EP3123097B1 - Optoelektronischer geschützturm - Google Patents

Optoelektronischer geschützturm Download PDF

Info

Publication number
EP3123097B1
EP3123097B1 EP15712661.6A EP15712661A EP3123097B1 EP 3123097 B1 EP3123097 B1 EP 3123097B1 EP 15712661 A EP15712661 A EP 15712661A EP 3123097 B1 EP3123097 B1 EP 3123097B1
Authority
EP
European Patent Office
Prior art keywords
opto
electronic
rws
optronic
weapon
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
EP15712661.6A
Other languages
English (en)
French (fr)
Other versions
EP3123097A1 (de
Inventor
Bernard Boehm
Jean-Paul SICRE
Patrick Curlier
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.)
Safran Electronics and Defense SAS
Original Assignee
Safran Electronics and Defense SAS
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=51726587&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP3123097(B1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Safran Electronics and Defense SAS filed Critical Safran Electronics and Defense SAS
Publication of EP3123097A1 publication Critical patent/EP3123097A1/de
Application granted granted Critical
Publication of EP3123097B1 publication Critical patent/EP3123097B1/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
    • F41A23/24—Turret gun mountings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/22—Aiming or laying means for vehicle-borne armament, e.g. on aircraft

Definitions

  • the invention relates to an armed optronic cupola having a weapon mounted for pivoting about a bearing axis and a sight mounted for pivoting about the same bearing axis independently of the pivoting of the weapon.
  • An armed cupola fitted for example with a military ship or an armed land vehicle, is intended to protect the ship or the land vehicle during the day and at night against various external aggressions by means of projectile fire (missiles, weapons bullets, etc.). fire, etc.).
  • Such an optronic cupola is known from the document US2012 / 0024143A1 .
  • Such an armed optronic cupola generally comprises a weapon (gun, submachine gun, etc.) and an optronic viewfinder integrating, for example, an infrared camera, a thermal camera, a video camera, a laser range finder, and making it possible to carry out the aiming for the weapon. .
  • Such a cupola also often includes various complementary equipment such as means for detecting and locating projectile shots, a hemispherical vision device, etc.
  • such a cupola is frequently "remote", that is to say it can be controlled remotely.
  • the first problem concerns the orientation of the weapon, which, on some turrets, can not be used in all directions in the field and in the field because of possible physical interactions with other equipment mounted on the vehicle such as a Panoramic observation viewfinder whose field of vision is also also partially obstructed by the cupola.
  • the second problem concerns the turrets on which the weapon and the optronic sight are fixedly mounted in rotation about a bearing axis.
  • the rotation of the optronic viewfinder around the bearing axis to make observations is accompanied by a simultaneous rotation of the weapon, which can be misinterpreted as a threat by people present near the cupola.
  • the invention relates to a means for increasing the area beaten by the weapon of the cupola and the observable area by a neighboring viewfinder.
  • an armed optronic cupola according to claim 1 is proposed. Since the weapon is integral in rotation with the body around the bearing axis, the orientation of the weapon in the field can be realized. in all directions without risk of physical interaction with other equipments of the cupola also integral in rotation of the body around the bearing axis.
  • the optronic viewfinder is mounted to pivot about the same bearing axis independently of the pivoting of the body and thus of the weapon, the orientation of the sight can be achieved without rotating the weapon and is therefore not interpreted as a threat.
  • the armed optronic cupola 1 of the invention intended here to equip a light armored ground vehicle, comprises a base 2 fixed directly to the vehicle, a body 3 constituted by a rotating base 4 and a notched support 5, and an optronic viewfinder. 6 having a viewfinder body 6a and two active parts 6b, 6c.
  • the outer forms of the base 2 and the rotating base 4 of the armed optronic cupola 1 are cylinders of revolution having for axis the same vertical axis called in this description bearing axis Z.
  • the body 3 of the armed optronic cupola 1 is pivotally mounted around the bearing axis Z, and is rotated about the bearing axis Z by first drive means 7 positioned inside the base 2.
  • the first drive means 7 comprise a first electric motor 8 cooperating with a first bearing 9 comprising a fixed portion 11 integral in rotation with the base 2 and a rotating portion 12 integral in rotation with the rotating base 4 of the body 3 .
  • the notched support 5 is fixed on the rotating base 4 of the body 3 of the armed optronic cupola 1.
  • the notched support 5 comprises two arms extending vertically from the rotating base 4 to an upper portion 14 of the armed optronic cupola 1.
  • the light weapon 15 is thus integral in rotation with the body 3 along the bearing axis Z and is so it also mounted pivoting around the bearing axis Z.
  • the light weapon 15 is also mounted to pivot about a first X1 site axis, which allows the light weapon 15 to be directed in elevation to shoot targets at different elevation angles.
