EP1596150B1 - Vorrichtung zum Trennen von Treibladungsmodulen - Google Patents

Vorrichtung zum Trennen von Treibladungsmodulen Download PDF

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Publication number
EP1596150B1
EP1596150B1 EP05290809A EP05290809A EP1596150B1 EP 1596150 B1 EP1596150 B1 EP 1596150B1 EP 05290809 A EP05290809 A EP 05290809A EP 05290809 A EP05290809 A EP 05290809A EP 1596150 B1 EP1596150 B1 EP 1596150B1
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EP
European Patent Office
Prior art keywords
modules
module
propellant charge
shanks
incorporating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP05290809A
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English (en)
French (fr)
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EP1596150A1 (de
Inventor
Julien Boutin
Patrick Minard
Robert Vernet
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.)
KNDS France SA
Original Assignee
Nexter Systems SA
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 Nexter Systems SA filed Critical Nexter Systems SA
Priority to PL05290809T priority Critical patent/PL1596150T3/pl
Publication of EP1596150A1 publication Critical patent/EP1596150A1/de
Application granted granted Critical
Publication of EP1596150B1 publication Critical patent/EP1596150B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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

Definitions

  • the technical sector of the present invention is that devices for feeding an embedded field weapon using propellant charges in a given amount.
  • the FR-A-2764055 describes a system for automatically entering separate propellant charge modules stored in a store. No indication is given in this patent on the subsequent handling of these modules.
  • the FR-A-2778235 describes a device for feeding an artillery gun into ammunition elements consisting of a projectile and separate modules of propellant charge.
  • the store is equipped with an elevator for taking the number of modules that one wishes to use.
  • the FR-A-2743411 discloses a device for transferring separate modules, constituting a propellant charge, between a storage magazine and a loading system of these modules in the chamber of an artillery gun. This device is intended to collect all the modules stored in a row of the store without any distinction.
  • the US-A-5844163 describes a system for loading propellant charge modules into a gun, modules taken from a storage container.
  • the modules are stored in individual compartments and are taken in number at the discretion of the user. In other words, the modules are separated in the store but are then linked together before loading.
  • the object of the present invention is to provide a system for overcoming this disadvantage of the prior art by allowing to feed an artillery gun with the desired amount of modules, whether these modules are stored linked together or not.
  • the invention therefore relates to a device for separating propellant charge modules for field weapons, each module comprising a head and a bottom, the head of a module being engaged in the bottom of an adjacent module, characterized in that it comprises means for receiving all the modules comprising blocking means of each module, these blocking means being connected by connecting and separating means for controlling a relative translation of each module relative to its neighbors thus ensuring the separation of the modules.
  • the locking means consist of a set of pairs of clamps arranged on either side of a module, each module being held by a pair of clamps, each pair of clamps. being controlled in translation by the connecting and separating means.
  • the connecting means comprises two screws comprising, facing each module, a threaded rod carrying a clamp, each screw being connected to a rotating drive means.
  • each screw comprises a first group of threaded rods all having threads of different pitch and in the same direction, and a second group of threaded rods all having threads of different pitch and the same meaning, but in the opposite direction to that of the first group, the number of threaded rods being equal to the number of propellant charge modules.
  • the threaded rods of each group have different diameters, the end rods having a smaller diameter than the intermediate rods whose diameter is smaller than that of the median rods.
  • the clamps consist of jacks having a body integral with a threaded rod and a jaw movable relative to the body.
  • the separate modules are transferred into a selection zone comprising means for selecting the modules to switch the selected modules in a reception means.
  • connection and separation means and said selection zone are arranged in the same box.
  • the selection zone is provided with transverse walls defining a number of compartments equal to the number of propellant charge modules separated by the separation means.
  • the modules are transferred into the selection zone by gravity.
  • the means for selecting the modules consists of a set of pushers, each pushbutton being selectively controlled.
  • the receiving means comprises a receiving bucket of the individual modules, whose shape is such that it ensures the coaxial centering of the modules.
  • said receiving means is provided with means for assembling the modules able to engage the head of a module in the bottom of the adjacent module.
  • said module assembly means comprises a mobile stop under the action of a cylinder and a fixed counter-stop.
  • the fixed counter-stop may advantageously be tilted with respect to the receiving means.
  • a first advantage of the device according to the invention resides in the possibility of selecting at will the propellant charge modules to be loaded, whether they are stored linked or not.
