EP1596150A1 - Dispositif de séparation de modules de charge propulsive - Google Patents
Dispositif de séparation de modules de charge propulsive Download PDFInfo
- Publication number
- EP1596150A1 EP1596150A1 EP05290809A EP05290809A EP1596150A1 EP 1596150 A1 EP1596150 A1 EP 1596150A1 EP 05290809 A EP05290809 A EP 05290809A EP 05290809 A EP05290809 A EP 05290809A EP 1596150 A1 EP1596150 A1 EP 1596150A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- modules
- module
- rods
- propellant charge
- separation
- 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
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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 to feed a field weapon embedded with propulsive charges in a given quantity.
- FR-A-2764055 discloses an entry system automatic propellant charge separate modules stored in a store. No indication is given in this patent on the subsequent handling of these modules.
- FR-A-2778235 discloses a device supply of an artillery gun in elements of ammunition consisting of a projectile and separate modules of propulsive charge.
- the store is equipped an elevator to collect the number of modules that we want to use.
- FR-A-2743411 discloses a transfer device separate modules, constituting a propulsive charge, between a storage warehouse and a loading system of these modules in the room of an artillery gun. This device is planned to collect all stored modules in a row of the shop without any distinction.
- US-A-5844163 discloses a charging system for propellant charge modules in a gun, modules removed in a storage container.
- the modules are stored in individual compartments and are taken in number at the discretion of the user.
- the modules are separated in the store but are then tied together before loading.
- the object of the present invention is to provide a system to overcome this drawback of the prior art by allowing to feed an artillery gun with the desired amount of modules, whether these modules are stored related to each other or not.
- the subject of the invention is therefore a separation device 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 locking means of each module, these locking means being connected by a connecting and separating means for controlling a relative translation of each module with respect to its neighbors thus ensuring the separation of the modules.
- the blocking means consist of a set of pairs of pliers arranged on both sides of a module, each module being maintained by a pair of tongs, each pair of tongs being translationally controlled by the connecting and separating means.
- the connecting means comprises two screws comprising next to each module a threaded rod carrying a clamp, each screw being linked to a drive means in rotation.
- 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 carrying threads of different pitch and likewise meaning, but in the opposite direction to that of the first group, the number of threaded rods being equal to the number of modules of propulsive charge.
- the threaded rods of each group have different diameters, the stems end of a diameter smaller than that of the stems intermediaries whose diameter is smaller than that of median stems.
- the tongs are constituted by jacks comprising a solidarity body a threaded rod and a movable jaw with respect to body.
- the separate modules are transferred into a selection area comprising a selection means for selecting modules to switch the chosen modules in a way reception.
- said connecting and separating means and said selection area are arranged in one and the same caisson.
- the area of selection is provided with transverse walls defining a number of compartments equal to the number of propellant charge modules separated by the means of separation.
- the modules are transferred to the area of gravity selection.
- the module selection means is constituted a set of pushers, each push being controlled selectively.
- the receiving means comprises a bucket reception of the individual modules, the shape of which is it ensures the coaxial centering of the modules.
- said receiving means is provided a module assembly means adapted to engage the head a module in the bottom of the adjacent module.
- said module assembly means comprises a movable stop under the action of a jack and a counter-stop fixed.
- the fixed counter-stop can advantageously be tilted relative to the receiving means.
- a first advantage of the device according to the invention lies in the possibility of selecting at will propellant charge modules to be loaded, whether they are stored related or not.
- Another advantage of the device according to the invention is absorb dispersions of diameter and length of modules.
- Another advantage lies in the simultaneous separation of all the modules, which makes it possible to respect the constraints rate of fire.
- Another advantage lies in the fact that only one actuator, acting on the worm screws, allows the separation of modules, which reduces congestion.
- Another advantage lies in the fact that the cylinder linear without stem being located under the receiving bucket reduces the size of the device despite the great stroke of the cylinder.
- the device according to the invention is intended to equip a weapon powered automatically from a store 1 separately using projectiles and charge modules propellant.
- Figure 1 shows the store 1 where are arranged rows 2 of propellant modules 4. Above store 1, we can see the gripping device 3 loaded of a row of modules 4. This gripping device 3 takes a row of propellant charge modules 4 in the store and brings it to the device 5 according to the invention.
- This gripping device is well known in its structure and his function. It is the subject of patent FR2842893 and it is not not necessary to describe it in more detail. Of course, these different elements are connected to each other by means known which are not part of the invention.
- the device 5 comprises a box 6 and means 7 for meeting the modules.