  • the orientation of the light weapon 15 in situ is achieved by means of second drive means 16 comprising a second electric motor and mounted on the notched support 5.
  • the viewfinder body 6a of the optronic viewfinder 6 is, for its part, mounted to pivot about the bearing axis Z independently of the pivoting of the body 3 of the armed optronic cupola 1 and therefore of the light weapon 15.
  • the orientation in the field of the optronic viewfinder 6, to achieve the aim for the light weapon 15 or to make observations at different bearing angles, is performed by third drive means 18 positioned, as the first drive means 7, inside the base 2 of the armed optronic cupola 1.
  • the third drive means 18 comprise a third electric motor 19 cooperating with a second bearing 21 comprising a fixed part 22 integral in rotation with the base 2 and a part rotating member 23 rotatably connected to the viewfinder body 6a of the optronic viewfinder 6.
  • the first bearing 9 and the second bearing 21 are thus mounted coaxially around the bearing axis Z.
  • the first motor 8 and the third electric motor 19 operate independently of each other, which allows to orient the weapon in traverse light 15 and the optronics viewfinder 6 independently of one another. Note, however, that the optronic viewfinder 6 can be used to point the weapon. In this phase, the optronic viewfinder 6 sends deposit position instructions which are copied by servocontrol copying to the position of the weapon, each of the two devices being provided with angular position sensors in precision bearing sufficient for this purpose.
  • the simbleautage is achieved by adjusting the angular offset between the indications of the sensors of the weapon and the viewfinder when they aim in the same direction (this is a conventional procedure of simbleautage of the viewfinder with the weapon made in the turrets where the weapon is slaved in position on the viewfinder).
  • the active parts 6b, 6c of the optronic viewfinder 6 are also mounted to pivot around a second axis of site X2, which allows to orient the optronic viewfinder 6 in site to achieve the aim for the light weapon 15 and to perform observations at different angles of elevation.
  • the orientation of the active parts 6a, 6b of the optronic viewfinder 6 in situ is achieved by means of fourth drive means 25 (shown schematically in the figure) comprising a fourth electric motor and located inside the viewfinder body 6a of the optronic viewfinder 6.
  • the light weapon 15 is situated above the optronic viewfinder 6, and that the indented support 5 on which the light weapon 15 is mounted releases a major peripheral zone around the optronic viewfinder 6.
  • the optronic viewfinder 6 can be oriented over a large extent of bearing angle without its field of vision being masked by obstacles located on the armed optronic cupola 1, said obstacles being here constituted in particular by the vertical arms of the notched support 5. This minimizes an angular zone in which the field of view of the optronic viewfinder 6 is masked.
  • the armed optronic cupola 1 of the invention has a very good quality of simbleautage.
  • the optronic viewfinder 6 and the light weapon 15 are very close to each other on the cupola, possible parallax problems are minimized.
  • the armed optronic cupola 1 further comprises means 31 for detecting a projectile firing and a hemispherical vision device 32 both located on the upper part 14 of the body 3 of the armed optronic cupola 1 and mounted on the indented support 5.
  • the detection means 31 comprise a semi-spherical sensing head 33 equipped with a plurality of acoustic sensors 34 distributed over the entire surface of the detection head 33, as well as processing means 35 located in the detection head. 33 (shown schematically in the figure).
  • the processing means 35 are adapted to acquire acoustic measurements made by the acoustic sensors 34 and to analyze these acoustic measurements.
  • the processing means 35 deduce from these acoustic measurements that a shot has been fired.
  • the processing means 35 are also adapted to locate the origin of the projectile, by analyzing the differences between the sound intensities associated with the acoustic measurements and perceived by the various acoustic sensors 34.
  • the hemispherical vision device 32 comprises in particular a camera 38 provided with a "fisheye” type of lens (or “fish eye”) allowing the camera 38 to provide panoramic images of 220 °.
  • the position of the hemispherical vision device, located on the upper part 14 of the body 3 of the armed optronic cupola 1 provides a completely unobstructed view of the surroundings and the top of the vehicle.
  • the armed optronic cupola 1 further comprises a two-part 41 grenade launcher device 41a, 41b adapted to launch smoke grenades.
  • the grenade launcher device 41 is mounted on the rotating base 4 of the body 3 of the armed optronic cupola 1 and is rotationally integral with the body 3. The orientation of the grenade launcher 41 in the bearing is thus achieved by the first drive means 7, as well as the orientation in the field of the light weapon 15.
  • the armed optronic cupola 1 finally comprises a centralized computer 42 (shown schematically in the figure) located in the base 2 of the armed optronic cupola 1.
  • the centralized computer 42 is here connected to a plurality of equipment of the cupola to control and / or to acquire data from these equipment.