  • Another advantage of the device according to the invention is to absorb the dispersions of diameter and length of the modules.
  • Another advantage lies in the simultaneous separation of all the modules, which makes it possible to respect the constraints of rate of fire.
  • Another advantage lies in the fact that a single actuator, acting on the worm, allows the separation of the modules, which reduces the bulk.
  • Another advantage lies in the fact that the linear cylinder without rod being located under the receiving bucket reduces the size of the device despite the large stroke of the cylinder.
  • the device according to the invention is intended to equip a weapon fed automatically from a magazine 1 separately using projectiles and propellant charge modules.
  • the figure 1 shows the magazine 1 where are arranged rows 2 of propellant modules 4. Above the magazine 1, we can see the gripper 3 loaded with a row of modules 4. This gripping device 3 takes a row of propellant charge modules 4 in the magazine and brings it to the device 5 according to the invention.
  • This gripping device is well known in its structure and function. It is the subject of FR2842893 and it is not necessary to describe it in more detail. Of course, these different elements are interconnected by known means which do not form part of the invention.
  • the device 5 comprises a box 6 and a means 7 for meeting the modules.
  • the box 6 contains in its upper part 6a a means 11 for receiving and blocking the modules, a connecting and separating means and locking means.
  • the casing 6 comprises in its lower part 6b a selection zone 10 of the modules.
  • the box 6 is shown empty of modules.
  • the means 11 for receiving and blocking the modules the means 9 for separating the modules and the selection means 10.
  • the box 6 is in the form of a parallelepiped having a lower lateral opening arranged in look at the average 7 meeting modules.
  • the means 11 for receiving and locking consists of two rows of clamps 8 arranged vis-à-vis and coming to bear on each module to immobilize temporarily.
  • the clamps 8 of each row are each joined by means 9 of connection and separation.
  • the means 9 is constituted by a pair of screws of which only one 9a is visible in the drawing.
  • the two screws 9 are connected to the box 6 via their two ends so as to ensure their rotation relative to the box 6 in this embodiment.
  • Each clamp 8 is constituted by a pneumatic cylinder (or hydraulic) which is more particularly visible on the figure 8 .
  • the clamp thus comprises a fixed body 28 having a thread 29 which receives the screw 9.
  • a movable jaw 30 can translate relative to the body 28.
  • a housing 31 is interposed between the movable jaw 30 and the body 28. This housing receives a rubber bladder (not shown) which is connected to a pneumatic (or hydraulic) device. Inflation of the bladder causes the thrust of the jaw 30 which then applies against the load module 4.
  • the jaw 30 carries on its face applied against the load module a rubber pad 32 having a V profile ensuring the reliable setting of the load module without the risk of damage.
  • two clamps arranged opposite are controlled, they ensure a reliable maintenance of the load module, when their bladders are deflated, the mass of the load module which acts on the V-shaped profiles is enough to push the jaws 30 on the bodies of cylinder 28.
  • the casing 6 has in its lower part at the level of the selection means 10 compartments 12, of which only the compartment 12a is noted on the figure 2 .
  • Each compartment 12 is intended to receive a module 4 once the modules are separated from each other.
  • Each compartment 12 is provided with a pusher (not visible in the figures), for passing each corresponding module in the meeting means 7 (not shown in this figure). All of these push-buttons constitute the means for selecting the modules 4.
  • Such a push-button selection means is the subject of the FR-2743411 and it is not necessary to describe it in more detail.
  • the figure 3 shows the cooperation between the box 6 and the meeting means 7 illustrating a step of the operation of the device 1.
  • the wall of the box 6, opposite the magazine 1, is provided with a transverse opening 26 for the transfer of the selected modules to the means meeting 7 arranged in the immediate vicinity.
  • the device 5 then comprises in this figure a first series of modules 4a located in the receiving and locking means 11 (upper part 6a of the box), another 4b being in the selection zone 10 (part bass 6b of the caisson), and finally a third 4c in the means of meeting 7.
  • the modules 4b which have been separated, are isolated from each other by transverse walls 14a to 14e which separate the compartments 12, of which only 12c is designated in the figure.
  • the bottom of each compartment is pierced with orifices 13, of which only 13e is shown. These orifices allow the passage of the pushers (not shown in the figures).
  • the meeting means 7 of the propellant charge modules 4 comprises a receiving means 15 which consists of a V-shaped gutter. This shape makes it possible to ensure axial centering of the modules 4c. Indeed, the modules can be of variable length and diameter and the gutter compensates for these variations so that the meeting of the modules is possible.
  • Gutter 15 is provided with a meeting means (not shown in this figure) able to exert an axial pressure on the modules in order to fit into each other.
  • the gutter is provided with a fixed counter-stop (not visible) intended to hold the bottom of the last module and a movable stop 16 for pushing the head of the first module.
