EP1721114A1 - Dispositif pour introduire des charges propulsives dans une arme lourde - Google Patents

Dispositif pour introduire des charges propulsives dans une arme lourde

Info

Publication number
EP1721114A1
EP1721114A1 EP05754726A EP05754726A EP1721114A1 EP 1721114 A1 EP1721114 A1 EP 1721114A1 EP 05754726 A EP05754726 A EP 05754726A EP 05754726 A EP05754726 A EP 05754726A EP 1721114 A1 EP1721114 A1 EP 1721114A1
Authority
EP
European Patent Office
Prior art keywords
propellant charge
propellant
modules
magazine
chain
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP05754726A
Other languages
German (de)
English (en)
Other versions
EP1721114B1 (fr
Inventor
Jens Grünewald
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 EP1721114A1 publication Critical patent/EP1721114A1/fr
Application granted granted Critical
Publication of EP1721114B1 publication Critical patent/EP1721114B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F41A9/01—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
    • F41A9/14—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging in a vertical plane which is transverse 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 invention relates to a device for supplying propellant charges to a heavy weapon with at least one propellant charge magazine and a propellant charge supply device, by means of which the propellant charges are removed from the propellant charge magazine and transferred to a propellant charge transfer arm which has a propellant charge supply shell with a propellant charge adapter which can be pivoted into the area behind the weapon ,
  • a device for supplying propellant charges to a heavy weapon with at least one propellant charge magazine and a propellant charge supply device, by means of which the propellant charges are removed from the propellant charge magazine and transferred to a propellant charge transfer arm which has a propellant charge supply shell with a propellant charge adapter which can be pivoted into the area behind the weapon ,
  • a propellant charge transfer arm which has a propellant charge supply shell with a propellant charge adapter which can be pivoted into the area behind the weapon ,
  • Such a device is basically known and described for example in DE 102 58 263.7 AI.
  • the invention has for its object to provide a device with the features specified in the preamble of claim 1, which is as compact as possible, so that the often limited interior space inside a tank tower or the turret housing of a shooting module is installed as little as possible and yet the fully automatic feeding of the propellant charges from the propellant charge magazine to the weapon is ensured.
  • the device should also be constructed in such a way that it is possible to arrange the propellant charge magazine and at least parts of the propellant charge supply device within an additional housing, which can be arranged on the outer wall of a tower housing in a removable or pivotable manner.
  • a basic idea of the invention is to design one or more propellant charge magazines as fixedly arranged magazines, in which the propellant charges are mounted in guides with horizontally oriented longitudinal axes, with several propellant charge modules being arranged axially one behind the other in each guide.
  • the guides are arranged parallel to each other and one above the other in horizontal planes.
  • an automatic propellant charge is arranged with a propellant charge chain encircling in a vertical plane, on which receptacle elements are arranged, the arrangement of the guides of the propellant charge magazine and the receptacle elements of the propellant charge machine being such that the receptacle elements in a position can be brought in which they are aligned with the guides so that the propellant charge modules can be transferred from the guides of the propellant charge magazine into the receiving elements of the propellant charge chain.
  • a portioning unit with means for transferring and joining a predetermined number of propellant charge modules from the receiving element into the portioning unit is provided axially to the uppermost receiving element of the automatic propellant charge. The joined propellant charge modules are then fed from the portioning unit to the propellant charge supply shell on the propellant charge transfer arm.
  • FIG. 1 is an isometric illustration of a propellant charge magazine with a propellant charge supply device consisting of an automatic propellant charge and a portioning unit;
  • Fig. 2 is a side view of the device of Fig. 1;
  • FIGS. 1 and 2A shows an individual illustration of an pick-up tube of the propellant charge magazine and a pick-up element of the propellant charge automat according to FIGS. 1 and 2 in an isometric illustration
  • FIG. 3A shows an individual representation of the automatic propellant charge according to FIGS. 1 and 2 in an isometric representation
  • 3B and 3C individual representations of receiving elements of the automatic propellant charge according to FIG. 3A;
  • FIG. 6 is an isometric illustration of a shooting module with an additional housing which can be pivoted away from the tower housing to accommodate a device for supplying propellant charges to a heavy weapon.
  • the propellant charge magazine 2 is designed as a fixedly arranged magazine in which propellant charge modules TM are mounted in guides 2.1 in such a way that their longitudinal axes run horizontally.
  • the guides 2.1 are designed as receiving tubes which are shown with a partially cut lateral surface for a clearer illustration.
  • other guides for example mounting rails, can also be used at this point.
  • a predetermined number of guides 2.1 are arranged parallel to one another and one above the other in horizontal planes.
  • an automatic propellant charge 3 is arranged with a propellant charge chain 3.1 rotating in a vertical plane and driven by a motor 3.11, with receiving elements 3.2 for receiving one or two propellant charge modules TM depending on the axial length.
  • the transfer of propellant charge modules TM from the receptacle tubes 2.1 into the receptacle elements 3.2 of the automatic propellant charge 3 can, if the receptacle elements are aligned with the receptacle tubes, by supplying excess air pressure via lines 2.2. During loading, air underpressure can be supplied via these lines to feed the propellant charge modules into the receiving tubes 2.1.
