EP2169341B1 - Von Hand versenkbare Luke - Google Patents
Von Hand versenkbare Luke Download PDFInfo
- Publication number
- EP2169341B1 EP2169341B1 EP09290676A EP09290676A EP2169341B1 EP 2169341 B1 EP2169341 B1 EP 2169341B1 EP 09290676 A EP09290676 A EP 09290676A EP 09290676 A EP09290676 A EP 09290676A EP 2169341 B1 EP2169341 B1 EP 2169341B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- active system
- arm
- elevation
- turret
- retractable
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 230000001681 protective effect Effects 0.000 claims description 3
- 238000007789 sealing Methods 0.000 claims description 2
- 210000000056 organ Anatomy 0.000 claims 3
- 230000003213 activating effect Effects 0.000 claims 2
- 230000005540 biological transmission Effects 0.000 abstract 1
- 238000010304 firing Methods 0.000 description 3
- 230000007123 defense Effects 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 230000000873 masking effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000009527 percussion Methods 0.000 description 1
Images
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 see eg the document DE932297C .
- 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.
Landscapes
- 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)
- Gear Transmission (AREA)
- Steering Devices For Bicycles And Motorcycles (AREA)
- Manipulator (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Blinds (AREA)
Claims (10)
- Versenkbarer Drehturm (1), der drehbar auf einer Plattform (2) montiert ist, umfassend ein aktives System (5), das in vertikaler und horizontaler Richtung ausrichtbar ist, eine Haube (6) zum Schutz des aktiven Systems, die einen Kasten (4) verschließt, dadurch gekennzeichnet, dass er Mittel zum Entfalten des aktiven Systems, die von einem ersten und einem zweiten Arm (11, 12) gebildet werden, die ein verformbares Parallelogramm bilden und beiderseits des aktiven Systems (5) angeordnet sind, und Mittel zum Richten in vertikaler und horizontaler Richtung (23, 25) des sogenannten aktiven Systems umfasst, wobei das Entfalten durch ein erstes, manuelles, den ersten Arm (11) betätigendes Mittel (24, 25) gesteuert wird, wobei die Ausrichtung in vertikaler und horizontaler Richtung des aktiven Systems durch ein zweites manuelles, den zweiten Arm (12) betätigendes Mittel (19, 30) gesteuert wird.
- Versenkbarer Drehturm (1) nach Anspruch 1, dadurch gekennzeichnet, dass der erste Arm (11) drehbar mit einer Achse (15) verbunden ist, die fest mit einem am Kasten (4) befestigten Träger (18) verbunden ist.
- Versenkbarer Drehturm (1) nach Anspruch 2, dadurch gekennzeichnet, dass das erste manuelle Mittel (24, 25) von einer Einheit (24) aus Ritzel (31) und Endlosschraube (30) gebildet wird, die mit einem Steuerorgan (25) verbunden ist, um das aktive System (5) in horizontaler Richtung auszurichten.
- Versenkbarer Drehturm (1) nach Anspruch 3, dadurch gekennzeichnet, dass die Endlosschraube (30) fest mit der Achse (15) und somit dem ersten Arm (11) verbunden und das Ritzel (31) fest mit dem Steuerorgan (25) verbunden ist.
- Versenkbarer Drehturm (1) nach Anspruch 3 oder 4, dadurch gekennzeichnet, dass das Steuerorgan (25) seitlich betätigbar ist, um das Ritzel (31), welches die Endlosschraube (24) antreibt, in Drehung zu versetzen.
- Versenkbarer Drehturm (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der zweite Arm (12) drehbar mit einem Winkelgetriebe (19) verbunden ist, das sich in der Form eines L darstellt, das drehfest mit einem am Kasten (4) befestigten Träger (20) verbunden ist, wobei ein Ende (21) des L mit diesem zweiten Arm (12) und das andere Ende (22) mit einem Steuer-Handrad (23) verbunden ist, um das sogenannte aktive System (5) in vertikaler Richtung auszurichten.
