EP1721114B1 - Dispositif pour introduire des charges propulsives dans une arme lourde - Google Patents

Dispositif pour introduire des charges propulsives dans une arme lourde Download PDF

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Publication number
EP1721114B1
EP1721114B1 EP05754726A EP05754726A EP1721114B1 EP 1721114 B1 EP1721114 B1 EP 1721114B1 EP 05754726 A EP05754726 A EP 05754726A EP 05754726 A EP05754726 A EP 05754726A EP 1721114 B1 EP1721114 B1 EP 1721114B1
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EP
European Patent Office
Prior art keywords
propelling
charge
propellant charge
modules
magazine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP05754726A
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German (de)
English (en)
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EP1721114A1 (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
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Publication of EP1721114A1 publication Critical patent/EP1721114A1/fr
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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
    • F41A9/01—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 amaschineiadungsübergabearm having a einschwenkbare in the area behind the weapon propellant charge tray with a propellant charge ,
  • 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 amaschineiadungsübergabearm having a einschwenkbare in the area behind the weapon propellant charge tray with a propellant charge
  • Such a device is basically known and, for example, in DE 102 58 263.7 A1 described.
  • the invention has for its object to provide a device with the features specified in the preamble of claim 1, which is constructed as compact as possible, so that the often limited space inside a turret or the tower housing of a shooting module is installed as little as possible and yet the fully automatic supply of the propellant charges from the propellant charge magazine to the weapon is ensured.
  • the device should furthermore be constructed so 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 removably or swingably on the outer wall of a tower housing.
  • a basic idea of the invention is to design one or more propellant charge magazines as permanently arranged magazines in which the propellant charges are mounted in guides with horizontally aligned longitudinal axes, wherein in each guide several propellant charge modules are arranged axially one behind the other.
  • the guides are each arranged parallel to each other and in horizontal planes one above the other.
  • a propellant charge machine is arranged with a revolving in a vertical plane propellant charge chain, are arranged on the receiving elements, the arrangement of the guides of the propellant charge magazine and the receiving elements of the propellant charge machine is such that the receiving 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 in 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 respective uppermost receiving element of the propellant charge device. From the portioning unit, the joined propellant charge modules are then fed to the propellant charge feed tray at the propellant charge transfer arm.
  • FIGS. 1 to 5 show an embodiment of a device with a propellant charge magazine and a part of the propellant charge supply device consisting of a propellant charge automaton and a portioning unit.
  • the propellant charge magazine 2 is designed as a permanently arranged magazine in which propellant charge modules TM are mounted in guides 2.1 such that their longitudinal axes are horizontal.
  • the guides 2.1 are formed in the illustrated embodiment as receiving tubes, which are shown for clarity of view with partially cut lateral surface. However, other guides, for example receiving rails, can also be used at this point. As can be seen from FIGS. 1 and 2, a predetermined number of guides 2.1 are arranged one above the other parallel to one another and in horizontal planes.
  • a propellant charge machine 3 On a front side of the thus formed propellant charge magazine 2, a propellant charge machine 3 is arranged with a circulating in a vertical plane, driven by a motor 3.11 propellant charge chain 3.1 with receiving elements 3.2 for each recording of depending on the axial length of one or two propellant charge modules TM.
  • the supply and discharge of propellant charge modules in a manner not shown can be done by guided on spindles or circulating chains driver.
  • locking notches can also be arranged in a manner not shown.
  • the receiving elements 3.2 of the propellant charge chain 3.1 are formed as open shells, and each chain link has in each case in the region of the two ends of a shell on one of two contacting and interconnected at the contact point circular ring sections 3.31 and 3.32 built-on headband.
  • the arrangement is such that in each case 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 headband is constructed in this way that the openings of the circular ring sections 3.31 and 3.32 are at an angle of 90 ° to each other, and the headband are arranged and guided in the propellant charge chain 3.1 so that each standing in the removal position at the upper end of the propellant charge chain 3.1 receiving element 3.2 in the axial direction having extending open feedthrough area, through which a displaceable in the axial direction, designed as a gripping hook transfer element 6 can be passed in such a way that the propellant charge modules contained in this receiving element transferred into a above the propellant charge magazine 2 portioning unit 5 and joined there.
  • the shells are completely enclosed on the closed and on the open side by the cooperating circular ring sections 3.31 and 3.32 of two retaining clips.
  • each receiving element of the propellant charge chain 3.1 sensor elements for determining the type of module and the degree of filling are arranged.
  • the sensor elements are designed as guided around the circumference of the shells 3.2 spring strips 3.41 to 3.43 with a protruding through an opening of the shell sensing element, and each spring strip 3.41 to 3.43 is assigned to its outside a proximity sensor or switch 3.51 to 3.53, the each 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 standard modules TM 1 (FIG. 3B) lying axially one behind the other or a base module TM 2 having a somewhat longer length (FIG.
  • the sensor elements are precisely identified by the sensor elements in this case can be used, which type and which number of propellant charge modules are contained in the shell.
  • some or all of the spring strips 3.41 to 3.43 are pushed out in the direction of the proximity switches 3.51 to 3.53.
  • the portioning unit 5 has an axially to the receiving element 3.2 of the propellant charge chain 3.1 arranged in the removal position, divided in the axial direction receiving tray with a large shell part 5.1, which has a stop 5.3 for the propellant modules at the end facing away from the propellant charge chain 3.1 end, and a small shell part to 5.2 lateral support of the propellant charge modules.
  • the large shell part 5.1 is pivotable from a receiving position into a delivery position for transferring the joined propellant charge modules TM to a propellant charge feed tray.
  • 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 delivered.
  • 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 tower housing 1, in which a heavy weapon W is mounted in a manner not specifically shown pivotable about a trunnion in elevation.
  • the tower housing 1 may be rotatably mounted in azimuth on a support structure which may be formed, for example, as a chassis of a Panzerhaubitze or as a battle tank.
  • the tower housing contains in not specifically shown and known manner at least one bullet magazine, from which the weapon W bullets are fed by means of a known fully automatic working bullet feed device.
  • an additional housing 4 pivotally mounted about a vertical axis such that, as well as Fig. 6, the additional housing 4 made one can be moved to the tower housing tightly positioned position in a pivoted outward position.
  • the propellant charge magazine 2 is arranged and the propellant charge machine 3, with which the propellant charges are removed from the propellant charge magazine 2 and the portioning unit 5 are supplied.
  • the additional housing 4 has on the side facing the tower housing 1 a, not visible in Fig. 1, passage opening to which a correspondingly formed passage opening 1.2 in the outer wall 1.1 of the tower housing 1 is opposite.
  • the joined propellant charge is ejected through the passage openings in the additional housing 4 and in the outer wall 1.1 of the tower housing 1.
  • the propellant charge is then taken up by the propellant charge supply shell, which, not shown in Fig. 6, is arranged on the arranged in the tower housing 1 propellant transfer arm and in the area behind the weapon W is pivoted so that they by means of a her arranged propellant charge applicator of the weapon can be supplied.
  • a propellant charge magazine 2 which has a propellant charge machine 3 on one end face.
  • a propellant charge machine 3 can be arranged on both sides of the propellant charge machine, a propellant charge magazine, 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)
  • Warehouses Or Storage Devices (AREA)
  • Elimination Of Static Electricity (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Cosmetics (AREA)
  • Toys (AREA)

