contour are offset from each other, see. Fig. 3 , By this offset of the circle centers results in a sickle-shaped cross-section of the propellant charge recording 8 with a thicker material side and a weaker material side narrow side.
  • Ansetzriegel 9 is articulated freely pivotable on the thicker material side propellant charge 8.
  • the anvil 6 and the hinge 7 are located in a horizontal plane which extends through the center of the cross section of the propellant charge receiver 8.
  • the Ansetzriegel 9 extends in its closed position along a midpoint line from the hinge 7 on the circle center of the outer contour of the propellant charge receptacle 8 toward the anvil 6th
  • the Ansetzriegel 9 is of a total beam-shaped geometry and has a thickness which substantially corresponds to the thickness of the broad side of the propellant charge receiving 8. Therefore, the Ansetzriegel 9 can be pivoted so that it does not protrude in its open position in Ansetzraum over the broad side of the propellant charge recording 8. The Ansetzriegel 9 is hidden in its open position behind the material of the broadside.
  • the bearing surface of the propellant charge receiving 8 is adapted to the cylindrical geometry of the propellant charges 4, that they rest flat on the receiving surface.
  • the propellant charges 4 are positioned on the propellant charge receptacle 8 eccentric to the tube axis A of the weapon, cf. also Fig. 8 ,
  • the cargo space 10 widens along the axis of the pipe axis A in the direction of the loading-side end of the weapon 11. Accordingly, the pipe diameter D1 at a position inside the charge space 10 is smaller than the pipe diameter D2 in the region of the charge-side end of the charge space 10, cf. Fig. 8 , In order to be able to transfer high piecing forces, the cross section of the propellant charge receiver 8 follows this widening. As a result of this adaptation of the outer contour of the charging device 2 to the inner contour of the charge space 10, an increased compressive strength of the propellant charge receptacle 8 is achieved.
  • a gun with a weapon 11 which has a closable via a closure wedge 12 cargo space 10.
  • a projectile 1 and six propellant charges 4 can be seen.
  • the closure wedge 12 is in its closed position, in which it completely closes off the charge space 10 on the loading side, so that the projectile 1 can be fired.
  • the propellant charges 4 are introduced into the propellant charge receptacle 8 of the charging device 2.
  • the propellant charges 4 are inserted from above into the receiving space of the propellant charge receptacle 8, so that they rest on the support surface 13.
  • the propellant charges 4 may rest against the rear of the Ansetzriegels 9 or be arranged at a distance to this.
  • the projectile 1 is positioned in front of the attachment surface 3, in particular in front of the Ansetzriegel 9, the loading device 2. Subsequently, the loading device 2, including the propellant charge 4 received therein and the projectile 1 is moved to a position behind the cargo space 10, in which they are in axial alignment with the through the cargo space 10 extending bore A axis.
  • the loading device 2 for attaching the projectile 1 at high speed in the cargo space 10 of the weapon 11 is introduced.
  • the loading device 2 accelerates via the Ansetzriegel 9 the projectile 1 in the direction of its Ansetzwolf within the cargo space 10.
  • the loading device 2 is so far introduced into the cargo space of the weapon, that the propellant charges 4 are introduced into the cargo space 10 of the weapon 11.
  • the charging device 2 After attachment, the charging device 2 is removed from the cargo space 10, wherein both the projectile 1 and the propellant charges 4 remain in the cargo space. For this purpose, the charging device 2 is pulled out of the charge space 10 under the propellant charges 4. To prevent entrainment of resting on the propellant charge receiving 8 propellant charges 4, the propellant charges 4 are held by a retainer 12 in the cargo space 10.
  • the retainer 12 may, as in Fig. 7 represented by the shutter wedge of the weapon 11 are formed, which is moved before the withdrawal of the charging device 2 from the cargo space 10 in a position in which it at least partially closes the charging-side end of the cargo space 10.
  • the remaining opening of the cargo space 10 is dimensioned such that the charging device 2 can be removed through the opening from the cargo space, the propellant charges 4, however, held within the cargo space 10 become.
  • the propellant charges 4 can be held in place of the closure wedge 12 by a separate retainer in the cargo space 10 of the weapon 11.
  • the closure wedge 12 of the weapon 11 can be completely closed.
  • the closure wedge 12 can be transferred from the partially closed position for removing the loading device 2 from the loading space 10 into a completely closed position, in which it completely seals the loading-side end of the loading space 10.
  • This alsmunitiontechnische state of the weapon 11 is in Fig. 7 , shown.
  • the Ansetzriegel 9 is pivoted on retraction of the loading device 2 from the cargo space 10 by the pressure of the held on the retainer 12 propellant charges 4 on the inside of the Ansetzriegels 9 automatically.
  • the propellant charges 4 are held during retraction of the charging device 2 via the retainer 12 in the cargo space 10, resulting in a relative movement between the charging device 2 and the propellant charges 4 results.
  • the propellant charges 4 remain in the cargo space 10 and thereby pivot the Ansetzriegel 9.
  • Ansetzriegel 9 With fully swung Ansetzriegel 9 this is applied to the side of the wall of the cargo space 10 and the charging device 2 can be pulled out of the charge space 10 under the propellant charges 4 therethrough.
  • the thickness of the Ansetzriegels less than or equal to the thickness of the propellant charge receiver 8 on the side of the hinge 7. Therefore, the Ansetzriegel 9 as well as the propellant charge 8 between the propellant charge 4 and the inner contour of the charge space 10 from the charge space 10 to slide while the projectile 1 and the propellant charges 4 remain in their Ansetzwolf too in the cargo space 10.
  • the above-described shared ammunition loading apparatus, and the gun comprising this loading apparatus and the method for loading a weapon with this loading apparatus make it possible to set the projectile and the propellant charges in one movement. This allows a high firing frequency of the weapon. It is not necessary to first remove the loading device 2 used for attaching the projectile 1 from the cargo space 10, before the propellant charges can then be introduced, so that a rapid Aviationmunition Schl the weapon is possible.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Claims (15)

