EP2169341A1 - Manually retractable turret - Google Patents
Manually retractable turret Download PDFInfo
- Publication number
- EP2169341A1 EP2169341A1 EP09290676A EP09290676A EP2169341A1 EP 2169341 A1 EP2169341 A1 EP 2169341A1 EP 09290676 A EP09290676 A EP 09290676A EP 09290676 A EP09290676 A EP 09290676A EP 2169341 A1 EP2169341 A1 EP 2169341A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- active system
- arm
- cupola
- retractable
- box
- 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
- F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
- F41A23/20—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles for disappearing guns
Definitions
- the technical sector of the present invention is that of cupolas mounted on a platform.
- Turrets are known that equip a platform (vehicle, building, ...) and intended to support an active system consisting of offensive or defensive weapons and / or a remote viewing means such as an episcope or a camera.
- Gun-type devices are also known having several tubes mounted in battery. They are not steerable and have an important rigid structure capable of supporting the efforts.
- Deployable weapon systems are also known, but these weapon systems are not rechargeable from within a vehicle.
- the invention thus relates to a cupola mounted retractably and having manual deployment means to bring it into a position of use.
- the invention relates to a retractable turret rotatably mounted on a platform, comprising an active system which can be oriented in a site and in a bearing, a protective cover of the active system closing a box, characterized in that it comprises deployment means the active system consisting of a first and a second arm forming a deformable parallelogram disposed on either side of the active system and pointing means in elevation and location of said active system, the deployment being controlled by a first manual means actuating the first arm, the orientation in the site and bearing of the active system being controlled by a second manual means actuating the second arm.
- the first arm is rotatably connected to an axis integral with a support (18) fixed to the casing.
- the first manual means is constituted by a pinion and worm assembly connected to a control member for orienting the active system in position.
- the worm is secured to the axis of the first arm and the pinion is integral with the control member.
- control member is operable laterally to drive in rotation the pinion which drives the worm.
- the second arm is connected in rotation to an angle gear in the form of an integral L rotation of a support fixed to the box, an end of the L being connected to this second arm and the other end to an operating wheel for orienting in elevation said active system.
- the lid is connected to the active system by means of at least one fixing lug constituting a hinge, a spring means being provided allowing the lid to be pivoted so as to disengage a front face. the active system in the deployed position.
- the steering wheel is operable in two directions, one in a horizontal plane for positioning in position or direction the active system and the other in a vertical plane to position the active system in site or in elevation.
- the box forms a closed enclosure making it possible to seal between the outside and the inside of the platform, the box having an opening closed by a flap allowing access to the active system when the latter is in the retracted position.
- the active system is orientable at an angle of between -10 ° and 60 °.
- a first advantage of the cupola according to the invention lies in the fact that it occupies a reduced volume and therefore allows a possible reloading ammunition in all positions and over the entire gyration zone.
- Another advantage of the invention lies in the absence of the need for electrical energy to bring the cupola into its site and deposit positions.
- Yet another advantage of the invention lies in the fact that the on-site orientation only requires traction and extension of moderate amplitude and easily achievable by an operator even in a small space.
- cupola can support one or more active systems. These systems can be means of vision, weapons or defenses.
- this active system is represented by a multitubes block allowing firing of projectiles (for example masking or decoying).
- projectiles for example masking or decoying
- the cupolas are intended to equip a platform such as a vehicle or a fixed structure such as a building, where we can distinguish the exterior and the interior.
- the figure 1 represents in section a cupola 1 according to the invention fixed on a platform 2 by means of a bearing 3 allowing a 360 ° rotation of the cupola.
- sealing means (not shown), for example a seal, are provided between the cupola 1 and the platform 2 to isolate the interior thereof from the external environment.
- the cupola comprises a box 4 enclosing an active system 5 and connected thereto by a deformable parallelogram.
- the box 4 is closed by a protective cover 6 which is fixed to the active system 5 by a fixing lug 7 which constitutes a hinge.
- a spring means 43 is provided between the cover 6 and a rear leg 8 secured to the active system 5.
- the cover 6 pivots on its articulation and tilts by the action of the spring 43.
- Such an arrangement allows to release the front face of the active system 5 in the deployed position.
- the active system 5 is constituted here by a block provided with launch tubes 41 containing ammunition and closed at the rear by a cylinder head 9.