- Box 6 contains in its upper part 6a a means 11 for receiving and Blocking modules, a means of connection and separation as well as locking means.
- Box 6 includes in its lower part 6b a selection zone 10 modules.
- the casing 6 is shown empty of modules.
- the means 11 of receiving and blocking modules the means 9 of separation modules and the means of selection 10.
- the box 6 is present in the form of a parallelepiped presenting a lower side opening arranged opposite means 7 meeting of the modules.
- the means 11 for receiving and blocking consists of two rows of clamps 8 arranged vis-a-vis and coming take support on each module in order to immobilize it temporarily.
- the clamps 8 of each row are each joined by a 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 casing 6 by through their both ends so as to ensure their rotation relative to this box 6 in this mode of production.
- 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 comprising a tapping 29 which receives the screw 9.
- a movable jaw 30 can to translate with respect to the body 28.
- a dwelling 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 jaw thrust 30 which then applies against the load module 4.
- the jaw 30 bears on its face applied against the load module a rubber pad 32 having a V-shaped profile ensures reliable calibration of the load module without risk of damaging it.
- two clamps arranged opposite are controlled, they ensure a Reliable maintenance of the load module, when their bladders are deflated, the mass of the charging module acting on V-shaped profiles enough to push the jaws 30 on the cylinder body 28.
- the box 6 has in its lower part at the level the means of selection 10 compartments 12, of which only the compartment 12a is noted in Figure 2.
- Each compartment 12 is intended to receive a module 4 once the modules separated from each other.
- Each compartment 12 is provided with a pusher (not visible in the figures), intended to pass each corresponding module in the meeting medium 7 (not shown in this figure). All of these pushers constitute the means of selection modules 4.
- Such a push-button selection means the subject matter of FR-2743411 and it is therefore not necessary to describe it in more detail.
- Figure 3 shows the cooperation between box 6 and the meeting means 7 illustrating a step of operation of the device 1.
- the wall of the box 6, opposite the magazine 1, is provided with a transverse opening 26 allowing the transfer of the selected modules to the meeting facility 7 arranged in the immediate vicinity.
- the device 5 then comprises this figure a first series of modules 4a found in the receiving and locking means 11 (upper part 6a of the box), another 4b located in the area of selection 10 (lower part 6b of the box), and finally a third 4c in the means of meeting 7.
- the modules 4b which have been separated, are isolated from each other by walls transverse 14a to 14e which separate the compartments 12, of which only 12c is indicated in the figure.
- the bottom of each compartment is pierced with orifices 13, of which only 13e is represent. These holes allow the passage of pushers (not shown in the figures).
- the means of meeting 7 modules 4 propellant charge comprises a reception means 15 which consists of a Gutter shaped V. This form ensures a axial centering of the modules 4c. Indeed, modules can be of varying length and diameter and the gutter compensates for these variations so that the meeting of modules is possible.
- the gutter 15 is provided with a means of meeting (no shown in this figure) able to exert pressure axial to the modules in order to fit them into each other other.
- the gutter is provided with a fixed counter-stop (no visible) to hold the bottom of the last module and a movable stop 16 intended to push the head of the first module.
- a cylinder (not visible) without rod, placed under gutter, ensures the necessary thrust.
- FIG 4 shows the detail of the elements which are inside the box 6, gathering the means 11 of receiving and blocking the modules, the means 9 link and separation and the selection zone 10, each being loaded with propellant charge modules.
- Each module 4 is held by a pair of clamps 8a to 8f, and each row of clips is also joined by the means of connection and separation 9 modules.
- the connecting and separating means 9 consists of two screws 9a, 9b whose structure is illustrated in FIG. two screws 9 are rotated by a motor 20 (secured to the box), via a belt 21.
- each module is isolated from its neighbors by 14.
- This figure shows the structure of the modules 4 which each comprise a head 23, a body 24 and a bottom formed of a cylindrical wall 24.
- the outer diameter of the head 23 is the same as the internal diameter of the wall 24.
- the modules 4 can therefore to fit into each other.
- the separation means 9 makes it possible to ensure relative translation of one module with respect to another of way to separate them.
- the modules 4 being separated the each other it is then possible to select the number of modules that one wishes to use to ensure the Shot of the projectile by the weapon. This selection is done at the aid of breeder 10 as described by the patent FR2743411.
- FIGS. 5 and 6 show the means of meeting 7, respectively without modules and filled with modules.
- the meeting means comprises a gutter 15 in the shape of V. This form ensures a axial centering of the modules.