Claims (14)

  1. Dispositif pour l'introduction de charges propulsives dans une arme lourde comprenant au moins un chargeur de charge propulsive et un dispositif pour l'introduction de charge propulsive, au moyen duquel les charges propulsives sont enlevées du chargeur de charge propulsive et sont transférées à un bras de transfert de charge propulsive, qui présente une coque d'introduction de charge propulsive pouvant basculer à l'intérieur de la zone derrière l'arme avec un dispositif de préparation de charge propulsive, caractérisé par les caractéristiques suivantes :
    a) chaque chargeur de charge propulsive (2) est réalisé sous la forme d'un chargeur disposé de façon fixe, dans lequel des modules de charge propulsive TM sont montés dans des guides (2.1) de telle sorte que leurs axes longitudinaux sont agencés horizontalement, un nombre prédéfini de modules de charge propulsive étant montés ensuite axialement les uns contre les autres dans chaque guide et à chaque fois un nombre prédéfini de guides (2.1) étant disposés parallèlement entre eux et les uns au-dessus des autres dans des plans horizontaux.
    b) le dispositif d'introduction de charge propulsive présente un automate de charge propulsive (3) disposé à côté du chargeur de charge propulsive (2) avec une chaîne de charge propulsive (3.1) entraînée, tournant dans un plan vertical, avec des éléments de réception (3.2) pour la réception respective d'au moins un module de charge propulsive et des dispositifs pour le transfert de modules de charge propulsive des guides du chargeur de charge propulsive (2) dans les éléments de réception (3.2) de la chaîne de charge propulsive (3.1) ;
    c) sur la position de prélèvement sur l'extrémité supérieure de la chaîne de charge propulsive (3.1) est disposée, axialement à l'élément de réception (3.2) supérieur respectif, une unité de portionnement (5) avec des moyens (6) pour le transfert et l'assemblage d'un nombre prédéfini de modules de charge propulsive ;
    d) il existe des moyens (5.1) pour le transfert des modules de charge propulsive assemblés de l'unité de portionnement (5) à la coque d'introduction de charge propulsive.
  2. Dispositif selon la revendication 1, caractérisé en ce que les guides dans le chargeur de charge propulsive (2) sont conçus sous la forme de tubes de réception (2.1), qui peuvent être alimentés avec une dépression d'air pour l'introduction de modules de charge propulsive et avec une surpression d'air pour l'évacuation de modules de charge propulsive.
  3. Dispositif selon la revendication 1, caractérisé en ce que les guides dans le chargeur de charge propulsive sont conçus sous la forme de coques de réception ouvertes ou de rails de réception et l'arrivée et l'évacuation de modules de charge propulsive s'effectuent par des entraîneurs guidés sur des broches ou des chaînes circulantes.
  4. Dispositif selon la revendication 2 ou 3, caractérisé en ce que des cliquets d'arrêt sont disposés sur les guides du chargeur de charge propulsive (2).
  5. Dispositif selon l'une quelconque des revendications là 4, caractérisé en ce que les éléments de réception (3.2) de la chaîne de charge propulsive (3.1) sont conçus sont la forme de coques ouvertes et chaque maillon de chaîne présente respectivement dans la zone des extrémités d'une coque un étrier de retenue constitué de deux parties de bague circulaire (3.31 - 3.32) se touchant et reliées entre elles au point de contact, à chaque fois une partie de bague circulaire (3.31) comprenant la coque (3.2) de ce maillon de chaîne sur le côté fermé et l'autre partie de bague circulaire (3.32) comprenant également la coque d'un maillon de chaîne voisin sur le côté ouvert.
  6. Dispositif selon la revendication 5, caractérisé en ce que chaque étrier de retenue est conçu de telle sorte que les ouvertures des parties de bague circulaire (3.31, 3.32) sont disposées dans un angle de 90° les unes par rapport aux autres et les étriers de retenue sont disposés et guidés dans la chaîne de charge propulsive (3.1) de telle sorte qu'à chaque fois l'élément de réception (3.2) se trouvant dans la position d'enlèvement présente une zone de passage ouverte et s'étendant en direction axiale pour un élément de passage (6) alors que, dans au moins une partie des autres positions, les coques sur le côté fermé et sur le côté ouvert sont entourées complètement par les parties de bague circulaire (3.31, 3.32) coopérant de deux étriers de retenue.