- the cylinder head 9 is shown in the open position by being connected to the block by an articulation 10.
- the block is accessible to load ammunition from the inside of the platform 2 where are the cupola servers.
- the bolt 9 comprising a percussion system is locked at the rear of the block and ensures the firing chain of the selected munition. Unlocking means to unlock this bolt.
- the deformable parallelogram consists of a set of arms arranged on either side of the system 5. In the figure there is a single pair of arms, a first arm 11 and a second arm 12. This parallelogram constitutes the means of deployment of the active system 5 to bring it from the folded or closed position shown in this figure to an extended position described below.
- the arms 11 and 12 are connected to the system 5 by the respective hinges 13 and 14 and to the box 4 by the respective hinges 15 and 16.
- the first arm 11 is secured to an axis 17 ( figure 5 ) which pivots at the joints 15 with respect to two supports 18 fixed to the box 4 (see figure 5 ).
- the hinge 16 of the second arm 12 is connected to a bevel gear 19 in the form of a pivoting L on a 20a axis integral with a support 20 fixed to the box 4.
- One end 21 of the L is connected to the second arm 12 by a hinge 16 and the other end 22 is integral with a steering wheel 23 for maneuvering said active system in elevation 5.
- the steering wheel 23 can be maneuvered along the two directions Y and Z.
- the steering wheel 23 is fixed relative to the casing 4. It is then possible to manually rotate the casing 4 on the bearing 3 so as to orient in bearing (or direction) this box 4 (and the system 5).
- the pivoting can be carried out 360 ° thanks to the bearing 3.
- the system 4 can be oriented bearing at any time by the servant occupying the interior of the platform in any direction.
- the flywheel 23 which is integral with the reference 19 can pivot about the axis 20a to move the second arm 12 as will be explained below and thus guide in site (or elevation) the system 5.
- the parallelogram can also be deformed to move from the folded position shown on the figure 1 in the deployed position shown on the figure 2 .
- the first manual means 24 consists of an assembly comprising a pinion 31 meshing with a worm 30.
- the worm 30 is secured to the axis 17 ( figure 5 ) which is itself secured to the first arm 11. A rotation of the worm 30 thus causes the pivoting of the arm 11 on the hinges 15 relative to the supports 18.
- the pinion 31 is rotationally integral with an axis 32 which can pivot relative to the casing 4 on bearings (not shown).
- the axis 32 is also integral with a control member 25 having a handle 25a. A manual action on the handle 25a makes it possible to rotate in a horizontal plane (arrows S1, S2 - figure 5 ) the controller 25 which rotates the shaft 32 on its bearings and the pinion 31.
- control member 25 in a median position. It is clear that this member can pivot with the axis 32 in the directions S1 and S2 until the abutment of the handle 25a on a diametrical bar 42 secured to the wheel 23.
- a first direction S1 will then be the direction of maneuver for the deployment of the system 5 and the opposite direction S2 will be that adopted for the folding of the system 5.
- the angular travel of the member 25 will then be close to 90 °.
- the skilled person will define the pinion 31 and the screw 30 so that a pivoting of the control member 25 by an angle of about 80 to 90 ° ensures the complete deployment of the system.
- the pinion 31 is engaged in the worm 30. By its rotation, it rotates the latter which causes the rotation of the first arm 11 and the deployment of the system 5 out of the box 4.
- FIG. 2 we have shown an extended position of the system 5.
- This figure shows the screw 30 attached to the arm 11 and the pinion 31 integral with the axis 32, pivoting relative to the box 4, and integral with the control member 25
- the pinion 31 is rotated and consequently the first arm 11 moves from the folded position shown on FIG. figure 1 at the deployed position of the figure 2 .
- the cover 6 has tilted with respect to the system 5 by the action of the spring 43. The cover thus occupies its second position and makes it possible to avoid any interference between the ejected munitions and the cover 6.
- FIG. 3 there is shown an extended position of the system 5 with low orientation in site, position according to which the steering wheel 23 has been maneuvered tilting in the direction Z1 through the rotation of the bevel gear 19 around the axis 20a through a slot 44 of the box 4.
- the angle gear then translates the second arm 12 in a high extreme position without changing the position of the first arm 11.
- This rotation can bring the system 5 at a negative elevation angle of about -5 ° to the horizontal.
- the system 5 can be oriented in all the intermediate positions.