- the gutter 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 linked to the base 18 with the aid of an axis 20 which allows a tilting of the abutment 17 relative to the base 18.
- the counter stop can be tilted by an actuator (no represent). Once switched, it allows the passage of charging 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 crown whose outer diameter is slightly lower to the diameter of the bottom 25 of the module 4 and which has a hole axial. Such a provision makes it possible to avoid exercising pressure on the ignition means of the module which is generally disposed at the axis.
- Rodless cylinder (of a conventional type not shown) is arranged in the support 18 and it drives in translation the movable stop 16.
- FIG. 7 is a schematic external view of a screw endless 9 illustrating its structure.
- This screw 9 is consisting of a first group of three threaded rods a1, b1 and c1 not different but all in the same direction and a second group of three threaded rods a2, b2 and c2 step different but all of the opposite direction from that of the first group.
- the stem a1 has a p-step to the right while the stem a2 has a p step left.
- the stem b1 has a step 3p on the right and the stem b2 a step 3p left.
- the stem c1 has a step 5p right and the stem c2 a step 5p on the left.
- the diameter of the rods c1 and c2 are lower than the rods b1 and b2 which are themselves lower than the stems a1 and a2. These differences in diameters allow the screwing of the body 28 of the clamps on the screw despite the differences of steps.
- Each rod thus receives a clamp 8 and the pivoting of the screw 9 causes the movement of the six different clamps.
- the clamps move away from each other.
- the end clamps connected to threaded rods c1 and c2 travel in translation a distance five times more large than the center clamps connected to the threaded rods a1 and a2.
- the intermediate clamps connected to threaded rods b1 and b2 travel a distance three times larger than the clamps connected to the threaded rods a1 and a2.
- the separation of the modules requires in this case a very weak rotation of the screw 9, for example 2 turns.
- the clamps secured to the stems c1 and c2 deviate from the clamps integral rods b1 and b2 respectively from a distance equal to d.
- the pace of stems c1 and c2 is equal to 5 times the pitch of the stems a1 and a2.
- This structure of the screw 9 thus allows a separation simultaneous six propellant charge modules that are all separated from each other by the same distance.
- the operation of the device according to the invention is the next.
- the gripping module 3 withdraws from the store 1 six modules recessed into each other, brings them up of the device 5 as shown in FIG. engages them in the upper part 6a of the box as shown in FIG. pairs of clamps 8 in order to immobilize each module 4. then controls the rotation of the screws 9 to cause the respective translation of the modules with respect to other.
- FIGs 9a and 9b are top views of the showing device for Figure 9a the clamps 8 now the modules in their linked position and for Figure 9b the untied modules after rotation of the screws 9a, 9b. We observe that the spacing between the different modules is the same after separation.
- the spacing of the clamps is controlled 8 and the separate modules fall by gravity into the zone of selection 10 as can be seen in the same figure 4.
- this zone 10 where is the means for selecting the modules, we control the switching of the selected modules in the meeting means 7 whose stop 16 is in position extreme with respect to the abutment 17. It then controls the translation of the mobile stop 16 to engage the head 23 a module in the bottom 25 of the adjacent module.
- the number of selected modules is never less than half the number of modules brought to the device according to the invention.
- the number of selected modules in the described embodiment is included between 3 and 6.
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- Apparatus Associated With Microorganisms And Enzymes (AREA)
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Abstract
Description
- la figure 1 représente une vue en perspective du dispositif selon l'invention accolé à un magasin de modules de charge propulsive,
- la figure 2 représente une vue en perspective du caisson où sont disposés le moyen de liaison, le moyen de séparation et la zone de rétention,
- la figure 3 représente une autre vue en perspective du dispositif selon l'invention,
- la figure 4 représente une autre vue en perspective de l'intérieur du caisson,
- la figure 5 représente une vue en perspective du moyen de réunion des modules, dépourvu de module,
- la figure 6 représente une vue en perspective du même moyen de réunion des modules avec un ensemble de modules, et
- la figure 7 représente une vue schématique externe du moyen de séparation des modules,
- la figure 8 montre en perspective un module maintenu par une paire de pinces, ces dernières étant représentées partiellement en coupe,
- les figures 9a et 9b sont deux vues de dessus du moyen de séparation, montrant pour la figure 9a les modules dans leur position liée et pour la figure 9b les modules déliés.