  • a cylinder (not visible) without rod, placed under the gutter, provides the necessary thrust.
  • the figure 4 shows the detail of the elements that are inside the box 6, gathering the means 11 for receiving and blocking the modules, the means 9 for connection and separation and the selection area 10, each being loaded modules propulsive charges.
  • Each module 4 is held by a pair of clamps 8a to 8f, and each row of clamps is also joined by the connecting and separating means 9 of the modules.
  • the connecting and separating means 9 consists of two screws 9a, 9b, the structure of which is illustrated in FIG. figure 7 .
  • the two screws 9 are rotated by a motor 20 (integral with the box), via a belt 21.
  • the outer diameter of the head 23 is the same as the internal diameter of the wall 24.
  • the modules 4 can therefore fit into each other.
  • the separation means 9 ensures a relative translation of one module relative to another so as to separate them. Since the modules 4 are separated from one another, it is then possible to select the number of modules that one wishes to use to ensure that the projectile is fired by the weapon. This selection is done at the coach 10 as described by FR2743411 .
  • the meeting means comprises a gutter 15 V-shaped. This form makes it possible to ensure axial centering of the modules.
  • the channel 15 is mounted on a base 18, provided with a central groove 19 in which slides a movable stop 16.
  • a counter-stop 17 fixed in translation is connected to the base 18 by means of an axis 20 which allows a tilting of the abutment 17 relative to the base 18.
  • the abutment can be tilted by an actuator (not shown). Once rocked, it allows the passage of load modules pushed by the movable stop which can then transfer them to a loading arm of the weapon.
  • the fixed stop 17 is made here in the form of a ring whose outer diameter is slightly smaller than the diameter of the bottom 25 of the module 4 and which has an axial hole. Such an arrangement avoids exerting pressure on the ignition means of the module which is generally disposed at the axis.
  • a rodless cylinder (of a conventional type not shown) is disposed in the support 18 and drives the mobile stop 16 in translation.
  • the figure 7 is a schematic external view of a worm 9 illustrating its structure.
  • This screw 9 consists of a first group of three threaded rods a1, b1 and c1 with different pitch but all in the same direction and a second group of three threaded rods a2, b2 and c2 of different pitch but all of sense opposite of that of the first group.
  • the rod a1 has a p p to the right while the rod a2 has a p p left.
  • the stem b1 has a step 3p on the right and the stem b2 a step 3p on the left.
  • the stem c1 has a step 5p on the right and the stem c2 a step 5p on the left.
  • the diameter of the rods c1 and c2 are lower than that of the rods b1 and b2 which are themselves smaller than that of the rods a1 and a2. These differences in diameters allow the screwing of the bodies 28 of the clamps on the screw despite the differences in pitch.
  • Each rod thus receives a clamp 8 and the pivoting of the screw 9 causes the movement of the six different clamps.
  • each turn of the screw 9 the clamps move away from each other.
  • the end clamps connected to the threaded rods c1 and c2 travel in translation a distance five times greater than the central clamps connected to the threaded rods a1 and a2.
  • the intermediate clamps connected to the threaded rods b1 and b2 travel a distance three times greater than the clamps connected to the threaded rods a1 and a2. In this case, the separation of the modules requires very little rotation of the screw 9, for example 2 turns.
  • the clamps integral with the rods b1 and b2 deviate from the integral clamps of the rods a1 and a2 respectively by a distance equal to d.
  • the pitch of the rods b1 and b2 are equal to three times the pitch p of the rods a1 and a2
  • the result for a given rotation is a displacement of the tongs connected to the rods b1 and b2 which is three times the displacement of the tongs connected to the rods. a1 and a2.
  • the clamps secured to the rods c1 and c2 deviate from the integral clamps rods b1 and b2 respectively by a distance also equal to d.
  • the pitch of the rods c1 and c2 is equal to 5 times the pitch of the rods a1 and a2.
  • This structure of the screw 9 thus allows a simultaneous separation of the six propellant charge modules which are all spaced from each other by the same distance.
  • the operation of the device according to the invention is as follows.
  • the gripping module 3 withdraws from the magazine 1 six modules recessed into each other, brings them above the device 5 as shown on the drawing. figure 2 and engages them in the upper part 6a of the box as shown on the figure 3 .
  • the pairs of clamps 8 are then controlled so as to immobilize each module 4.
  • the screws 9 are then controlled to cause the respective translation of the modules relative to one another.
  • FIGs 9a and 9b are top views of the device showing for the figure 9a the clamps 8 holding the modules in their linked position and for the figure 9b the modules untied after rotation of the screws 9a, 9b. It is found that the spacing between the different modules is the same after separation.
  • the stop 16 is in the extreme position relative to the stop 17. It is then ordered the translation of the stop mobile 16 to engage the head 23 a module in the bottom 25 of the adjacent module.
  • the number of modules selected is never less than half the number of modules provided to the device according to the invention.
  • the number of modules selected in the embodiment described is between 3 and 6.