- FIG 4 there is shown an extended position of the system 5 with elevation in elevation, position according to which the steering wheel 23 has been manipulated in elevation in the direction Z2 through the rotation of the bevel gear 19 about the axis 20a.
- the angle gear 19 then drives in translation the second arm 12 in an extreme low position without changing the position of the first arm 11. This rotation makes it possible to bring the system 5 at an angle of elevation of about + 60 °.
- the system 5 can be oriented in all intermediate positions.
- the cupola according to the invention makes it possible to bring an active system from a folded position to an extended position (thanks to the member 25) and that, moreover, it makes it possible (with the steering wheel 23) to adjust the site ( elevation) of the system following an angular range of -5 ° to + 60 ° as well as the following deposit 360 °.
- the adjustment in elevation can be carried out in any position in the bearing of the system by simple manual maneuvers of the flywheel 23.
- the angle gear 19 By adding to the second arm 12 the angle gear 19, the orientation in elevation is ensured. ) keeping a compactness of the assembly to house it in the box 4.
- the manual controls 23 and 25 of the active system 5 make it possible to dispense with any means requiring electrical energy ensuring the availability of the cupola whatever the circumstances.
- FIG 5 there is shown a view to see the interior of the box 4.
- the system 5 is in the deployed position and the box 4 is provided with an opening 40 through which the system 5 can be reloaded in ammunition on the inner side of Turret after retraction of its cylinder head 9.
- This opening 40 can be closed by a shutter not shown in order to sealingly close the box 4.
- the first arms 11 are in the form of a U-shaped frame 11a fixed on either side of the cover 6, which frame is connected to the axis 17 by a single arm 11b.
- This embodiment makes it possible to implement a single pinion 31 / worm gear system 30 without any modification of the operation.
- the cupola is shown in a bottom view where we see the steering wheel 23, the control member 25, the angle returns 19a and 19b integral with a diametral bar 42 fixed to the steering wheel 23 and a slot 44.
- the brackets 7 hooking system 5 to cover 6 and its multiple tubes 41 We still see the realization of the frame 11a.
- This figure also shows the end of the axis 32 on which the control member 25 is fixed.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Lock And Its Accessories (AREA)
- Mechanical Pencils And Projecting And Retracting Systems Therefor, And Multi-System Writing Instruments (AREA)
- Steering Devices For Bicycles And Motorcycles (AREA)
- Gear Transmission (AREA)
- Manipulator (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Blinds (AREA)
Abstract
L'invention concerne un tourelleau escamotable (1) monté rotatif sur une plate-forme (2), comprenant un système actif (5) orientable en site et en gisement, un capot (6) de protection du système actif fermant un caisson (4). Il comporte des moyens de déploiement du système actif constitués par un premier et un second bras (11, 12) formant un parallélogramme déformable disposés de part et d'autre du système actif (5) et des moyens de pointage en site et en gisement (23, 25) dudit système actif, le déploiement étant commandé par un premier moyen manuel (24, 25) actionnant le premier bras (11), l'orientation en site et en gisement du système actif étant commandé par un second moyen manuel (19, 30) actionnant le second bras (12). Application aux véhicules militairesThe invention relates to a retractable turret (1) rotatably mounted on a platform (2), comprising an active system (5) orientable in a site and in a bearing, a cover (6) for protecting the active system closing a box (4). ). It comprises deployment means of the active system consisting of a first and a second arm (11, 12) forming a deformable parallelogram arranged on either side of the active system (5) and pointing means in site and on the bearing ( 23, 25) of said active system, the deployment being controlled by a first manual means (24, 25) actuating the first arm (11), the orientation in elevation and bearing of the active system being controlled by a second manual means (19). , 30) actuating the second arm (12). Application to military vehicles
Description
Le secteur technique de la présente invention est celui des tourelleaux montés sur une plate-forme.The technical sector of the present invention is that of cupolas mounted on a platform.
On connaît des tourelleaux équipant une plate-forme (véhicule, bâtiment ,...) et destinés à supporter un système actif constitué d'armes offensives ou défensives et/ou d'un moyen de vision déportée tel un épiscope ou une caméra. On connaît également des dispositifs de type canons présentant plusieurs tubes montés en batterie. Ils ne sont pas orientables et présentent une importante structure rigide capable de supporter les efforts. On connaît également des systèmes d'armes déployables, mais ces systèmes d'armes ne sont pas rechargeables depuis l'intérieur d'un véhicule.Turrets are known that equip a platform (vehicle, building, ...) and intended to support an active system consisting of offensive or defensive weapons and / or a remote viewing means such as an episcope or a camera. Gun-type devices are also known having several tubes mounted in battery. They are not steerable and have an important rigid structure capable of supporting the efforts. Deployable weapon systems are also known, but these weapon systems are not rechargeable from within a vehicle.