- Versenkbarer Drehturm (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Deckel (6) mit Hilfe wenigstens einer Befestigungslasche (7), die ein Gelenk bildet, mit dem aktiven System (5) verbunden ist, wobei ein Federmittel (43) vorgesehen ist, das es ermöglicht, den Deckel (6) derartig zu drehen, dass eine vordere Fläche des aktiven Systems in entfalteter Position freigegeben wird.
- Versenkbarer Drehturm (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das Handrad (23) in zwei Richtungen betätigbar ist, die eine in einer horizontalen Ebene, um das aktive System (5) in horizontaler Richtung zu positionieren, und die andere in einer vertikalen Ebene, um das aktive System (5) in vertikaler Richtung oder Elevation zu positionieren.
- Versenkbarer Drehturm (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Kasten (4) ein geschlossenes Gehäuse bildet, das es ermöglicht, die Dichtigkeit zwischen dem Außenbereich und dem Inneren der Plattform (1) zu gewährleisten, wobei der Kasten eine von einer Klappe verschlossene Öffnung (40) umfasst, die es ermöglicht, zu dem aktiven System (5) zu gelangen, wenn dieses Letztere sich in eingefahrener Position befindet.
- Versenkbarer Drehturm (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das aktive System (5) in vertikaler Richtung in einem Winkel ausrichtbar ist, der zwischen -10° und 60° liegt.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL09290676T PL2169341T3 (pl) | 2008-09-24 | 2009-09-07 | Ręcznie chowana wieżyczka |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0805234A FR2936305B1 (fr) | 2008-09-24 | 2008-09-24 | Tourelleau escamotable manuellement |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2169341A1 EP2169341A1 (de) | 2010-03-31 |
EP2169341B1 true EP2169341B1 (de) | 2011-06-22 |
Family
ID=40688310
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09290676A Active EP2169341B1 (de) | 2008-09-24 | 2009-09-07 | Von Hand versenkbare Luke |
Country Status (5)
Country | Link |
---|---|
US (1) | US8393258B2 (de) |
EP (1) | EP2169341B1 (de) |
AT (1) | ATE514046T1 (de) |
FR (1) | FR2936305B1 (de) |
PL (1) | PL2169341T3 (de) |
Families Citing this family (14)
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 (de) * | 2010-10-26 | 2013-01-24 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Befestigungsvorrichtung und Fahrzeug |
ITTO20110455A1 (it) * | 2011-05-25 | 2012-11-26 | Oto Melara Spa | Assieme di torretta e arma a bassa riflessione radar. |
WO2013183047A1 (en) | 2012-06-04 | 2013-12-12 | Rafael Advanced Defense Systems Ltd. | Remote controlled non-lethal weapon station |
DE102012025316B4 (de) * | 2012-12-22 | 2016-04-07 | Diehl Bgt Defence Gmbh & Co. Kg | Flugkörperbehälter |
DE102013101635A1 (de) | 2013-02-19 | 2014-08-21 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Waffenstation |
US10371479B2 (en) * | 2013-09-11 | 2019-08-06 | Merrill Aviation, Inc. | Stabilized integrated commander's weapon station for combat armored vehicle |
MX2018003811A (es) | 2015-09-29 | 2019-07-18 | Frank Russell | Sistema de torreta de cubierta para camper. |
CA3071196C (en) * | 2017-08-17 | 2023-10-17 | Mac Jee Industria De Defesa Ltda. | Rocket launch model and rocket launch vehicle |
US10309745B2 (en) * | 2017-11-09 | 2019-06-04 | Samuel Messinger | Mobile turret weapon delivery system |
DE202018103226U1 (de) * | 2018-06-08 | 2018-10-11 | Rheinmetall Landsysteme Gmbh | Zusatzsystemanordnung für ein Fahrzeug |