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  • Sink And Installation For Waste Water (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Special Conveying (AREA)
  • Automatic Assembly (AREA)

Claims (15)

  1. Vorrichtung zur Trennung (5) von Modulen (4) von Treibstoffladung für Feldwaffen, wobei jedes Modul einen Kopf (23) und einen Boden (25) umfasst, wobei der Kopf eines Moduls mit dem Boden eines benachbarten Moduls in Eingriff steht, dadurch gekennzeichnet, dass sie ein Mittel zur Aufnahme der Gesamtheit der Module umfasst, das Mittel zum Festsetzen (8) jedes Moduls umfasst, wobei diese Mittel zum Festsetzen durch ein Mittel zum Verbinden und Trennen (9) verbunden sind, um zu ermöglichen, eine relative Verschiebung jedes Moduls in Bezug auf seine Nachbarn zu betätigen, um so die Trennung der Module zu gewährleisten.
  2. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass die Mittel zum Festsetzen (8) von einem Satz von Paaren von Klammern (8a-8e) gebildet werden, die beiderseits eines Moduls (4) angeordnet sind, wobei jedes Modul von einem Paar Klammern gehalten wird, wobei jedes Paar Klammern durch das Mittel zum Verbinden und Trennen (9) in Verschiebebewegung betätigt wird.
  3. Vorrichtung nach Anspruch 2, dadurch gekennzeichnet, dass das Mittel zum Verbinden (9) zwei Schrauben (9a, 9b), die parallel zu den Modulen verlaufen, und vor jedem Modul eine Gewindestange mit Gewinde umfasst, die eine Klammer (a1-c1, a2-c2) trägt, wobei jede Schraube (9a, 9b) mit einem Dreh-Antriebsmittel (20, 21) verbunden ist.
  4. Vorrichtung nach Anspruch 3, dadurch gekennzeichnet, dass jede Schraube (9) eine erste Gruppe von Gewindestangen (a1-c1) umfasst, von denen alle Gewinde mit unterschiedlichen Gängen und gleicher Richtung tragen, und eine zweite Gruppe von Gewindestangen (a2-c2), von denen alle Gewinde mit unterschiedlichen Gängen und gleicher Richtung tragen, aber die Richtung, die jener der ersten Gruppe entgegengesetzt ist, wobei die Anzahl von Gewindestangen gleich der Anzahl von Modulen (4) von Treibstoffladung ist.
  5. Vorrichtung nach Anspruch 4, dadurch gekennzeichnet, dass die Gewindestangen von jeder Gruppe verschiedene Durchmesser aufweisen, wobei die Stangen am Ende einen Durchmesser besitzen, der kleiner als derjenige der dazwischen liegenden Stangen ist, deren Durchmesser kleiner als derjenige der mittleren Stangen ist.
  6. Vorrichtung nach einem der Ansprüche 3 bis 5, dadurch gekennzeichnet, dass die Klammern von Zylindern gebildet werden, die einen Körper, der fest mit einer Gewindestange verbunden ist, und eine in Bezug auf den Körper bewegliche Backe umfassen.