L'invention se rapporte donc à un tourelleau monté de manière escamotable et comportant des moyens de déploiement manuel afin de l'amener dans une position d'utilisation.The invention thus relates to a cupola mounted retractably and having manual deployment means to bring it into a position of use.
L'invention a pour objet un tourelleau escamotable monté rotatif sur une plate-forme, comprenant un système actif orientable en site et en gisement, un capot de protection du système actif fermant un caisson, caractérisé en ce qu'il comporte des moyens de déploiement du système actif constitués par un premier et un second bras formant un parallélogramme déformable disposés de part et d'autre du système actif et des moyens de pointage en site et en gisement dudit système actif, le déploiement étant commandé par un premier moyen manuel actionnant le premier bras, l'orientation en site et en gisement du système actif étant commandé par un second moyen manuel actionnant le second bras.The invention relates to a retractable turret rotatably mounted on a platform, comprising an active system which can be oriented in a site and in a bearing, a protective cover of the active system closing a box, characterized in that it comprises deployment means the active system consisting of a first and a second arm forming a deformable parallelogram disposed on either side of the active system and pointing means in elevation and location of said active system, the deployment being controlled by a first manual means actuating the first arm, the orientation in the site and bearing of the active system being controlled by a second manual means actuating the second arm.
Selon une caractéristique de l'invention, le premier bras est relié en rotation à un axe solidaire d'un support (18) fixé au caisson.According to a feature of the invention, the first arm is rotatably connected to an axis integral with a support (18) fixed to the casing.
Selon une autre caractéristique de l'invention, le premier moyen manuel est constitué par un ensemble pignon et vis sans fin relié à un organe de commande pour orienter en gisement le système actif.According to another characteristic of the invention, the first manual means is constituted by a pinion and worm assembly connected to a control member for orienting the active system in position.
Selon une autre caractéristique de l'invention, la vis sans fin est solidaire de l'axe donc du premier bras et le pignon est solidaire de l'organe de commande.According to another characteristic of the invention, the worm is secured to the axis of the first arm and the pinion is integral with the control member.
Selon une autre caractéristique de l'invention, l'organe de commande est manoeuvrable latéralement pour entraîner en rotation le pignon qui entraîne la vis sans fin.According to another characteristic of the invention, the control member is operable laterally to drive in rotation the pinion which drives the worm.
Selon une autre caractéristique de l'invention, le second bras est relié en rotation à un renvoi d'angle se présentant sous la forme d'un L solidaire en rotation d'un support fixé au caisson, une extrémité du L étant reliée à ce second bras et l'autre extrémité à un volant de manoeuvre pour orienter en site ledit système actif.According to another characteristic of the invention, the second arm is connected in rotation to an angle gear in the form of an integral L rotation of a support fixed to the box, an end of the L being connected to this second arm and the other end to an operating wheel for orienting in elevation said active system.
Selon une autre caractéristique de l'invention, le couvercle est relié au système actif par l'intermédiaire d'au moins une patte de fixation constituant une articulation, un moyen ressort étant prévu permettant de faire pivoter le couvercle de façon à dégager une face avant du système actif en position déployée.According to another characteristic of the invention, the lid is connected to the active system by means of at least one fixing lug constituting a hinge, a spring means being provided allowing the lid to be pivoted so as to disengage a front face. the active system in the deployed position.
Selon une autre caractéristique de l'invention, le volant est manoeuvrable suivant deux directions, l'une dans un plan horizontal pour positionner en gisement ou direction le système actif et l'autre dans un plan vertical pour positionner le système actif en site ou en élévation.According to another characteristic of the invention, the steering wheel is operable in two directions, one in a horizontal plane for positioning in position or direction the active system and the other in a vertical plane to position the active system in site or in elevation.