  • the supply and discharge of propellant charge modules can be carried out in a manner not shown by drivers guided on spindles or rotating chains.
  • Locking pawls can also be arranged on the guides 2.1 of the propellant charge magazine 2 in a manner also not shown.
  • the receiving elements 3.2 of the propellant charge chain 3.1 are designed as open shells, and each chain link has, in the area of the two ends of a shell, a circular ring section 3.31 and 3.32 which is in contact with one another and is connected at the point of contact
  • Bracket on The arrangement is such that one circular ring section 3.31 comprises the shell 3.2 of this chain link on the closed side and the other circular ring section 3.32 comprises the shell of an adjacent chain link on the open side.
  • Each bracket is constructed so that the openings of the circular ring sections 3.31 and 3.32 are at an angle of 90 ° to one another, and the holding brackets are arranged and guided in the propellant charge chain 3.1 such that the receiving element 3.2 standing in the removal position at the upper end of the propellant charge chain 3.1 is in the axial direction extending open lead-through area, through which a transfer element 6 designed as a gripping hook and displaceable in the axial direction can be passed such that the propellant charge modules contained in this pick-up element are transferred to a portioning unit 5 arranged above the propellant charge magazine 2 and are joined there.
  • the shells on the closed side and on the open side are completely encompassed by the interacting circular ring sections 3.31 and 3.32 of two holding brackets.
  • Sensor elements for determining the type of module and the degree of filling are arranged on each receiving element of the propellant charge chain 3.1.
  • the sensor elements are designed as spring strips 3.41 to 3.43 guided around the circumference of the shells 3.2, with a scanning element projecting through an opening in the shell, and each spring strip
  • 3.41 to 3.43 is assigned a proximity sensor or switch 3.51 to 3.53 on its outside, which is opposite the spring strip.
  • three spring strips 3.41 to 3.43 are arranged on each shell at a predetermined axial distance.
  • the length of the shells 3.2 is dimensioned such that either two axially successive standard modules TM 1 (FIG. 3B) or a somewhat longer basic module TM 2 (FIG. 3C) can be accommodated, in which case the sensor elements determine exactly can be what type and what number of propellant charge modules are contained in the shell.
  • some or all of the spring strips 3.41 to 3.43 are pressed out in the direction of the proximity switches 3.51 to 3.53.
  • the propellant charge chain 3.1 is driven by the drive motor 3.11 via a chain wheel 3.12. The deflection takes place in the upper area via a pinion 3.13. In the area of the removal position, further sensors for checking the transfer of the propellant charge modules from the receiving element 3.2 of the propellant charge chain 3.1 into the portioning unit 5 can be arranged.
  • the portioning unit 5 has a receiving shell arranged axially to the receiving element 3.2 of the propellant charge chain 3.1 in the removal position, divided in the axial direction, with a large shell portion 5.1, which has a stop 5.3 for the propellant charge modules at the end facing away from the propellant charge chain 3.1, and a small shell portion 5.2 for lateral support of the propellant charge modules.
  • the large shell part 5.1 can be pivoted from a receiving position into a delivery position for transferring the joined propellant charge modules TM to a propellant charge supply shell.
  • the stop 5.3 arranged at the end of the positioning unit 5 ensures that the propellant charge modules transferred from the gripping hook 6 into the portioning unit 5 are joined there before they are released.
  • Fig. 6 shows how the device described above can be arranged on the tower housing of a shooting module.
  • Fig. 6 shows a shooting module with an armored turret housing 1, in which a heavy weapon W is pivotally mounted in elevation in a manner not shown, about a shield pin.
  • the tower housing 1 can be rotatably supported in azimuth on a support structure, which can be designed, for example, as a chassis of a self-propelled howitzer or as a main battle tank.
  • the turret housing contains, in a manner that is not specifically shown and known, at least one projectile magazine from which projectiles are supplied to the weapon W by means of a fully automatic projectile supply device known per se.
  • an additional housing 4 is fastened on an outer wall 1.1, which is arranged within a recessed area 1.3 of the contour of the tower housing 1, so that it can pivot about a vertical axis such that, as can also be seen in FIG. 6, the additional housing 4 is made of one can be moved to the tower housing close position in a pivoted outward position.
  • the propellant charge magazine 2 and the propellant charge machine 3, with which the propellant charges are removed from the propellant charge magazine 2 and fed to the portioning unit 5, are arranged within the additional housing 4.
  • the additional housing 4 has, on the side facing the tower housing 1, a passage opening (not visible in FIG. 1), which is opposite a correspondingly designed passage opening 1.2 in the outer wall 1.1 of the tower housing 1.
  • the propellant charge is ejected through the through openings in the additional housing 4 and in the outer wall 1.1 of the tower housing 1.
  • the propellant charge is then received within the turret housing 1 by the propellant charge feed shell, which, not shown in FIG. 6, is arranged on the propellant charge transfer arm arranged in the turret housing 1 and can be pivoted into the area behind the weapon W, so that it can be pivoted by means of a at her arranged propellant charge gun can be supplied.
  • a propellant charge magazine 2 which has an automatic propellant charge 3 on one end face.
  • a propellant charge magazine can be arranged on both sides of the automatic propellant charge, and the portioning unit can be arranged above one of the two propellant charge magazines.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Elimination Of Static Electricity (AREA)
  • Warehouses Or Storage Devices (AREA)
  • Toys (AREA)
  • Cosmetics (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)