  7. Vorrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die getrennten Module (4) in eine Zone zur Auswahl (10) gebracht werden, die ein Mittel zur Auswahl der Module umfasst, um die ausgewählten Module in ein Aufnahmemittel (7) kippen zu lassen.
  8. Vorrichtung nach Anspruch 7, dadurch gekennzeichnet, dass das genannte Mittel (8) zum Verbinden und Trennen und die genannte Zone zur Auswahl (10) in ein und demselben Kasten (6) angeordnet sind.
  9. Vorrichtung nach Anspruch 7, dadurch gekennzeichnet, dass die Zone zur Auswahl (10) mit Querwänden (14) versehen ist, die eine Anzahl von Fächern festlegen, die gleich der Anzahl von durch das Mittel zum Trennen (8) getrennten Modulen von Treibstoffladung ist.
  10. Vorrichtung nach Anspruch 7, dadurch gekennzeichnet, dass die Module (4) durch Gravitation in die Zone zur Auswahl (10) gebracht werden.
  11. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass das Mittel zur Auswahl der Module von einem Satz Stößel gebildet wird, wobei jeder Stößel selektiv gesteuert wird.
  12. Vorrichtung nach Anspruch 7, dadurch gekennzeichnet, dass das Aufnahmemittel (7) einen Becher zur Aufnahme (17) der individuellen Module umfasst, dessen Form derartig ist, dass sie die koaxiale Zentrierung der Module gewährleistet.
  13. Vorrichtung nach Anspruch 12, dadurch gekennzeichnet, dass das genannte Aufnahmemittel (7) mit einem Mittel zur Montage (16, 17) der Module (4) versehen ist, das geeignet ist, den Kopf (23) eines Moduls mit dem Boden (25) des benachbarten Moduls in Eingriff zu bringen.
  14. Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, dass das genannte Mittel zur Montage der Module einen unter Einwirkung eines Zylinders beweglichen Anschlag (16) und einen festen Gegenanschlag (17) umfasst.
  15. Vorrichtung nach Anspruch 14, dadurch gekennzeichnet, dass der feste Gegenanschlag (17) in Bezug auf das Aufnahmemittel (7) gekippt werden kann.
EP05290809A 2004-04-29 2005-04-13 Vorrichtung zum Trennen von Treibladungsmodulen Expired - Lifetime EP1596150B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL05290809T PL1596150T3 (pl) 2004-04-29 2005-04-13 Urządzenie do rozdzielania modułów ładunków miotających

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0404560 2004-04-29
FR0404560A FR2869681B1 (fr) 2004-04-29 2004-04-29 Dispositif de separation de modules de charge propulsive

Publications (2)

Publication Number Publication Date
EP1596150A1 EP1596150A1 (de) 2005-11-16
EP1596150B1 true EP1596150B1 (de) 2009-06-24

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EP05290809A Expired - Lifetime EP1596150B1 (de) 2004-04-29 2005-04-13 Vorrichtung zum Trennen von Treibladungsmodulen

