EP1960729B1 - Vorrichtung zur befestigung eines waffensystems an einem fahrzeugrahmen - Google Patents

Vorrichtung zur befestigung eines waffensystems an einem fahrzeugrahmen Download PDF

Info

Publication number
EP1960729B1
EP1960729B1 EP06831109A EP06831109A EP1960729B1 EP 1960729 B1 EP1960729 B1 EP 1960729B1 EP 06831109 A EP06831109 A EP 06831109A EP 06831109 A EP06831109 A EP 06831109A EP 1960729 B1 EP1960729 B1 EP 1960729B1
Authority
EP
European Patent Office
Prior art keywords
frame
weapon system
chassis
sub
fastening device
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP06831109A
Other languages
English (en)
French (fr)
Other versions
EP1960729A1 (de
Inventor
Christophe Jamet
Ludovic Dupont
Franck Pollet
Philippe Grelat
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nexter Systems SA
Original Assignee
Nexter Systems SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nexter Systems SA filed Critical Nexter Systems SA
Priority to PL06831109T priority Critical patent/PL1960729T3/pl
Publication of EP1960729A1 publication Critical patent/EP1960729A1/de
Application granted granted Critical
Publication of EP1960729B1 publication Critical patent/EP1960729B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F41A23/34—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles on wheeled or endless-track vehicles