  • the centralized computer 42 is in this case connected to the light weapon 15 and the grenade launcher device 41 to control their actuation.
  • the centralized computer 42 is further connected to the first drive means 7 for controlling the bearing orientation of the body 3 of the armed optronic cupola 1 and thus of the light weapon 15, the grenade launcher device. 41, detection means 31 and the atmospheric vision device 32.
  • the centralized computer 42 is also connected to the second drive means 16 for controlling the orientation of the light weapon 15 in its location, to the third drive means 18 and the fourth drive means 25 for respectively controlling the orientation of the optronic viewfinder 6.
  • the centralized computer 42 is finally connected to the processing means 35 of the detection means 31, to the hemispherical vision device 32 and to the optronic viewfinder 6 to acquire data (images, acoustic measurements, location of the origin of a projectile, etc.) from these devices.
  • the centralized computer 42 comprises means of communication symbolized at 43 (these communication means are for example a connection by electric cables or but could be a wireless link) which make it possible to remote control the armed optronic cupola 1.
  • these communication means are for example a connection by electric cables or but could be a wireless link
  • teleoperating one means that the control means (pointing stick, display screen, firing button ...) are deported inside the vehicle.
  • a centralized computer 42 located in the heart of the armed optronic cupola 1 makes it possible to facilitate the integration of the armed optronic cupola 1 in the vehicle, to reduce the number and the length of the cables connected to the different equipment of the armed optronic cupola. 1, decrease the response time associated with the control of these equipment, improve the monitoring functions of these equipment, etc.
  • the first drive means 7 and the third drive means 18 may be driven by the centralized computer 42 to implement a coordinated mode in which a coordinated rotation drive of the body 3 and the optronic viewfinder 6 around the Z bearing axis is controlled. Coordinated mode is used to reduce or totally eliminate the angular area in which the field of view of the optronic viewfinder 6 is masked.
  • the centralized computer 42 controls the first drive means 7 and the third drive means 18 by coordinating the first drive means 7 and the third drive means. drive means 18 so as to ensure that the angular position of the body 3 and the optronic viewfinder 6 remain such that the field of view of the optronic viewfinder 6 is never hidden by the vertical arms of the indented support 5.
  • the optronic viewfinder 6 can therefore be oriented over a 360 ° angle of view angle without its field of vision being masked.
  • the rotational drive of the optronic viewfinder 6 is accompanied by a coordinated rotation drive of the body 3 when the angular position in the bearing of the optronic viewfinder 6 is such that its field of vision is about to be masked by the arms 5.
  • means for estimating the rotary drive speed according to the bearing angle of the optronic viewfinder 6 and the body 3, as well as means for estimating the angular position in the bearing of the 6 optronic viewfinder and 3 body are used to implement the coordinated mode.
  • the centralized computer 42 controls the third drive means 18 to interrupt the rotation drive of the optronic viewfinder 6.
  • the centralized computer 42 is configured to deduce respective bearing angular positions of the optronic viewfinder 6 and the body 3 that the field of view of the optronic viewfinder 6 will be masked by one of the arms.
  • the centralized computer 42 controls the third drive means 18 to drive the optronic viewfinder 6 in a direction opposite to the direction of rotation controlled, so as to reposition the optronic viewfinder 6 in an angular position where its field of vision n is not hidden.
  • reference data of the angular position of the body 3 and the optronic viewfinder 6 and the rotational speed of the body 3 and the optronic viewfinder 6 are stored in a memory module associated with the centralized computer 42.
  • the centralized computer 42 uses these reference data to implement the coordinated mode, for example by stopping the rotational drive of the optronic viewfinder when its speed exceeds a predefined threshold included in the reference data or when its angular position exceeds a predefined position included in the data reference.
  • the base of the armed optronic cupola is fixed directly on the light armored ground vehicle, the armed optronic cupola can of course be mounted on a turret equipping such a vehicle.
  • turret includes any type of carriage carrying any weapon, which may or may not be mounted on a turret.
  • the cupola armed optronics equip a light armored land vehicle, it can of course be mounted on another type of support: military ship, aircraft or helicopter fighter, fixed military installation (antiaircraft turret), etc.
  • bearing axis is here a vertical axis, it may be any axis of orientation forming a non-zero angle with a vertical axis.
  • the body 3 can be fixed or driven in the same direction as the optronic viewfinder 6 (to avoid a masking of the field of view of the optronic viewfinder 6 by one of the arms) or in an opposite direction (for increase the speed of passage of the arm in front of the optronic viewfinder and reduce the duration of masking).