Selon une autre caractéristique de l'invention, le caisson forme une enceinte fermée permettant d'assurer l'étanchéité entre l'extérieur et l'intérieur de la plate-forme, le caisson comportant une ouverture fermée par un volet permettant d'accéder au système actif lorsque ce dernier est en position escamotée.According to another characteristic of the invention, the box forms a closed enclosure making it possible to seal between the outside and the inside of the platform, the box having an opening closed by a flap allowing access to the active system when the latter is in the retracted position.
Selon une autre caractéristique de l'invention, le système actif est orientable en site selon un angle compris entre -10° et 60°.According to another characteristic of the invention, the active system is orientable at an angle of between -10 ° and 60 °.
Un tout premier avantage du tourelleau selon l'invention réside dans le fait qu'il occupe un volume réduit et autorise de ce fait un rechargement possible en munitions dans toute les positions et sur la totalité de la zone de giration.A first advantage of the cupola according to the invention lies in the fact that it occupies a reduced volume and therefore allows a possible reloading ammunition in all positions and over the entire gyration zone.
Un autre avantage de l'invention réside dans l'absence de besoin en énergie électrique pour amener le tourelleau dans ses positions de site et de gisement.Another advantage of the invention lies in the absence of the need for electrical energy to bring the cupola into its site and deposit positions.
Un autre avantage encore de l'invention réside dans le fait que l'orientation en site ne nécessite que des mouvements de traction et d'extension d'amplitude modérée et facilement réalisables par un opérateur même dans un espace réduit.Yet another advantage of the invention lies in the fact that the on-site orientation only requires traction and extension of moderate amplitude and easily achievable by an operator even in a small space.
D'autres caractéristiques, détails et avantages de l'invention ressortiront plus clairement de la description détaillée donnée ci-après à titre indicatif en relation avec des vues perspectives sur lesquelles:
- la
figure 1 représente le tourelleau selon l'invention en position repliée, - la
figure 2 représente le tourelleau selon l'invention en position déployée, - la
figure 3 montre le tourelleau selon l'invention orienté en site en position extrême basse, - la
figure 4 représente le tourelleau orienté en site en position extrême haute, - la
figure 5 est une vue montrant l'intérieur du tourelleau, et - la
figure 6 est une vue montrant la paroi inférieure du tourelleau.
- the
figure 1 represents the cupola according to the invention in the folded position, - the
figure 2 represents the cupola according to the invention in the deployed position, - the
figure 3 shows the cupola according to the invention oriented in situ in the extreme low position, - the
figure 4 represents the site-oriented turret in the extreme high position, - the
figure 5 is a view showing the inside of the cupola, and - the
figure 6 is a view showing the bottom wall of the cupola.
Il est connu que les tourelleaux peuvent supporter un ou plusieurs systèmes actifs. Ces systèmes peuvent être des moyens de vision, des armes ou des moyens de défense. Dans les exemples de réalisation décrits par la suite, ce système actif est représenté par un bloc multitubes permettant le tir de projectiles (par exemple de masquage ou de leurrage). Bien entendu, cet exemple n'est pas limitatif et on pourra remplacer ce bloc multitube par n'importe quel autre système actif. Les tourelleaux sont destinées à équiper une plate-forme telle un véhicule ou une structure fixe telle un bâtiment, où on distinguera l'extérieur et l'intérieur.It is known that cupola can support one or more active systems. These systems can be means of vision, weapons or defenses. In the embodiments described hereinafter, this active system is represented by a multitubes block allowing firing of projectiles (for example masking or decoying). Of course, this example is not limiting and we can replace this multitube block by any other active system. The cupolas are intended to equip a platform such as a vehicle or a fixed structure such as a building, where we can distinguish the exterior and the interior.