Definitions

  • the technical field of the invention is that of devices for fixing a weapon system on a vehicle chassis.
  • Self-propelled weapons systems are usually attached to a turret that is attached to an armored chassis.
  • the mechanical characteristics of the turret and the frame are defined so as to ensure the resistance of these different elements to the shooting constraints.
  • Such a solution can not be transposed to the assembly of a large caliber weapon system (such an artillery) and for which the shooting efforts are much higher. In particular, it does not make it possible to sufficiently reduce the stresses transmitted by the subframe to the chassis.
  • connection means between a plate and a vehicle chassis a connecting means which has four points: two pivot links (arranged at the front and rear of the plateau at a central axis) and two simple supports arranged laterally on both sides of median luxury and between the pivots.
  • the object of the invention is to propose a connection device which, with a reduced mass, makes it possible to ensure the connection between a carrier vehicle chassis and a weapon system while minimizing the stresses to which the carrier chassis is subjected during firing.
  • the subject of the invention is a device for attaching a weapon system to a vehicle chassis, a device comprising a false chassis carrying the weapon system and secured to the chassis by a connecting means, characterized in that the linking means comprises at least two attachment points; disposed between the frame and the subframe and distributed on the lateral faces of the frame and false frame on either side of the weapon system, attachment points formed of lugs integral with the frame, each lugs having a rod, parallel to the side faces of the frame and false frame, and on which is mounted a block secured to the subframe, block that can both translate and rotate relative to the rod, so relative to the frame.
  • the legs will be fixed on both sides of the frame on side faces of spars.
  • the blocks may be fixed to the subframe by means of brackets integral side faces of side beams of the subframe.
  • the blocks may be fixed to the brackets by securing means, spring means being interposed between the securing means and the brackets.
  • the stiffness of the spring means will advantageously be different from one point of attachment to the other, the stiffness being defined according to the deformations that the point of attachment must undergo.
  • the axis of the securing means may be remote from the pivot axis of the block.
  • the device may include at least six pairs of attachment points.
  • the device may comprise a positioning pin secured to the frame at a median plane thereof, pivot cooperating with a socket carried by the false frame.
  • the positioning pin will preferably be disposed near the implantation of the weapon system on the subframe.
  • the attachment points will advantageously be closer to each other in the vicinity of the implantation of the weapon system on the subframe.
  • a vehicle 1 carries a weapon system 2 which is here an artillery system comprising a large caliber gun (caliber greater than 90 mm).
  • the vehicle 1 is a truck comprising a cabin 3 carried by a chassis 4. It comprises a ground connection comprising here (by way of non-limiting example) two axles 5 with wheels.
  • the weapon system 2 comprises a tube 6 sliding in a sled 7, which is itself pivotally mounted on a carriage 8 by pins 9.
  • the carriage is carried by a plate 12 or subframe.
  • the tube 6 carries at its front end a muzzle brake 10.
  • the weapon or artillery system 2 is shown here in an extremely simplified manner. It comprises of course and in a usual manner one or more hydraulic firing brakes (not shown) interposed between the recoil mass (tube 6 and brake 10) and the sled 7 and at least one recuperator (not shown) ensuring the back in battery after firing.
  • a rear stabilizer 11 is articulated (articulation 11a) on the plate 12 (or on the carriage 8) behind the axis 13 of the rear axle.
  • This stabilizer comprises at least one spade 14 integral with a telescopic arm.
  • the stabilizer 11 ensures before firing a ground anchor of the rear of the vehicle 1, the ground anchor 16 is defined by the position of the spade. One or two arms and one or two spades may be provided. The stabilizer 11 is shown in the figure in the deployed position, the spade 14 anchored in the ground.
  • the telescopic arm 15 can be shortened and the complete stabilizer can then tilt around the hinge 11a and rise.
  • the false frame 12 is secured to the frame 4 of the vehicle by a connecting means which comprises a plurality of attachment points 17a, 17b, 17c, — 17h arranged between the frame 4 and the false frame 12 and distributed on the lateral faces of the chassis and subframes, on both sides of the artillery 2.
  • the figure 1 is schematic and shows the false frame 12 disposed at a distance from the frame. 4. In fact these two elements are in contact with each other. It can provide a damping means (such as rubber sheets) interposed between the subframe and the frame.
  • a damping means such as rubber sheets
  • the latter comprises a tab 18 which is fixed to the frame 4 by bolts (not shown) fixed through holes 19.
  • the tab comprises two lateral flanges 31a and 31b carrying bores 21 and between which is disposed a cylindrical rod 20 axis 27.
  • the rod is stopped in translation relative to the flanges 31a, 31b by conventional means not shown (for example transverse pins or nuts).
  • the rod 20 receives a block 22 which is secured to the false frame 12 via a bracket 23.
  • the axis of the rod 20 is parallel to the lateral faces of the chassis and subframe, thus also parallel to the median planes 32 and 33 of the chassis and the subframe (see Figures 4a and 4b ).
  • the bracket 23 comprises a sheet metal plate 30a which is welded to a side face of the subframe 12 and on which is welded a profile 30b reinforced by a rib 30c.
  • the block 22 is fixed to the bracket 23 by fastening means which are here screws 24.
  • fastening means which are here screws 24.
  • One or more spring washers 25 are interposed between the head of the screws 24 and the profile 30b.
  • the axis 28 of the screws is thus disposed at a distance D from the axis 27 of pivoting of the block (see figure 3 ). As far as possible, we will try to minimize this distance D in order to limit the stresses at the level of the connection between the bracket 23 and the subframe 12.
  • washers 25 will be different from one attachment to another. As will be described later, the skilled person will calculate the mechanical stresses on each fastener 17 when firing and it will define the desired mechanical stiffness for each attachment point to minimize mechanical stress. If necessary, depending on the desired stiffness, the washers may be replaced by simple cylindrical spacers.
  • the block 22 can both translate (T directions) and pivot (R arrow) relative to the geometric axis 27 of the rod 20.
  • the subframe 12 is subjected to significant stresses that result in deformations of its structure.
  • the warping (or twisting) of the subframe lead to a pivoting of the side edges of the subframe relative to the chassis. These warps are absorbed by the pivoting capacity R of each block 22 relative to its rod 20, so relative to the frame.
  • the subframe 12 can therefore pivot relative to the chassis 4 at each attachment point 17.
  • the invention thus provides each attachment point 17 of the subframe 12 with a translation and pivoting capacity relative to the chassis 4.
  • the invention While ensuring a safe and light connection between chassis and subframe, the invention thus allows to absorb the deformations caused by the shot and thus to limit the stresses on the chassis 4 of the vehicle 1. This is particularly important when the chassis has a rigid structure that does not tolerate such deformations.
  • FIGs 4a and 4b respectively show in simplified top views, the subframe ( figure 4a ) and the chassis ( figure 4b ).
  • chassis 4 comprises two side rails 29a and 29b on which are fixed the different tabs 18 of the attachment points 17.
  • the spar 29a thus carries eight lugs 18a, 18b ... 18h in the figure and the spar 29b carries, in a symmetrical manner with respect to the vertical median plane 32, eight other lugs also marked 18a, 18b ... 18h.
  • the longitudinal members 29a and 29b are connected to each other by screwed or welded spacers 34, 34a.
  • An intermediate spacer 34a also bears a cylindrical rod or pivot 35 perpendicular to the plane of the frame 4.
  • the subframe 12 shown at figure 4a is also realized in the form of a welded structure comprising lateral beams 36a and 36b connected in particular by at least one spacer 37 as well as a plate 38 on which is fixed a ring 39 intended to receive the carriage 8.
  • the rear portion of the subframe 12 also carries the hinges 11a for the stabilizer or stabilizers (not shown).
  • the lateral beams 36a and 36b each carry eight brackets marked 23a, 23b ... 23h in the figure.
  • the brackets carried on the beam 36b are arranged symmetrically to the brackets of the beam 36a with respect to the median vertical plane 33.
  • the spacer 37 carries a cylindrical sleeve 40 which is intended to receive the rod 35 integral with the chassis 4.
  • the figure 4c shows the assembly of the subframe 12 on the chassis 4.
  • the correct positioning of the false frame is facilitated by the cooperation of the rod 35 with the sleeve 40.
  • the rod 35 and the sleeve 40 are positioned in the vicinity of the place where the shooting forces are applied. by the weapon system with the false frame, that is to say near the crown 39.
  • the bushing / rod connection makes it possible to position the false frame relative to the chassis but also makes it possible to take back part of the firing forces transmitted from the subframe to the chassis, thus relieving the attachment points 17 during firing.
  • each bracket 23 is above a lug 18.
  • Each lug 18 carries a block 22.
  • the assembly is completed by screwing the brackets 23 on the different blocks 22 so as to constitute the different points of fastener 17 of the connecting means.
  • each attachment point will size each attachment point and he will choose the number and distribution of the latter as a function of the characteristics of the weapon system and those of the carrier on which it is desired to install it. Positioning and sizing will be realized by numerical simulation of the firing constraints on the structure.
  • the desired stiffness will be calculated at each attachment point 17 so as to minimize the stresses undergone. This stiffness calculation will make it possible to define the washers or spacers 25 which will be implemented at each attachment point 17.
  • the invention is particularly useful when the intended carrier vehicle is provided with a rigid chassis.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Body Structure For Vehicles (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Air Bags (AREA)