Claims (12)

  1. Optoelektronischer Geschützturm, umfassend ein Gehäuse (3), das um eine Achse (Z) zur Seitenrichtungsverstellung drehbar ist, eine Waffe (15), die drehfest mit dem Gehäuse (3) zur Drehung um die Achse (Z) zur Seitenrichtungsverstellung verbunden und gelagert ist, um sich um eine erste Achse (X1) zur Zielhöhenverstellung zu drehen, und einen optoelektronischen Sucher (6), der unabhängig von der Drehung des Gehäuses (3) um die Achse zur Seitenrichtungsverstellung drehbar um die dieselbe Achse (Z) zur Seitenrichtungsverstellung gelagert ist, dadurch gekennzeichnet, dass sich die Waffe (15) auf einem oberen Teil (14) des Gehäuses (3) des Turms über dem optoelektronischen Sucher (6) befindet und die Waffe auf einem ausgeschnittenen Träger (5) gelagert ist, der eine überwiegende Umfangszone um den optoelektronischen Sucher herum freilegt.
  2. Optoelektronischer Geschützturm nach dem vorhergehenden Anspruch, umfassend Antriebsmittel, die ausgebildet sind, um einen koordinierten Antrieb des Gehäuses (3) und des optoelektronischen Suchers (6) in Drehung um die Achse (Z) zur Seitenrichtungsverstellung zu gestatten, um zu verhindern, dass ein Sichtfeld des optoelektronischen Suchers von einem sich an dem Gehäuse (3) befindlichen Hindernis verdeckt wird.
  3. Optoelektronischer Geschützturm nach Anspruch 2, bei dem eine Winkelposition in Seitenrichtung des optoelektronischen Suchers (6) und/oder des Gehäuses (3) verwendet wird, um den koordinierten Drehantrieb umzusetzen.
  4. Optoelektronischer Geschützturm nach Anspruch 2, bei dem eine Drehgeschwindigkeit in Seitenrichtung des optoelektronischen Sensors (6) und/oder des Gehäuses (3) verwendet wird, um den koordinierten Drehantrieb umzusetzen.
  5. Optoelektronischer Geschützturm nach Anspruch 2, bei dem die in einem Speichermodul gespeicherten Winkelpositions- und/oder Drehgeschwindigkeitsreferenzdaten verwendet werden, um den koordinierten Drehantrieb umzusetzen.
  6. Optoelektronischer Geschützturm nach einem der vorhergehenden Ansprüche, bei dem der optoelektronische Sucher drehbar um eine zweite Achse (X2) zur Zielhöhenverstellung gelagert ist.
  7. Optoelektronischer Geschützturm nach einem der vorhergehenden Ansprüche, umfassend Detektionsmittel zum Erfassen eines Projektilschusses (31), wobei sich die genannten Detektionsmittel auf dem oberen Teil des Gehäuses des Turms befinden.
  8. Optoelektronischer Geschützturm nach Anspruch 7, bei dem die Detektionsmittel ferner dazu geeignet sind, einen Ursprung des Projektils zu lokalisieren.
  9. Optoelektronischer Geschützturm nach einem der Ansprüche 7 oder 8, bei dem die Detektionsmittel einen akustischen Sensor (34) umfassen.
  10. Optoelektronischer Geschützturm nach einem der vorhergehenden Ansprüche, umfassend eine halbkugelförmige Sichtvorrichtung (32), die sich auf dem oberen Teil des Gehäuses des Turms befindet.
  11. Optoelektronischer Geschützturm nach einem der vorhergehenden Ansprüche, umfassend einen zentralisierten Rechner (42), der an eine Vielzahl von Geräten des Turms angeschlossen ist, um sie zu steuern und/oder Daten, die aus diesen Geräten stammen, zu erfassen, wobei die Vielzahl von Geräten die Waffe und/oder den optoelektronischen Sucher und/oder die Detektionsmittel und/oder die halbkugelförmige Sichtvorrichtung und/oder die Drehantriebsmittel zum Drehantrieb dieser Geräte umfasst.
  12. Optoelektronischer Geschützturm nach Anspruch 11, bei dem der zentralisierte Rechner (42) fernsteuerbar ist.
EP15712661.6A 2014-03-28 2015-03-30 Optoelektronischer geschützturm Active EP3123097B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1452728A FR3019279B1 (fr) 2014-03-28 2014-03-28 Tourelleau optronique arme
PCT/EP2015/056924 WO2015144937A1 (fr) 2014-03-28 2015-03-30 Tourelleau optronique arme