ES2943576T3 (es) | 2018-11-28 | 2023-06-14 | John Cockerill Defense S A | Torreta con techo de protección replegable |
ES2904307T3 (es) * | 2019-02-21 | 2022-04-04 | John Cockerill Defense S A | Vehículo furtivo con sistema de arma integrado de despliegue rápido |
US20220397365A1 (en) * | 2021-06-11 | 2022-12-15 | Alexander RIVERA | Turret apparatus |
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FR494292A (fr) * | 1917-02-14 | 1919-09-04 | Louis Pierre Jacques Chapplain | Canon de tranchée à éclipse automatique |
GB118669A (en) * | 1917-09-04 | 1918-09-04 | Edouard Nieuwenhuyse | Improvements in Gun Mountings. |
DE932297C (de) * | 1952-03-20 | 1955-08-29 | Fritz Beeck | Panzer-Spaehwagen mit hoehenverstellbarer gepanzerter Kanzel |
FR2149637A6 (de) * | 1963-11-28 | 1973-03-30 | Aerospatiale | |
DE1259737B (de) * | 1964-11-06 | 1968-01-25 | Boelkow Gmbh | Abschuss- und Ladevorrichtung fuer rueckstossgetriebene Flugkoerper, die aus richtbaren Wechselmagazinen einzeln nacheinander oder gleichzeitig gestartet werden koennen |
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 (fr) * | 1977-02-11 | 1978-09-08 | Creusot Loire | Installation de lancement de missiles |
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 (de) * | 1984-11-02 | 1986-05-07 | Rheinmetall GmbH, 4000 Düsseldorf | Hochschwenkbare scheitellafettierung fuer das waffenrohr eines kampfpanzers |
DE3603623A1 (de) * | 1986-02-06 | 1987-08-13 | Salgad Int Ltd | Hoehenricht-vorrichtung fuer das abschussrohr eines granatwerfers |
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 |
DE4304761A1 (de) * | 1993-02-17 | 1994-08-18 | Mak System Gmbh | Waffenlafette für Panzerfahrzeuge |
DE4401587A1 (de) * | 1994-01-20 | 1995-07-27 | Wegmann & Co Gmbh | Kampffahrzeug sowie Transportsystem zu seiner Verladung in Transportflugzeuge |
US6584881B1 (en) * | 2001-03-26 | 2003-07-01 | United Defense Lp | Multi-purpose missile launcher system for a military land vehicle |
US7111544B2 (en) * | 2001-08-30 | 2006-09-26 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Artillery gun with a heavy weapon arranged on a support vehicle |
DE20214679U1 (de) * | 2002-09-23 | 2004-02-19 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Einrichtung zur Anpassung eines mehrere Artillerieraketen enthaltenden Containers an eine Abschußvorrichtung für Artillerieraketen |
US6907812B1 (en) * | 2003-01-21 | 2005-06-21 | United Defense Lp | Pop-up weapon system |
US7669513B2 (en) * | 2003-10-09 | 2010-03-02 | Elbit Systems Ltd. | Multiple weapon system for armored vehicle |
ITMI20060668A1 (it) * | 2006-04-05 | 2007-10-06 | Oto Melara Spa | Dispositivo ausiliario di puntamento |
US8146479B2 (en) * | 2009-09-10 | 2012-04-03 | Nexter Systems | Retractable light turret |
-
2008
- 2008-09-24 FR FR0805234A patent/FR2936305B1/fr not_active Expired - Fee Related
-
2009
- 2009-09-07 AT AT09290676T patent/ATE514046T1/de active
- 2009-09-07 PL PL09290676T patent/PL2169341T3/pl unknown
- 2009-09-07 EP EP09290676A patent/EP2169341B1/de active Active
- 2009-09-23 US US12/585,726 patent/US8393258B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
ATE514046T1 (de) | 2011-07-15 |
US20100071540A1 (en) | 2010-03-25 |
FR2936305B1 (fr) | 2010-10-22 |
US8393258B2 (en) | 2013-03-12 |
FR2936305A1 (fr) | 2010-03-26 |
EP2169341A1 (de) | 2010-03-31 |
PL2169341T3 (pl) | 2011-11-30 |
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