  1. Dispositif de chargement pour le chargement d'une arme (11) avec une munition en plusieurs pièces, avec une surface de pose (3) pour la pose d'un projectile (1) dans sa position de pose dans un espace de chargement (10) de l'arme (11) et un logement de charge propulsive (8) pour le logement d'une ou plusieurs charges propulsives (4), dans lequel la surface de pose (3) est formée au moins en partie par un verrou de pose (9) et l'une des extrémités du verrou de pose (9) étant articulée de manière à pouvoir pivoter au niveau d'un côté avant du logement de charge propulsive (8), caractérisé en ce que le logement de charge propulsive (8) comporte un contre-palier (6) pour l'appui résistant à la pression de l'autre extrémité du verrou de pose (9).
  2. Dispositif de chargement selon la revendication 1, caractérisé en ce que la surface de pose (3) est agencée sur un côté avant du logement de charge propulsive (8).
  3. Dispositif de chargement selon l'une quelconque des revendications précédentes, caractérisé en ce que le contour extérieur du logement de charge propulsive (8) présente la forme d'un arc de cercle.
  4. Dispositif de chargement selon l'une quelconque des revendications précédentes, caractérisé en ce que le contour intérieur du logement de charge propulsive (8) est adapté au contour extérieur de la charge propulsive (4) de telle manière que la charge propulsive (4) repose sur la surface du contour intérieur du logement de charge propulsive (8).
  5. Dispositif de chargement selon l'une quelconque des revendications précédentes, caractérisé en ce que le contour intérieur du logement de charge propulsive (8) présente la forme d'un arc de cercle.
  6. Dispositif de chargement selon les revendications 3 à 5, caractérisé en ce que les points médians circulaires du contour extérieur et intérieur sont agencés en déport l'un par rapport à l'autre de telle manière que la section transversale du logement de charge propulsive (8) soit en forme de croissant.
  7. Dispositif de chargement selon l'une quelconque des revendications précédentes, caractérisé en ce que l'une des extrémités du verrou de pose (9) est articulée par une charnière (7) de manière à pouvoir pivoter au niveau d'un côté avant du logement de charge propulsive (8).
  8. Dispositif de chargement selon la revendication 7, caractérisé en ce que le contre-palier (6) est agencé diamétralement en regard de la charnière (7).
  9. Canon avec une arme (11) présentant un espace de chargement (10) et un dispositif de chargement (2) selon l'une quelconque des revendications précédentes, caractérisé en ce que le dispositif de chargement (2) est configuré de telle manière que celui-ci puisse être introduit dans l'espace de chargement (10) de l'arme (11) pour le chargement de l'arme (11).
  10. Canon selon la revendication 9, caractérisé en ce que l'espace de chargement (10) s'élargit en direction de l'axe de l'âme du canon (A) de l'arme (11), le contour extérieur du dispositif de chargement (2) étant adapté à l'élargissement de l'arme (11).
  11. Canon selon l'une quelconque des revendications 9 à 10, caractérisé par un élément d'arrêt (12) qui est réalisé de manière mobile derrière l'espace de réception du logement de charge propulsive (8).
  12. Procédé de chargement d'une arme (11) avec un dispositif de chargement (2) selon l'une quelconque des revendications 1 à 8, caractérisé en ce que le dispositif de chargement (2) est introduit dans l'espace de chargement (10) de l'arme (11).
  13. Procédé selon la revendication 12, caractérisé en ce que les charges propulsives (4) sont introduites lors de la pose du projectile (1) dans l'espace de chargement (10).
  14. Procédé selon la revendication 13, caractérisé en ce que les charges propulsives (4) sont maintenues lors du retrait du dispositif de chargement (2) hors de l'espace de chargement (10) par un élément d'arrêt (12) dans l'espace de chargement (10).
  15. Procédé selon la revendication 14, caractérisé en ce que le verrou de pose (9) s'ouvre lors du retrait du dispositif de chargement (2) hors de l'espace de chargement (10) par les charges propulsives maintenues par l'élément d'arrêt (12).
EP11173097.4A 2010-07-08 2011-07-07 Dispositif de chargement et procédé de chargement d'une arme dotée d'une munition séparée et canon d'artillerie doté d'une arme et d'un dispositif de chargement Active EP2405227B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE201010017809 DE102010017809A1 (de) 2010-07-08 2010-07-08 Ladevorrichtung und Verfahren zum Laden einer Waffe mit geteilter Munition sowie Geschütz mit einer Waffe und einer Ladevorrichtung