  7. Dispositif selon l'une quelconque des revendications 1 à 6, caractérisé en ce que des éléments de détection pour la détermination du type de module et du degré de remplissage sont disposés sur chaque élément de réception de la chaîne de charge propulsive (3.1).
  8. Dispositif selon la revendication 7, caractérisé en ce que les éléments de détection présentent des bandes à ressort (3.41-3.43) guidées sur le pourtour des coques (3.2) avec un élément de balayage dépassant dans une ouverture de la coque et un capteur ou un commutateur de proximité (3.51-3.53) est disposé en face de chaque bande à ressort (3.41-3.43) sur son côté extérieur.
  9. Dispositif selon la revendication 8, caractérisé en ce que trois bandes à ressort (3.41-3.43) sont disposées sur chaque coque à une distance axiale prédéfinie.
  10. Dispositif selon l'une quelconque des revendications 1 à 9, caractérisé en ce que dans la zone de la position d'enlèvement sont disposés des capteurs pour le contrôle du transfert des modules de charge propulsive de l'élément de réception de la chaîne de charge propulsive (3.1) à l'unité de portionnement (5).
  11. Dispositif selon l'une quelconque des revendications 1 à 10, caractérisé en ce que les moyens pour le transfert et l'assemblage de modules de charge propulsive de l'élément de réception de la chaîne de charge propulsive (3.1) dans l'unité de portionnement (5) présentent comme élément de transfert au moins un crochet de préhension (6) qui peut être déplacé parallèlement à la direction radiale de l'élément de réception et de l'unité de portionnement.
  12. Dispositif selon l'une quelconque des revendications 1 à 11, caractérisé en ce que l'unité de portionnement (5) présente une coque de réception (5.1-5.2) disposée axialement à l'élément de réception de la chaîne de charge propulsive (3.1) dans la position de prélèvement et divisée dans la direction axiale avec une grande partie de coque (5.1), qui présente sur l'extrémité opposée à la chaîne de charge propulsive (3.1) une butée (5.3) pour le module de charge propulsive et avec une petite partie de coque (5.2) pour le soutien latéral des modules de charge propulsive, la grande partie de coque (5.1) pouvant être basculée d'une position de réception dans une position de distribution pour le transfert des modules de charge propulsive assemblés à la coque d'introduction de charge propulsive.
  13. Dispositif selon l'une quelconque des revendications 1 à 12, caractérisé en ce que le chargeur de charge propulsive (2) et l'automate de charge propulsive (3) ainsi que l'unité de portionnement (5) sont disposés à l'intérieur d'un boîtier supplémentaire (4) disposé de façon amovible ou basculante sur la paroi extérieure du boîtier de tour (1) blindé d'un module de tir, à chaque fois des ouvertures de passage (1.2) disposées en alignement les unes par rapport aux autres pour les charges propulsives à transférer du boîtier supplémentaire (4) dans le boîtier de tour (1) étant disposées sur la paroi extérieure (1.1) du boîtier de tour (1) ainsi que dans la paroi extérieure, opposée à la paroi extérieure (1.1) du boîtier de tour (1), du boîtier supplémentaire (4) et le bras de transfert de charge propulsive avec la coque d'introduction de charge propulsive étant disposé à l'intérieur du boîtier de tour (1).
  14. Dispositif selon les revendications 12 et 13, caractérisé en ce que, dans la position de distribution de la grande partie de coque (5.1), la charge propulsive assemblée est éjectée par les ouvertures de passage du boîtier supplémentaire (4) et de la paroi extérieure (1.1) du boîtier de tour (1).
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 EP1721114A1 (fr) 2006-11-15
EP1721114B1 true EP1721114B1 (fr) 2007-07-11