Claims (10)

  1. Vorrichtung zur Befestigung eines Waffensystems (2) an einem Fahrzeugrahmen (4), wobei die Vorrichtung einen Zwischenrahmen (12) umfasst, der das Waffensystem trägt und durch ein Verbindungsmittel fest mit dem Rahmen verbunden ist, wobei die Vorrichtung dadurch gekennzeichnet ist, dass das Verbindungsmittel wenigstens zwei Befestigungspunkte (17) umfasst, die zwischen dem Rahmen (4) und dem Zwischenrahmen (12) angeordnet sind und über die Seitenflächen des Rahmens und Zwischenrahmens beiderseits des Waffensystems (2) verteilt sind, wobei die Befestigungspunkte (17) von Laschen (18) gebildet werden, die fest mit dem Rahmen (4) verbunden sind, wobei die Laschen jeweils eine Stange (20) tragen, die parallel zu den Seitenflächen des Rahmens und Zwischenrahmens verläuft und an der ein Block (22) montiert ist, der fest mit dem Zwischenrahmen (12) verbunden ist, wobei sich der Block in Bezug auf die Stange (20) und somit in Bezug auf den Rahmen (4) gleichzeitig verschieben und drehen kann.
  2. Vorrichtung zur Befestigung eines Waffensystems nach Anspruch 1, wobei die Vorrichtung dadurch gekennzeichnet ist, dass die Laschen (18) beiderseits des Rahmens (4) an Seitenflächen von Längsträgern (29a, 29b) befestigt sind.
  3. Vorrichtung zur Befestigung eines Waffensystems nach einem der Ansprüche 1 oder 2, wobei die Vorrichtung dadurch gekennzeichnet ist, dass die Blöcke (22) am Zwischenrahmen (12) mit Hilfe von Winkeln (23) befestigt sind, die fest mit Seitenflächen von Seitenträgern (36a, 36b) des Zwischenrahmens (12) verbunden sind.
  4. Vorrichtung zur Befestigung eines Waffensystems nach einem der Ansprüche 1 bis 3, wobei die Vorrichtung dadurch gekennzeichnet ist, dass die Blöcke (22) durch Zusammenschlussmittel (24) an den Winkeln (23) befestigt sind, wobei Federmittel (25) zwischen die Zusammenschlussmittel (24) und die Winkel (23) eingefügt sind.
  5. Vorrichtung zur Befestigung eines Waffensystems nach Anspruch 4, wobei die Vorrichtung dadurch gekennzeichnet ist, dass die Steifigkeiten der Federmittel (25) von einem Befestigungspunkt (17) zum anderen verschieden sind, wobei die Steifigkeiten in Abhängigkeit von den Deformationen festgelegt werden, die der Befestigungspunkt erfahren muss.
  6. Vorrichtung zur Befestigung eines Waffensystems nach einem der Ansprüche 4 oder 5, wobei die Vorrichtung dadurch gekennzeichnet ist, dass die Achse der Zusammenschlussmittel (24) sich von der Drehachse des Blocks im Abstand (D) befindet.
  7. Vorrichtung zur Befestigung eines Waffensystems nach einem der Ansprüche 1 bis 6, wobei die Vorrichtung dadurch gekennzeichnet ist, dass sie wenigstens sechs Paare von Befestigungspunkten (17) umfasst.
  8. Vorrichtung zur Befestigung eines Waffensystems nach einem der Ansprüche 1 bis 7, wobei die Vorrichtung dadurch gekennzeichnet ist, dass sie ein Positionierungsdrehgelenk (35) umfasst, das fest mit dem Rahmen (4) im Bereich dessen Mittelebene (32) verbunden ist, wobei das Drehgelenk mit einer Hülse (40) zusammenwirkt, die von dem Zwischenrahmen (12) getragen wird.
  9. Vorrichtung zur Befestigung eines Waffensystems nach Anspruch 8, wobei die Vorrichtung dadurch gekennzeichnet ist, dass das Positionierungsdrehgelenk (35) in der Nähe der Anbringung des Waffensystems an dem Zwischenrahmen (12) angeordnet ist.
  10. Vorrichtung zur Befestigung eines Waffensystems nach einem der Ansprüche 1 bis 9, wobei die Vorrichtung dadurch gekennzeichnet ist, dass die Befestigungspunkte (17) in der Nähe der Anbringung des Waffensystems an dem Zwischenrahmen (12) enger zueinander liegen.
EP06831109A 2005-11-21 2006-11-13 Vorrichtung zur befestigung eines waffensystems an einem fahrzeugrahmen Active EP1960729B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL06831109T PL1960729T3 (pl) 2005-11-21 2006-11-13 Urządzenie do mocowania systemu broni na podwoziu pojazdu