La
Sur la
Le système actif 5 est constitué ici par un bloc muni de tubes de lancement 41 renfermant des munitions et fermé à l'arrière par une culasse 9. Sur la figure, la culasse 9 est représentée en position ouverte en étant reliée au bloc par une articulation 10. En position ouverte, le bloc est accessible afin de le charger en munitions à partir de l'intérieur de la plate-forme 2 où se trouvent les servants du tourelleau. La culasse mobile 9 comprenant un système de percussion est verrouillée en partie arrière du bloc et assure la chaîne de mise à feu de la munition sélectionnée. Un moyen de déverrouillage permet de déverrouiller cette culasse mobile.The
Le parallélogramme déformable est constitué par un ensemble de bras disposés de part et d'autre du système 5. Sur la figure on voit une seule paire de bras, un premier bras 11 et un second bras 12. Ce parallélogramme constitue le moyen de déploiement du système actif 5 pour l'amener de la position repliée ou fermée représentée sur cette figure à une position déployée décrite ci-après. Les bras 11 et 12 sont reliés au système 5 par les articulations respectives 13 et 14 et au caisson 4 par les articulations respectives 15 et 16.The deformable parallelogram consists of a set of arms arranged on either side of the
Le premier bras 11 est solidaire d'un axe 17 (
Le volant 23 est manoeuvrable suivant les deux directions Y et Z.The
Suivant la direction Y sensiblement horizontale et qui est perpendiculaire au plan de la
Suivant la direction Z qui est dans le plan de la
Le parallélogramme peut par ailleurs être déformé pour passer de la position repliée montrée sur la
Pour cela un premier moyen manuel permet de faire pivoter le premier bras 11 sur son articulation 15. Le premier moyen manuel 24 est constitué par un ensemble comprenant un pignon 31 engrenant avec une vis sans fin 30.For this purpose a first manual means makes it possible to pivot the
La vis sans fin 30 est solidaire de l'axe 17 (
Le pignon 31 est solidaire en rotation d'un axe 32 qui peut pivoter par rapport au caisson 4 sur des paliers (non représentés). L'axe 32 est par ailleurs solidaire d'un organe de commande 25 doté d'une poignée 25a. Une action manuelle sur la poignée 25a permet de faire pivoter dans un plan horizontal (flèches S1, S2 -
Pour améliorer la clarté des
Afin d'utiliser la course angulaire maximale disponible pour l'organe 25, ce dernier se trouvera donc avec sa poignée 25a en butée contre la barre 42 dans ses positions repliée et déployée. Un premier sens S1 sera alors le sens de manoeuvre pour le déploiement du système 5 et le sens inverse S2 sera celui adopté pour le repliement du système 5. La course angulaire de l'organe 25 sera alors voisine de 90°. L'Homme du Métier définira le pignon 31 et la vis 30 de telle sorte qu'un pivotement de l'organe de commande 25 d'un angle d'environ 80 à 90° assure le déploiement complet du système.In order to use the maximum angular travel available for the
Le pignon 31 est engagé dans la vis sans fin 30. Par sa rotation, il fait donc pivoter cette dernière ce qui provoque la rotation du premier bras 11 et le déploiement du système 5 hors du caisson 4.The
Sur la
Sur la
Sur la
On voit que le tourelleau selon l'invention permet d'amener un système actif d'une position repliée à une position déployée (grâce à l'organe 25) et que par ailleurs il permet (avec le volant 23) de régler le site (élévation) du système suivant une plage angulaire de -5° à +60° ainsi que le gisement suivant 360°.It can be seen that the cupola according to the invention makes it possible to bring an active system from a folded position to an extended position (thanks to the member 25) and that, moreover, it makes it possible (with the steering wheel 23) to adjust the site ( elevation) of the system following an angular range of -5 ° to + 60 ° as well as the following deposit 360 °.
Le réglage en site peut être réalisé dans n'importe quelle position en gisement du système par de simples manoeuvres manuelles du volant 23. Ainsi, en adjoignant au second bras 12 le renvoi d'angle 19, on assure l'orientation en site (élévation) en conservant une compacité de l'ensemble pour le loger dans le caisson 4.The adjustment in elevation can be carried out in any position in the bearing of the system by simple manual maneuvers of the
Les commandes manuelles 23 et 25 du système actif 5 permettent de s'affranchir de tout moyen nécessitant de l'énergie électrique assurant la disponibilité du tourelleau quelles que soient les circonstances.The manual controls 23 and 25 of the
Sur la
Sur la
L'homme du métier déterminera de manière simple la réalisation des bras constituant le parallélogramme de manière à assurer la résistance nécessaire pour absorber les contraintes de tir des munitions. Ces munitions peuvent être identiques ou différentes, de même calibre ou de calibre différent.The skilled person will determine in a simple manner the realization of the arms constituting the parallelogram so as to provide the necessary resistance to absorb the firing constraints of ammunition. These ammunition may be identical or different, of the same caliber or different caliber.