Publications (3)

Publication Number Publication Date
EP2405227A2 EP2405227A2 (fr) 2012-01-11
EP2405227A3 EP2405227A3 (fr) 2015-03-04
EP2405227B1 true EP2405227B1 (fr) 2016-08-10

Family

ID=44763677

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11173097.4A Active EP2405227B1 (fr) 2010-07-08 2011-07-07 Dispositif de chargement et procédé de chargement d'une arme dotée d'une munition séparée et canon d'artillerie doté d'une arme et d'un dispositif de chargement

Country Status (3)

Country Link
EP (1) EP2405227B1 (fr)
DE (1) DE102010017809A1 (fr)
ES (1) ES2600884T3 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102020106157B4 (de) 2020-03-06 2021-11-04 Rheinmetall Waffe Munition Gmbh Vorrichtung zur Sicherung einer Munition oder Treibladung sowie Waffenanlage mit einer derartigen Vorrichtung

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB191015035A (en) 1910-06-22 1911-06-26 Mehmed Hooloossy Improvements in or relating to Ordnance Loading Mechanism.
GB262858A (en) 1925-09-16 1926-12-16 Beardmore William & Co Improvements in ramming devices employed in the loading of guns
GB308025A (en) 1928-01-30 1929-03-21 William Beardmore & Company Lt Improvements in loading arrangements for guns
FR931240A (fr) 1948-02-20
DE1578083A1 (de) 1967-05-13 1970-08-27 Bundesrep Deutschland Verfahren und Vorrichtung zur Zufuehrung mechanisch instabiler Treibladungen in den Ladungsraum von Geschuetzen
US4157678A (en) 1976-03-31 1979-06-12 Ab Bofors Rammer device
GB2065841A (en) 1979-12-18 1981-07-01 Bofors Ab Rammer head for a ramming unit of a firearm
DE3826350A1 (de) 1988-08-03 1990-03-08 Rheinmetall Gmbh Ansetzvorrichtung zum zufuehren von getrennt zu ladender munition
EP0419762B1 (fr) 1989-09-27 1993-06-30 Rheinmetall GmbH Outil pour porter des gargousses modulaires
EP0360776B1 (fr) 1988-09-21 1993-11-10 Ab Bofors Dispositif de chargement
EP0727635A1 (fr) 1995-02-16 1996-08-21 Giat Industries Dispositif d'aide au chargement d'un canon d'artillerie
DE69519935T2 (de) 1994-10-13 2001-06-07 Bofors Weapon Systems Ab Karls Ansetzer system
DE69807146T2 (de) 1997-05-29 2002-12-12 Giat Ind Sa Vorrichtung zum automatischen Greifen von Treibladungsmodulen aus einem Magazin