Publications (2)

Publication Number Publication Date
EP3123097A1 EP3123097A1 (de) 2017-02-01
EP3123097B1 true EP3123097B1 (de) 2018-05-09

Family

ID=51726587

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15712661.6A Active EP3123097B1 (de) 2014-03-28 2015-03-30 Optoelektronischer geschützturm

Country Status (7)

Country Link
EP (1) EP3123097B1 (de)
AU (1) AU2015238173B2 (de)
CA (1) CA2943372C (de)
FR (1) FR3019279B1 (de)
NO (1) NO3123097T3 (de)
RU (1) RU2672454C2 (de)
WO (1) WO2015144937A1 (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2743597C1 (ru) * 2020-07-29 2021-02-20 Юрий Иосифович Полевой Способ наведения орудия на цель
RU206350U1 (ru) * 2021-05-27 2021-09-07 Акционерное общество «Аэроэлектромаш» Пушечная установка вертолета с усовершенствованным подшипником поворота в горизонтальной плоскости
RU2759065C1 (ru) * 2021-06-08 2021-11-09 Акционерное общество «Аэроэлектромаш» Пушечная установка вертолета с усовершенствованным креплением снарядных контейнеров

Citations (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2660794A (en) 1942-09-12 1953-12-01 Sperry Corp Computing gun sight
US3309962A (en) 1965-03-01 1967-03-21 Fmc Corp Gun mount and gunsight assembly
US3505465A (en) 1967-04-21 1970-04-07 Us Army Panoramic television viewing system
DE1578269A1 (de) 1965-11-15 1970-12-10 Bofors Ab Fahrbares Luftabwehrgeschuetz mit Eigenantrieb
DE1578279A1 (de) 1968-04-26 1971-12-16 Messerschmitt Boelkow Blohm Richt- und Nachfuehreinrichtung fuer fernlenkbare,rueckstossgetriebene Flugkoerper
US3685159A (en) 1969-01-03 1972-08-22 Bofors Ab Method and system for establishing a correct lead when firing at a moving target
DE2507451A1 (de) 1975-02-21 1976-09-09 Wegmann & Co Lafette fuer eine maschinenwaffe
EP0016490A1 (de) 1979-03-23 1980-10-01 Werkzeugmaschinenfabrik Oerlikon-Bührle AG Verfahren zum indirekten Richten eines Geschützes und Einrichtung zur Durchführung des Verfahrens
DE3125678A1 (de) 1981-06-30 1983-01-13 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Richtgeraet
EP0111192A1 (de) 1982-12-06 1984-06-20 Hollandse Signaalapparaten B.V. Integriertes Waffensteuersystem
DE3229819C2 (de) 1982-08-11 1985-02-14 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Integriertes Navigations- und Feuerleitsystem für Kampfpanzer
US4518990A (en) 1983-07-11 1985-05-21 The United States Of America As Represented By The Secretary Of The Army Observation system for military vehicles
DE3410467A1 (de) 1984-03-22 1985-09-26 Rheinmetall GmbH, 4000 Düsseldorf Mehrrohrige waffenanlage
DE3931883C1 (de) 1989-09-23 1990-12-06 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
FR2720513A1 (fr) 1994-05-27 1995-12-01 Metravib Sa Procédé et système pour localiser une arme à feu à partir d'une détection acoustique.
US5994864A (en) 1995-09-11 1999-11-30 Kabushiki Kaisha Yaskawa Denki Robot controller
DE4396177C2 (de) 1992-11-30 2001-02-01 Mitsubishi Electric Corp Panoramaspiegelobjektiv
WO2002033342A1 (en) 2000-10-17 2002-04-25 Electro Optic Systems Pty Limited Autonomous weapon system
US6396235B1 (en) 2001-01-05 2002-05-28 Engineered Support Systems, Inc. Stabilized common gimbal
DE10059313A1 (de) 2000-11-29 2002-06-13 Bosch Gmbh Robert Anordnung und Verfahren zur Überwachung des Umfelds eines Fahrzeugs
EP0778952B1 (de) 1994-08-30 2002-10-16 Aai Corporation Bestimmung der herkunft eines projektils