Claims (15)
- Dispositif de séparation (5) de modules (4) de charge propulsive pour armes de campagne, chaque module comportant une tête (23) et un fond (25), la tête d'un module étant engagée dans le fond d'un module adjacent, caractérisé en ce qu 'il comporte un moyen de réception de l'ensemble des modules comportant des moyens de blocage (8) de chaque module, ces moyens de blocage étant reliés par un moyen de liaison et séparation (9) permettant de commander une translation relative de chaque module par rapport à ses voisins assurant ainsi la séparation des modules.
- Dispositif selon la revendication 1, caractérisé en ce que les moyens de blocage (8) sont constitués d'un ensemble de paires de pinces (8a-8e) disposées de part et d'autres d'un module (4), chaque module étant maintenu par une paire de pinces, chaque paire de pinces étant commandée en translation par le moyen de liaison et séparation (9).
- Dispositif selon la revendication 2, caractérisé en ce que le moyen de liaison (9) comprend deux vis (9a, 9b) parallèles aux modules et comportant en regard de chaque module une tige filetée portant une pince (a1-c1, a2-c2), chaque vis (9a, 9b) étant liée à un moyen d'entraínement en rotation (20, 21).
- Dispositif selon la revendication 3, caractérisé en ce que chaque vis (9) comprend un premier groupe de tiges filetées (a1-c1) portant toutes des filetages de pas différents et de même sens, et un deuxième groupe de tiges filetées (a2-c2) portant toutes des filetages de pas différents et de même sens, mais dans le sens opposé à celui du premier groupe, le nombre de tiges filetées étant égal au nombre de modules (4) de charge propulsive.
- Dispositif selon la revendication 4, caractérisé en ce que les tiges filetées de chaque groupe ont des diamètres différents, les tiges d'extrémité ayant un diamètre inférieur à celui des tiges intermédiaires dont le diamètre est inférieur à celui des tiges médianes.
- Dispositif selon l'une des revendications 3 à 5, caractérisé en ce que les pinces sont constituées par des vérins comportant un corps solidaire d'une tige filetée et une mâchoire mobile par rapport au corps.
- Dispositif selon l'une quelconque des revendications précédentes, caractérisé en ce que les modules (4) séparés sont transférés dans une zone de sélection (10) comportant un moyen de sélection des modules pour faire basculer les modules choisis dans un moyen de réception (7).
- Dispositif selon la revendication 7, caractérisé en ce que ledit moyen (8) de liaison et de séparation et ladite zone de sélection (10) sont disposés dans un même caisson (6).
- Dispositif selon la revendication 7, caractérisé en ce que la zone de sélection (10) est munie de parois transversales (14) définissant un nombre de compartiments égal au nombre de modules de charge propulsive séparés par le moyen de séparation (8).
- Dispositif selon la revendication 7, caractérisé en ce que les modules (4) sont transférés dans la zone de sélection (10) par gravité.
- Dispositif selon la revendication 7, caractérisé en ce que le moyen de sélection des modules est constitué d'un ensemble de poussoirs, chaque poussoir étant commandé sélectivement.
- Dispositif selon la revendication 7, caractérisé en ce que le moyen de réception (7) comporte un godet de réception (17) des modules individuels, dont la forme est telle qu'elle assure le centrage coaxial des modules.
- Dispositif selon la revendication 12, caractérisé en ce que ledit moyen de réception (7) est muni d'un moyen de d'assemblage (16, 17) des modules (4) apte à engager la tête 23 d'un module dans le fond (25) du module adjacent.
- Dispositif selon la revendication 13, caractérisé en ce que ledit moyen d'assemblage des modules comprend une butée mobile (16) sous l'action d'un vérin et une contre-butée fixe (17) .
- Dispositif selon la revendication 14, caractérisé en ce que la contre-butée fixe (17) peut être basculée par rapport au moyen de réception (7).