Patent Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR931240A (fr) 1948-02-20
GB191015035A (en) 1910-06-22 1911-06-26 Mehmed Hooloossy Improvements in or relating to Ordnance Loading Mechanism.
GB262858A (en) 1925-09-16 1926-12-16 Beardmore William & Co Improvements in ramming devices employed in the loading of guns
GB308025A (en) 1928-01-30 1929-03-21 William Beardmore & Company Lt Improvements in loading arrangements for guns
DE1578083A1 (de) 1967-05-13 1970-08-27 Bundesrep Deutschland Verfahren und Vorrichtung zur Zufuehrung mechanisch instabiler Treibladungen in den Ladungsraum von Geschuetzen
DE2713965C2 (fr) 1976-03-31 1989-07-20 Aktiebolaget Bofors, Bofors, Se
US4157678A (en) 1976-03-31 1979-06-12 Ab Bofors Rammer device
GB2065841A (en) 1979-12-18 1981-07-01 Bofors Ab Rammer head for a ramming unit of a firearm
DE3826350A1 (de) 1988-08-03 1990-03-08 Rheinmetall Gmbh Ansetzvorrichtung zum zufuehren von getrennt zu ladender munition
EP0360776B1 (fr) 1988-09-21 1993-11-10 Ab Bofors Dispositif de chargement
EP0419762B1 (fr) 1989-09-27 1993-06-30 Rheinmetall GmbH Outil pour porter des gargousses modulaires
DE69519935T2 (de) 1994-10-13 2001-06-07 Bofors Weapon Systems Ab Karls Ansetzer system
EP0727635A1 (fr) 1995-02-16 1996-08-21 Giat Industries Dispositif d'aide au chargement d'un canon d'artillerie
DE69605336T2 (de) 1995-02-16 2000-03-23 Giat Ind Sa Hilfsvorrichtung zur Ladung einer Artilleriekanone
DE69807146T2 (de) 1997-05-29 2002-12-12 Giat Ind Sa Vorrichtung zum automatischen Greifen von Treibladungsmodulen aus einem Magazin

Also Published As

Publication number Publication date
ES2600884T3 (es) 2017-02-13
DE102010017809A1 (de) 2012-01-12
EP2405227A3 (fr) 2015-03-04
EP2405227A2 (fr) 2012-01-11

Similar Documents

Publication Publication Date Title
DE1958925A1 (de) Patrone
DE2413615C3 (de) Handfeuerwaffe mit schwenkbarem VerschluBteU
DE3108783C2 (de) Auszieher für Schußwaffen
WO2012159623A2 (fr) Dispositif de chargement pour charger une arme, arme et procédé pour faire fonctionner une arme
DE2215398C3 (de) Lafettiertes Mehrrohrgeschütz
EP2405227B1 (fr) Dispositif de chargement et procédé de chargement d'une arme dotée d'une munition séparée et canon d'artillerie doté d'une arme et d'un dispositif de chargement
DE2152181C2 (de) Auszieher für hülsenlose Munition
DE1919245C3 (de) Brennkraftbolzensetzer
DE19644524A1 (de) Geschützturm für Panzerfahrzeuge
EP2715269B1 (fr) Tube à enficher pour la mise à feu de corps de munition sous-calibrés et arme comportant un tube à enficher
EP3607261B1 (fr) Dispositif pour charger une arme à canon avec des corps de munition
DE1099905B (de) Manoeverpatrone fuer Maschinenwaffen
CH626162A5 (en) Loading device, which is intended for loading a projectile or a propulsion charge, on a gun
WO1993018364A1 (fr) Procede et dispositif pour tirer des munitions sans douilles
DE1728019A1 (de) Munition zum Zuenden einer ueblichen Patrone fuer die geschlossene Kammerbauart in einem Verschluss der Bauart mit offener Kammer
EP1749181A1 (fr) Dispositif comprenant un bloc-culasse et un projectile entourant la charge propulsive et la charge d'amorçage
DE3009884A1 (de) Schusswaffe und verfahren zum schiessen mit derselben
EP2442062A2 (fr) Procédé et dispositif de fixation d'un projectile et d'une charge propulsive séparée du projectile dans la culasse d'une arme
DE2810613C1 (de) Handfeuerwaffe mit einem Patronenlager fuer eine huelsenlose Patrone und zu dieser Waffe gehoerende Patrone
DE10212313B4 (de) Selbstladewaffe
EP0149014B1 (fr) Ejecteur de douilles
DE3543728C2 (fr)
EP0530197A1 (fr) Ensemble complementaire pour armes a feu permettant de tirer des munitions de plus petit calibre, et procede de fabrication du canon inserable correspondant
DE3210128A1 (de) Laufkammer fuer ein geschuetz
DE3820943C1 (en) Shooting weapon