WO2003054471A1 (en) 2001-11-19 2003-07-03 Bofors Defence Ab Weapon sight
EP0878686B1 (de) 1997-05-14 2003-08-06 Kollmorgen Corporation Waffensteuerungssystem mit Waffenstabilisierung
DE10333647A1 (de) 2003-07-24 2005-02-10 Krauss-Maffei Wegmann Gmbh & Co. Kg Sichteinrichtung an einem Kampffahrzeug, insbesondere einem Kampfpanzer
DE102004003476A1 (de) 2004-01-22 2005-08-18 Rheinmetall Landsysteme Gmbh Vorrichtung für Aufbau und Halterung einer Waffenstation
EP1793195A2 (de) 2005-12-05 2007-06-06 FN HERSTAL, société anonyme Improved device for remote control of a weapon
WO2007086874A2 (en) 2005-01-31 2007-08-02 David Ehrlich Grober Stabilizing mount for hands-on and remote operation of cameras, sensors, computer intelligent devices and weapons
US20070208459A1 (en) 2006-03-03 2007-09-06 Samsung Techwin Co., Ltd. Sentry robot
EP1467237B1 (de) 2003-04-11 2008-05-07 Carl Zeiss Optronics GmbH Periskop für ein gepanzertes Fahrzeug und gepanzertes Fahrzeug
EP1923657A1 (de) 2006-11-16 2008-05-21 Saab Ab Eine kompakte und vollstabilisierte, mit vier Achsen ausgerüstete, Fernwaffestelle mit unabhängiger Visierlinie
DE4306913B4 (de) 1993-03-05 2008-07-03 Rheinmetall Defence Electronics Gmbh Feuerleiteinrichtung für, insbesondere mobile, Flugabwehrsysteme
DE102007002976A1 (de) 2007-01-19 2008-07-24 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren zur Fernsteuerung eines Waffensystems
US20090086015A1 (en) 2007-07-31 2009-04-02 Kongsberg Defence & Aerospace As Situational awareness observation apparatus
US20090200978A1 (en) 2008-02-08 2009-08-13 Fanuc Ltd Robot controller having component protecting function and robot control method
US20090251530A1 (en) 2008-01-29 2009-10-08 Andrew Cilia Omnidirectional camera for use in police car event recording
US7614333B2 (en) 2007-05-24 2009-11-10 Recon/Optical, Inc. Rounds counter remotely located from gun
US7870816B1 (en) 2006-02-15 2011-01-18 Lockheed Martin Corporation Continuous alignment system for fire control
WO2011033514A1 (en) 2009-09-17 2011-03-24 Israel Military Industries Ltd. Multi-weapons system
EP2306137A1 (de) 2009-10-01 2011-04-06 NEXTER Systems Turm zur Montage von Ausrüstung, insbesondere eine Sekundärwaffe
WO2011061562A1 (es) 2009-11-19 2011-05-26 La Nacion, Ministerio De Defensa, Fuerza Aerea Colombiana Sistema electrónico de disparo teledirigido
US20110181722A1 (en) 2010-01-26 2011-07-28 Gnesda William G Target identification method for a weapon system
US20110288804A1 (en) 2010-05-19 2011-11-24 In Jung Sighting Apparatus for Remote-Control Shooting System and Sight Alignment Method Using the Same
US20120024143A1 (en) 2010-07-27 2012-02-02 Raytheon Company Weapon Station and Associated Method
FR2964818A1 (fr) 2010-09-14 2012-03-16 Thales Sa Systeme optronique a vision supra hemispherique
US20120177219A1 (en) 2008-10-06 2012-07-12 Bbn Technologies Corp. Wearable shooter localization system
US20120191292A1 (en) 2011-01-21 2012-07-26 Control Solutions LLC Customizable control apparatus and method for a vehicle turret
WO2013058856A2 (en) 2011-08-09 2013-04-25 Raytheon Company Weapon posturing system and methods of use
DE102012102325B3 (de) 2012-03-20 2013-07-18 OxiMa Tec GmbH Elektrode zur Bearbeitung eines Werkstückes
US20130192451A1 (en) 2011-06-20 2013-08-01 Steven Gregory Scott Anti-sniper targeting and detection system