Abstract

L'invention concerne un dispositif pour introduire des charges propulsives dans une arme lourde dotée d'un chargeur (2) et d'un dispositif automatique (3) pour les charges propulsives, le dispositif automatique permettant d'extraire les charges propulsives du chargeur et de les amener dans une unité de répartition (5). Dans le chargeur (2) se trouve des modules de charges propulsives (TM) disposés dans des éléments de guidage les uns derrière les autres dans l'axe, de sorte que les axes longitudinaux sont horizontaux. Le dispositif automatique (3) est pourvu d'une chaîne de charges propulsive (3.1) rotative, elle-même dotée d'éléments de réception (3.2) pour les modules de charges propulsives, ainsi que de dispositifs pour le transfert des modules de charges propulsives hors des éléments de guidage du chargeur (2) dans les éléments de réception (3.2). En une position de prélèvement, à l'extrémité supérieure de la chaîne de charges propulsives (3.1) est disposée une unité de répartition (5) comprenant des moyens pour le transfert et l'assemblage d'un nombre prédéterminé de charges propulsives. En outre, des dispositifs servent à transférer les modules de charges propulsives assemblés de l'unité de prélèvement (5) à une enveloppe de guidage de charges propulsives.
EP05754726A 2004-05-26 2005-05-14 Dispositif pour introduire des charges propulsives dans une arme lourde Active EP1721114B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004025742A DE102004025742A1 (de) 2004-05-26 2004-05-26 Einrichtung zur Zuführung von Treibladungen zu einer schweren Waffe
PCT/DE2005/000888 WO2005116564A1 (fr) 2004-05-26 2005-05-14 Dispositif pour introduire des charges propulsives dans une arme lourde