Legal Events

Date Code Title Description
AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

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

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

RIC1 Information provided on ipc code assigned before grant

Ipc: F41A 9/20 20060101ALI20150126BHEP

Ipc: F41A 9/42 20060101ALI20150126BHEP

Ipc: F41A 9/37 20060101AFI20150126BHEP

17P Request for examination filed

Effective date: 20150820

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20160225

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): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

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

Ref country code: AT

Ref legal event code: REF

Ref document number: 819451

Country of ref document: AT

Kind code of ref document: T

Effective date: 20160815

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502011010350

Country of ref document: DE

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20160810

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

Ref country code: RS

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: 20160810

Ref country code: IS

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: 20161210

Ref country code: LT

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: 20160810

Ref country code: NO

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: 20161110

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: 20160810

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: 20160810

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2600884

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20170213

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161212

Ref country code: PL

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: 20160810

Ref country code: LV

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: 20160810

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: 20161111

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: 20160810

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: 20160810

REG Reference to a national code

Ref country code: DE

Ref legal event code: R026

Ref document number: 502011010350

Country of ref document: DE

PLBI Opposition filed

Free format text: ORIGINAL CODE: 0009260

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

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: 20160810

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: 20160810

Ref country code: SM

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: 20160810

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: 20160810

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: 20161110

26 Opposition filed

Opponent name: RHEINMETALL WAFFE MUNITION GMBH

Effective date: 20170509

PLAX Notice of opposition and request to file observation + time limit sent

Free format text: ORIGINAL CODE: EPIDOSNOBS2

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 7

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: 20160810

PLBB Reply of patent proprietor to notice(s) of opposition received

Free format text: ORIGINAL CODE: EPIDOSNOBS3

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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 NON-PAYMENT OF DUE FEES

Effective date: 20170707

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20170731

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: 20170707

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 8

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: 20170731

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 819451

Country of ref document: AT

Kind code of ref document: T

Effective date: 20170707

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

Ref country code: MT

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: 20160810

REG Reference to a national code

Ref country code: DE

Ref legal event code: R100

Ref document number: 502011010350

Country of ref document: DE

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

Ref country code: AL

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: 20160810

PLCK Communication despatched that opposition was rejected

Free format text: ORIGINAL CODE: EPIDOSNREJ1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

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: 20170707

PLBN Opposition rejected

Free format text: ORIGINAL CODE: 0009273

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: OPPOSITION REJECTED

27O Opposition rejected

Effective date: 20181015

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

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; INVALID AB INITIO

Effective date: 20110707

Ref country code: MC

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: 20160810

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

Ref country code: CY

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

Effective date: 20160810

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

Ref country code: MK

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: 20160810

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: 20160810

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

Ref country code: HR

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: 20160810

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230517

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

Ref country code: IT

Payment date: 20230731

Year of fee payment: 13

Ref country code: GB

Payment date: 20230724

Year of fee payment: 13

Ref country code: ES

Payment date: 20230821

Year of fee payment: 13

Ref country code: CH

Payment date: 20230802

Year of fee payment: 13

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

Ref country code: SE

Payment date: 20230724

Year of fee payment: 13

Ref country code: FR

Payment date: 20230724

Year of fee payment: 13

Ref country code: DE

Payment date: 20230731

Year of fee payment: 13