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL09290676T PL2169341T3 (en) | 2008-09-24 | 2009-09-07 | Manually retractable turret |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0805234A FR2936305B1 (en) | 2008-09-24 | 2008-09-24 | MANUALLY RETRACTABLE TURRET |
Publications (2)
Publication Number | Publication Date |
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EP2169341A1 true EP2169341A1 (en) | 2010-03-31 |
EP2169341B1 EP2169341B1 (en) | 2011-06-22 |
Family
ID=40688310
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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EP09290676A Active EP2169341B1 (en) | 2008-09-24 | 2009-09-07 | Manually retractable turret |
Country Status (5)
Country | Link |
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US (1) | US8393258B2 (en) |
EP (1) | EP2169341B1 (en) |
AT (1) | ATE514046T1 (en) |
FR (1) | FR2936305B1 (en) |
PL (1) | PL2169341T3 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2746714A3 (en) * | 2012-12-22 | 2016-07-20 | Diehl BGT Defence GmbH & Co.KG | Container for missile |
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8584573B2 (en) * | 2010-02-04 | 2013-11-19 | Quantum Fuel Systems Technologies Worldwide Inc. | Orbital device with stowable mount |
DE102010060192B9 (en) * | 2010-10-26 | 2013-01-24 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Fastening device and vehicle |
ITTO20110455A1 (en) * | 2011-05-25 | 2012-11-26 | Oto Melara Spa | TURRET ASSEMBLY AND WEAPON WITH LOW REFLECTION RADAR. |
WO2013183047A1 (en) | 2012-06-04 | 2013-12-12 | Rafael Advanced Defense Systems Ltd. | Remote controlled non-lethal weapon station |
DE102013101635A1 (en) | 2013-02-19 | 2014-08-21 | Krauss-Maffei Wegmann Gmbh & Co. Kg | weapon station |
US10371479B2 (en) * | 2013-09-11 | 2019-08-06 | Merrill Aviation, Inc. | Stabilized integrated commander's weapon station for combat armored vehicle |
MX2018003811A (en) * | 2015-09-29 | 2019-07-18 | Frank Russell | Camper shell turret system. |
CN110998219A (en) * | 2017-08-17 | 2020-04-10 | 麦可吉国防工业有限公司 | Rocket projectile launching module and rocket projectile launching carrier |
US10309745B2 (en) * | 2017-11-09 | 2019-06-04 | Samuel Messinger | Mobile turret weapon delivery system |
DE202018103226U1 (en) * | 2018-06-08 | 2018-10-11 | Rheinmetall Landsysteme Gmbh | Additional system arrangement for a vehicle |
ES2943576T3 (en) | 2018-11-28 | 2023-06-14 | John Cockerill Defense S A | Turret with retractable protective roof |
ES2904307T3 (en) * | 2019-02-21 | 2022-04-04 | John Cockerill Defense S A | Stealth vehicle with integrated rapid deployment weapon system |
US20220397365A1 (en) * | 2021-06-11 | 2022-12-15 | Alexander RIVERA | Turret apparatus |
US12123672B1 (en) * | 2023-06-20 | 2024-10-22 | United States Of America, As Represented By The Secretary Of The Navy | Modular tube-stowable rifle mount |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB118669A (en) * | 1917-09-04 | 1918-09-04 | Edouard Nieuwenhuyse | Improvements in Gun Mountings. |
FR494292A (en) * | 1917-02-14 | 1919-09-04 | Louis Pierre Jacques Chapplain | Auto Eclipse Trench Cannon |
DE932297C (en) * | 1952-03-20 | 1955-08-29 | Fritz Beeck | Panzer-Spaehwagen with a height-adjustable armored pulpit |
FR2149637A6 (en) * | 1963-11-28 | 1973-03-30 | Aerospatiale | |
DE4304761A1 (en) * | 1993-02-17 | 1994-08-18 | Mak System Gmbh | Gun mount for armored vehicles |
WO2004097325A2 (en) * | 2003-01-21 | 2004-11-11 | United Defense, L.P. | Pop-up weapon system |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1259737B (en) * | 1964-11-06 | 1968-01-25 | Boelkow Gmbh | Launching and loading device for recoil-propelled missiles, which can be launched individually one after the other or at the same time from adjustable interchangeable magazines |