Publications (2)

Publication Number Publication Date
EP1721114A1 true EP1721114A1 (fr) 2006-11-15
EP1721114B1 EP1721114B1 (fr) 2007-07-11

Family

ID=34971278

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05754726A Active EP1721114B1 (fr) 2004-05-26 2005-05-14 Dispositif pour introduire des charges propulsives dans une arme lourde

Country Status (9)

Country Link
US (1) US7475626B2 (fr)
EP (1) EP1721114B1 (fr)
AT (1) ATE366909T1 (fr)
CA (1) CA2567774C (fr)
DE (2) DE102004025742A1 (fr)
ES (1) ES2289714T3 (fr)
IL (1) IL179556A (fr)
NO (1) NO334270B1 (fr)
WO (1) WO2005116564A1 (fr)

Families Citing this family (11)

* 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
DE102005040407B4 (de) * 2005-08-26 2007-05-16 Rheinmetall Waffe Munition Vorrichtung zur Identifizierung des Munitionstyps einer Munition
SE534616C2 (sv) * 2009-10-21 2011-10-25 Bae Systems Bofors Ab Automatiserat laddningsmagasin
IT1404036B1 (it) * 2010-12-17 2013-11-08 Oto Melara Spa Veicolo armato con struttura migliorata.
KR101974079B1 (ko) * 2014-10-28 2019-04-30 한화디펜스 주식회사 장약 공급 장치
KR20210100434A (ko) 2020-02-06 2021-08-17 한화디펜스 주식회사 장약 공급 장치
EP4215865A1 (fr) 2022-01-19 2023-07-26 Krauss-Maffei Wegmann GmbH & Co. KG Magasin
DE102022101215A1 (de) 2022-01-19 2023-07-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Portioniervorrichtung
DE102022101219A1 (de) 2022-01-19 2023-07-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren zur Handhabung von Treibladungsmodulen
DE102022101216B3 (de) 2022-01-19 2023-04-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Vorrichtung zur Überführung von Treibladungsmodulen, Überführungsbaugruppe mit mindestens zwei Überführungsvorrichtungen, Magazin zur Aufnahme mehrerer Treibladungsmodule und/oder Treibladungsstangen und Verfahren zur Überführung von Treibladungsmodulen und/oder Treibladungsstangen
DE102022101213B3 (de) 2022-01-19 2023-06-15 Krauss-Maffei Wegmann Gmbh & Co. Kg Magazin

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Also Published As

Publication number Publication date
US7475626B2 (en) 2009-01-13
ES2289714T3 (es) 2008-02-01
IL179556A0 (en) 2007-05-15
US20080047417A1 (en) 2008-02-28
DE502005001021D1 (de) 2007-08-23
IL179556A (en) 2011-06-30
WO2005116564A1 (fr) 2005-12-08
NO20065698L (no) 2007-02-23
EP1721114B1 (fr) 2007-07-11
NO334270B1 (no) 2014-01-27
CA2567774C (fr) 2009-06-23
CA2567774A1 (fr) 2005-12-08
ATE366909T1 (de) 2007-08-15
DE102004025742A1 (de) 2005-12-22

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