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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)

Cited By (5)

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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
DE102022101219A1 (de) 2022-01-19 2023-07-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren zur Handhabung von Treibladungsmodulen
DE102022101215A1 (de) 2022-01-19 2023-07-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Portioniervorrichtung
EP4215865A1 (fr) 2022-01-19 2023-07-26 Krauss-Maffei Wegmann GmbH & Co. KG Magasin

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KR102704014B1 (ko) 2020-02-06 2024-09-06 한화에어로스페이스 주식회사 장약 공급 장치

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE102022101219A1 (de) 2022-01-19 2023-07-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren zur Handhabung von Treibladungsmodulen
DE102022101215A1 (de) 2022-01-19 2023-07-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Portioniervorrichtung
EP4215865A1 (fr) 2022-01-19 2023-07-26 Krauss-Maffei Wegmann GmbH & Co. KG Magasin
WO2023138728A1 (fr) 2022-01-19 2023-07-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Chargeur à charge propulsive
WO2023138729A1 (fr) 2022-01-19 2023-07-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Procédé de manipulation de modules de charge propulsive et de tiges de charge propulsive
WO2023138730A1 (fr) 2022-01-19 2023-07-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Appareil de portionnement
WO2023138731A1 (fr) 2022-01-19 2023-07-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Dispositif de transfert pour charges de propulsion

Also Published As

Publication number Publication date
IL179556A0 (en) 2007-05-15
IL179556A (en) 2011-06-30
EP1721114A1 (fr) 2006-11-15
ATE366909T1 (de) 2007-08-15
DE102004025742A1 (de) 2005-12-22
US20080047417A1 (en) 2008-02-28
DE502005001021D1 (de) 2007-08-23
US7475626B2 (en) 2009-01-13
NO334270B1 (no) 2014-01-27
ES2289714T3 (es) 2008-02-01
NO20065698L (no) 2007-02-23
WO2005116564A1 (fr) 2005-12-08
CA2567774A1 (fr) 2005-12-08
CA2567774C (fr) 2009-06-23

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