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0511826A FR2893710B1 (fr) 2005-11-21 2005-11-21 Dispositif de fixation d'un systeme d'arme sur un chassis de vehicule
PCT/FR2006/002509 WO2007057550A1 (fr) 2005-11-21 2006-11-13 Dispositif de fixation d'un systeme d'arme sur un chassis de vehicule

Publications (2)

Publication Number Publication Date
EP1960729A1 EP1960729A1 (de) 2008-08-27
EP1960729B1 true EP1960729B1 (de) 2011-02-16

Family

ID=36694190

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06831109A Active EP1960729B1 (de) 2005-11-21 2006-11-13 Vorrichtung zur befestigung eines waffensystems an einem fahrzeugrahmen

Country Status (11)

Country Link
EP (1) EP1960729B1 (de)
JP (1) JP4901875B2 (de)
AT (1) ATE498814T1 (de)
DE (1) DE602006020171D1 (de)
DK (1) DK1960729T3 (de)
ES (1) ES2361438T3 (de)
FR (1) FR2893710B1 (de)
IL (1) IL191606A (de)
PL (1) PL1960729T3 (de)
WO (1) WO2007057550A1 (de)
ZA (1) ZA200804372B (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3044753B1 (fr) 2015-12-08 2019-03-22 Nexter Systems Dispositif de manutention d'obus pour piece d'artillerie
SE541539C2 (sv) * 2017-06-30 2019-10-29 Bae Systems Bofors Ab Infästningsanordning för en pjäsmodul på en bärare samt ett vapensystem

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0365474A (ja) * 1989-08-04 1991-03-20 Ee S:Kk 荷台の防振支持装置
FR2663727B1 (fr) * 1990-06-22 1992-10-02 Lohr Ind Structure composite pour le tir au mortier a partir d'un engin motorise.
DE9208524U1 (de) * 1991-08-08 1992-08-27 Titan Spezialfahrzeugbau GmbH, 7600 Offenburg Kraftfahrzeug mit abnehmbarer Kipp-Ladepritsche
US5390582A (en) * 1993-05-12 1995-02-21 Sanderson; Paul H. Plank-mounted aircraft armanent apparatus
DE10106495C2 (de) * 2001-02-13 2003-08-07 Crossmobil Gmbh Lastfahrzeug
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
JP3862674B2 (ja) * 2003-06-13 2006-12-27 株式会社クボタ 乗用型移植機
JP4133903B2 (ja) * 2004-03-30 2008-08-13 株式会社日本製鋼所 りゅう弾砲の車両搭載装置