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 true EP1596150A1 (fr) | 2005-11-16 |
EP1596150B1 EP1596150B1 (fr) | 2009-06-24 |
Family
ID=34942114
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05290809A Not-in-force EP1596150B1 (fr) | 2004-04-29 | 2005-04-13 | Dispositif de séparation de modules de charge propulsive |
Country Status (7)
Country | Link |
---|---|
US (1) | US7140300B2 (fr) |
EP (1) | EP1596150B1 (fr) |
AT (1) | ATE434750T1 (fr) |
DE (1) | DE602005015054D1 (fr) |
ES (1) | ES2328158T3 (fr) |
FR (1) | FR2869681B1 (fr) |
PL (1) | PL1596150T3 (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2945615A1 (fr) * | 2009-05-18 | 2010-11-19 | Nexter Systems | Dispositif de separation d'un ensemble de modules de charge propulsive |
DE102011050282B3 (de) * | 2011-05-11 | 2012-09-13 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Vorrichtung und Verfahren zum Portionieren einer Treibladung |
FR3057058A1 (fr) * | 2016-10-04 | 2018-04-06 | Nexter Systems | Dispositif de calage pour obus et casier apte a accueillir un tel dispositif |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE534616C2 (sv) * | 2009-10-21 | 2011-10-25 | Bae Systems Bofors Ab | Automatiserat laddningsmagasin |
DE102011055045B4 (de) * | 2011-11-04 | 2019-01-17 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Treibladungsportioniereinrichtung |
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 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5107751A (en) * | 1989-09-19 | 1992-04-28 | Rheinmetall Gmbh | Chute magazine for modular propelling charges |
US5111730A (en) * | 1989-09-18 | 1992-05-12 | Rheinmetall Gmbh | Apportioning apparatus for loading a loading tray with a variable number of propelling charge modules |
FR2743413A1 (fr) * | 1996-01-05 | 1997-07-11 | Giat Ind Sa | Systeme de stockage et d'alimentation de modules constituant des charges propulsives pour canon d'artillerie |
FR2743411A1 (fr) * | 1996-01-05 | 1997-07-11 | 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 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
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 |
-
2004
- 2004-04-29 FR FR0404560A patent/FR2869681B1/fr not_active Expired - Fee Related
-
2005
- 2005-04-13 AT AT05290809T patent/ATE434750T1/de not_active IP Right Cessation
- 2005-04-13 DE DE602005015054T patent/DE602005015054D1/de active Active
- 2005-04-13 ES ES05290809T patent/ES2328158T3/es active Active
- 2005-04-13 EP EP05290809A patent/EP1596150B1/fr not_active Not-in-force
- 2005-04-13 PL PL05290809T patent/PL1596150T3/pl unknown
- 2005-04-27 US US11/115,171 patent/US7140300B2/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5111730A (en) * | 1989-09-18 | 1992-05-12 | Rheinmetall Gmbh | Apportioning apparatus for loading a loading tray with a variable number of propelling charge modules |
US5107751A (en) * | 1989-09-19 | 1992-04-28 | Rheinmetall Gmbh | Chute magazine for modular propelling charges |
FR2743413A1 (fr) * | 1996-01-05 | 1997-07-11 | Giat Ind Sa | Systeme de stockage et d'alimentation de modules constituant des charges propulsives pour canon d'artillerie |
FR2743411A1 (fr) * | 1996-01-05 | 1997-07-11 | 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 |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2945615A1 (fr) * | 2009-05-18 | 2010-11-19 | Nexter Systems | Dispositif de separation d'un ensemble de modules de charge propulsive |
EP2253926A1 (fr) * | 2009-05-18 | 2010-11-24 | NEXTER Systems | Dispositif de séparation d'un ensemble de modules de charge propulsive |
DE102011050282B3 (de) * | 2011-05-11 | 2012-09-13 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Vorrichtung und Verfahren zum Portionieren einer Treibladung |
EP2522949A2 (fr) | 2011-05-11 | 2012-11-14 | Krauss-Maffei Wegmann GmbH & Co. KG | Dispositif et procédé de mise en portions d'une charge propulsive |
EP2522949A3 (fr) * | 2011-05-11 | 2014-12-17 | Krauss-Maffei Wegmann GmbH & Co. KG | Dispositif et procédé de mise en portions d'une charge propulsive |
FR3057058A1 (fr) * | 2016-10-04 | 2018-04-06 | Nexter Systems | Dispositif de calage pour obus et casier apte a accueillir un tel dispositif |
WO2018065713A1 (fr) * | 2016-10-04 | 2018-04-12 | Nexter Systems | Dispositif de calage pour obus et casier a charges propulsives apte a accueillir un tel dispositif |
Also Published As
Publication number | Publication date |
---|---|
US7140300B2 (en) | 2006-11-28 |
ATE434750T1 (de) | 2009-07-15 |
DE602005015054D1 (de) | 2009-08-06 |
EP1596150B1 (fr) | 2009-06-24 |
FR2869681B1 (fr) | 2006-07-28 |
ES2328158T3 (es) | 2009-11-10 |
PL1596150T3 (pl) | 2009-12-31 |
US20050241469A1 (en) | 2005-11-03 |
FR2869681A1 (fr) | 2005-11-04 |
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