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US (1) US7140300B2 (de)
EP (1) EP1596150B1 (de)
AT (1) ATE434750T1 (de)
DE (1) DE602005015054D1 (de)
ES (1) ES2328158T3 (de)
FR (1) FR2869681B1 (de)
PL (1) PL1596150T3 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2945615B1 (fr) 2009-05-18 2011-06-17 Nexter Systems Dispositif de separation d'un ensemble de modules de charge propulsive
SE534616C2 (sv) 2009-10-21 2011-10-25 Bae Systems Bofors Ab Automatiserat laddningsmagasin
DE102011050282B3 (de) 2011-05-11 2012-09-13 Krauss-Maffei Wegmann Gmbh & Co. Kg Vorrichtung und Verfahren zum Portionieren einer Treibladung
DE102011055045B4 (de) * 2011-11-04 2019-01-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Treibladungsportioniereinrichtung
FR3057058B1 (fr) * 2016-10-04 2019-03-29 Nexter Systems Dispositif de calage pour obus et casier apte a accueillir un tel dispositif
DE102019106848A1 (de) * 2019-03-18 2020-09-24 Krauss-Maffei Wegmann Gmbh & Co. Kg Treibladungsportioniereinrichtung mit einem expandierbaren Halteelement
DE102019106849A1 (de) 2019-03-18 2020-09-24 Krauss-Maffei Wegmann Gmbh & Co. Kg Haltevorrichtung für Munitionskörper mit einem expandierbaren Halteelement
DE102020104466B4 (de) * 2020-02-20 2023-02-02 Krauss-Maffei Wegmann Gmbh & Co. Kg Geschosslift
DE102022101215A1 (de) * 2022-01-19 2023-07-20 Krauss-Maffei Wegmann Gmbh & Co. Kg Portioniervorrichtung

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Publication number Priority date Publication date Assignee Title
DE3931059A1 (de) * 1989-09-18 1991-03-28 Rheinmetall Gmbh Treibladungs-portionierer fuer eine mengenvariabel beladbare ladeschale
DE3931192A1 (de) * 1989-09-19 1991-03-28 Rheinmetall Gmbh Schachtmagazin fuer modulare treibladung
FR2702551B1 (fr) * 1993-03-12 1995-05-12 Giat Ind Sa Système de stockage et d'alimentation de charges propulsives destinées à être introduites dans la chambre du canon d'une arme de moyen ou de gros calibre d'un véhicule blindé.
SE503841C2 (sv) 1994-09-07 1996-09-16 Bofors Ab Laddsystem
SE503489C2 (sv) * 1994-10-13 1996-06-24 Bofors Ab Ansättningssystem
SE503490C2 (sv) * 1994-10-13 1996-06-24 Bofors Ab Ammunitionstransportör
FR2743411B1 (fr) * 1996-01-05 1998-02-27 Giat Ind Sa Dispositif de transfert de modules constituant des charges propulsives, entre un magasin de stockage et un systeme de chargement de ces modules dans la chambre d'un canon d'artillerie
FR2743413B1 (fr) * 1996-01-05 1998-02-27 Giat Ind Sa Systeme de stockage et d'alimentation de modules constituant des charges propulsives pour canon d'artillerie
FR2764055B1 (fr) 1997-05-29 1999-07-16 Giat Ind Sa Systeme de saisie automatique de modules de charge propulsive stockes dans un magasin
US6073534A (en) * 1998-01-14 2000-06-13 General Dynamics Armament Systems, Inc. Transfer mechanism and method for uploading and downloading propellant charges and projectiles
FR2778235B1 (fr) 1998-04-30 2000-06-02 Giat Ind Sa Dispositif d'alimentation d'un canon d'artillerie en elements de munition

Also Published As

Publication number Publication date
DE602005015054D1 (de) 2009-08-06
ES2328158T3 (es) 2009-11-10
PL1596150T3 (pl) 2009-12-31
US7140300B2 (en) 2006-11-28
ATE434750T1 (de) 2009-07-15
EP1596150A1 (de) 2005-11-16
US20050241469A1 (en) 2005-11-03
FR2869681A1 (fr) 2005-11-04
FR2869681B1 (fr) 2006-07-28

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