Also Published As

Publication number Publication date
JP4901875B2 (ja) 2012-03-21
FR2893710A1 (fr) 2007-05-25
WO2007057550A8 (fr) 2008-07-10
ZA200804372B (en) 2010-04-28
ATE498814T1 (de) 2011-03-15
ES2361438T3 (es) 2011-06-17
FR2893710B1 (fr) 2010-02-12
DE602006020171D1 (de) 2011-03-31
DK1960729T3 (da) 2011-06-06
IL191606A (en) 2011-12-29
JP2009516815A (ja) 2009-04-23
PL1960729T3 (pl) 2011-07-29
EP1960729A1 (de) 2008-08-27
IL191606A0 (en) 2008-12-29
WO2007057550A1 (fr) 2007-05-24

Similar Documents

Publication Publication Date Title
RU2555375C2 (ru) Убирающееся посадочное шасси вертолета
FR2887211A1 (fr) Voie basse guidee pour avant de vehicule automobile
FR2516455A1 (fr) Suspension de vehicule automobile par lame elastique
CA2487047C (fr) Dispositif de liaison souple entre un longeron flexible et une boite d'essieu
EP2598398A1 (de) Verfahren und vorrichtung zur ausrüstung eines flugzeugbugraums in einem avionikraum
FR3019785A1 (fr) Poutre de pare-chocs de vehicule, ensemble pare-chocs et vehicule associes
EP0251850A1 (de) Radaufhängung für Fahrzeug
EP3052886A1 (de) Schnittstelle für eine sichtvorrichtung einer feuerwaffe
EP1960729B1 (de) Vorrichtung zur befestigung eines waffensystems an einem fahrzeugrahmen
EP1081023A1 (de) Vorderes Tragwerk für ein Kraftfahrzeug und Kraftfahrzeug mit solchem Tragwerk
FR2726227A1 (fr) Suspension pour un train de roues arriere independantes de vehicule automobile
EP3578460B1 (de) Fahrwerk eines luftfahrzeugs, das mit routing-mitteln für kabel und leitungen ausgestattet ist
FR3036375A1 (fr) Train d'atterrissage pour un aeronef et presentant un systeme de verrouillage en position de stockage
FR2766916A1 (fr) Tourelle de char
EP2736793A1 (de) Kopfmodul für ein kraftfahrzeug
EP3901019A1 (de) Stabilisierungsanordnung für fahrzeug
FR3051721A1 (fr) Procede d’assemblage d’un systeme de suspension pour vehicule automobile
EP3224139A1 (de) Fahrwerk für ein leichtes luftfahrzeug mit mindestens zwei rädern
EP3814218B1 (de) Fahrwerk für ein flugzeug, das weniger als 5,7 tonnen wiegt
FR3038573A1 (fr) Structure arriere de vehicule pour choc urbain
FR2523677A1 (fr) Suspension elastique a ressort, notamment pour vehicule automobile
FR2895323A3 (fr) Biellette de reprise de couple
FR3086227A1 (fr) Support de projecteur de vehicule automobile.
EP3027442B1 (de) Antriebsstrang für ein kraftfahrzeug
EP3424757B1 (de) Hinterachse eines kraftfahrzeugs, die energieabsorptionsmittel eines seitlichen aufpralls umfasst

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20080620

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

17Q First examination report despatched

Effective date: 20091116

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

DAX Request for extension of the european patent (deleted)
GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REF Corresponds to:

Ref document number: 602006020171

Country of ref document: DE

Date of ref document: 20110331

Kind code of ref document: P

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602006020171

Country of ref document: DE

Effective date: 20110331

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20110216

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2361438

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20110617

LTIE Lt: invalidation of european patent or patent extension

Effective date: 20110216

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110517

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110616

REG Reference to a national code

Ref country code: PL

Ref legal event code: T3

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110516

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

Ref country code: IE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20111117

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602006020171

Country of ref document: DE

Effective date: 20111117

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111113

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110216

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 12

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20231019

Year of fee payment: 18

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20231201

Year of fee payment: 18

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20231027

Year of fee payment: 18

Ref country code: SE

Payment date: 20231020

Year of fee payment: 18

Ref country code: IT

Payment date: 20231019

Year of fee payment: 18

Ref country code: FR

Payment date: 20231020

Year of fee payment: 18

Ref country code: DK

Payment date: 20231019

Year of fee payment: 18

Ref country code: DE

Payment date: 20231019

Year of fee payment: 18

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: PL

Payment date: 20231025

Year of fee payment: 18

Ref country code: BE

Payment date: 20231019

Year of fee payment: 18

REG Reference to a national code

Ref country code: BE

Ref legal event code: HC

Owner name: KNDS FRANCE; FR

Free format text: DETAILS ASSIGNMENT: CHANGE OF OWNER(S), CHANGE OF OWNER(S) NAME; FORMER OWNER NAME: NEXTER SYSTEMS

Effective date: 20240530