US3757635A (en) * | 1971-03-23 | 1973-09-11 | F Hickerson | Multi-purpose munitions carrier |
US3865009A (en) * | 1973-09-13 | 1975-02-11 | Us Navy | Launcher mount |
FR2380527A2 (en) * | 1977-02-11 | 1978-09-08 | Creusot Loire | MISSILES LAUNCHING INSTALLATION |
US4282794A (en) * | 1979-04-30 | 1981-08-11 | Miller Avy L | Self-propelled off-road vehicle |
US4481862A (en) * | 1982-07-13 | 1984-11-13 | Fmc Corporation | Automatic loading system for fixed ammunition at gun elevation |
US4574685A (en) * | 1983-06-22 | 1986-03-11 | Am General Corporation | Turret system for lightweight military vehicle |
DE3440041A1 (en) * | 1984-11-02 | 1986-05-07 | Rheinmetall GmbH, 4000 Düsseldorf | HIGH-SWIVEL HEAD Grease for the weapon barrel of a battle tank |
DE3603623A1 (en) * | 1986-02-06 | 1987-08-13 | Salgad Int Ltd | ALTITUDE DEVICE FOR THE BULLET PIPE OF A GRENADE LAUNCHER |
GB8817274D0 (en) * | 1988-07-20 | 1988-12-14 | Marconi Co Ltd | Weapon systems |
US5129308A (en) * | 1989-03-21 | 1992-07-14 | Fuereder Georg F | Combat vehicle with extendible combat platform |
DE4401587A1 (en) * | 1994-01-20 | 1995-07-27 | Wegmann & Co Gmbh | Combat vehicle and transport system for loading it onto transport aircraft |
US6584881B1 (en) * | 2001-03-26 | 2003-07-01 | United Defense Lp | Multi-purpose missile launcher system for a military land vehicle |
DE50214510D1 (en) * | 2001-08-30 | 2010-08-12 | Krauss Maffei Wegmann Gmbh & C | ARTILLERY PROTECTION WITH A HEAVY WEAPON ARRANGED ON A TRUCK VEHICLE |
DE20214679U1 (en) * | 2002-09-23 | 2004-02-19 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Device for adapting a container containing several artillery rockets to a launching device for artillery rockets |
US7669513B2 (en) * | 2003-10-09 | 2010-03-02 | Elbit Systems Ltd. | Multiple weapon system for armored vehicle |
ITMI20060668A1 (en) * | 2006-04-05 | 2007-10-06 | Oto Melara Spa | AUXILIARY STORAGE DEVICE |
US8146479B2 (en) * | 2009-09-10 | 2012-04-03 | Nexter Systems | Retractable light turret |
-
2008
- 2008-09-24 FR FR0805234A patent/FR2936305B1/en not_active Expired - Fee Related
-
2009
- 2009-09-07 AT AT09290676T patent/ATE514046T1/en active
- 2009-09-07 EP EP09290676A patent/EP2169341B1/en active Active
- 2009-09-07 PL PL09290676T patent/PL2169341T3/en unknown
- 2009-09-23 US US12/585,726 patent/US8393258B2/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR494292A (en) * | 1917-02-14 | 1919-09-04 | Louis Pierre Jacques Chapplain | Auto Eclipse Trench Cannon |
GB118669A (en) * | 1917-09-04 | 1918-09-04 | Edouard Nieuwenhuyse | Improvements in Gun Mountings. |
DE932297C (en) * | 1952-03-20 | 1955-08-29 | Fritz Beeck | Panzer-Spaehwagen with a height-adjustable armored pulpit |
FR2149637A6 (en) * | 1963-11-28 | 1973-03-30 | Aerospatiale | |
DE4304761A1 (en) * | 1993-02-17 | 1994-08-18 | Mak System Gmbh | Gun mount for armored vehicles |
WO2004097325A2 (en) * | 2003-01-21 | 2004-11-11 | United Defense, L.P. | Pop-up weapon system |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2746714A3 (en) * | 2012-12-22 | 2016-07-20 | Diehl BGT Defence GmbH & Co.KG | Container for missile |
Also Published As
Publication number | Publication date |
---|---|
US20100071540A1 (en) | 2010-03-25 |
US8393258B2 (en) | 2013-03-12 |
ATE514046T1 (en) | 2011-07-15 |
PL2169341T3 (en) | 2011-11-30 |
FR2936305A1 (en) | 2010-03-26 |
FR2936305B1 (en) | 2010-10-22 |
EP2169341B1 (en) | 2011-06-22 |
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