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120285275A1 (en) * 2011-05-10 2012-11-15 Kongsberg Defence & Aerospace As Stabilization platform

Patent Citations (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2660794A (en) 1942-09-12 1953-12-01 Sperry Corp Computing gun sight
US3309962A (en) 1965-03-01 1967-03-21 Fmc Corp Gun mount and gunsight assembly
DE1578269A1 (de) 1965-11-15 1970-12-10 Bofors Ab Fahrbares Luftabwehrgeschuetz mit Eigenantrieb
US3505465A (en) 1967-04-21 1970-04-07 Us Army Panoramic television viewing system
DE1578279A1 (de) 1968-04-26 1971-12-16 Messerschmitt Boelkow Blohm Richt- und Nachfuehreinrichtung fuer fernlenkbare,rueckstossgetriebene Flugkoerper
US3685159A (en) 1969-01-03 1972-08-22 Bofors Ab Method and system for establishing a correct lead when firing at a moving target
DE2507451A1 (de) 1975-02-21 1976-09-09 Wegmann & Co Lafette fuer eine maschinenwaffe
EP0016490A1 (de) 1979-03-23 1980-10-01 Werkzeugmaschinenfabrik Oerlikon-Bührle AG Verfahren zum indirekten Richten eines Geschützes und Einrichtung zur Durchführung des Verfahrens
DE3125678A1 (de) 1981-06-30 1983-01-13 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Richtgeraet
DE3229819C2 (de) 1982-08-11 1985-02-14 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Integriertes Navigations- und Feuerleitsystem für Kampfpanzer
EP0111192A1 (de) 1982-12-06 1984-06-20 Hollandse Signaalapparaten B.V. Integriertes Waffensteuersystem
US4518990A (en) 1983-07-11 1985-05-21 The United States Of America As Represented By The Secretary Of The Army Observation system for military vehicles
DE3410467A1 (de) 1984-03-22 1985-09-26 Rheinmetall GmbH, 4000 Düsseldorf Mehrrohrige waffenanlage
DE3931883C1 (de) 1989-09-23 1990-12-06 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
DE4396177C2 (de) 1992-11-30 2001-02-01 Mitsubishi Electric Corp Panoramaspiegelobjektiv
DE4306913B4 (de) 1993-03-05 2008-07-03 Rheinmetall Defence Electronics Gmbh Feuerleiteinrichtung für, insbesondere mobile, Flugabwehrsysteme
FR2720513A1 (fr) 1994-05-27 1995-12-01 Metravib Sa Procédé et système pour localiser une arme à feu à partir d'une détection acoustique.
EP0778952B1 (de) 1994-08-30 2002-10-16 Aai Corporation Bestimmung der herkunft eines projektils
US5994864A (en) 1995-09-11 1999-11-30 Kabushiki Kaisha Yaskawa Denki Robot controller
EP0878686B1 (de) 1997-05-14 2003-08-06 Kollmorgen Corporation Waffensteuerungssystem mit Waffenstabilisierung
WO2002033342A1 (en) 2000-10-17 2002-04-25 Electro Optic Systems Pty Limited Autonomous weapon system
US20040050240A1 (en) 2000-10-17 2004-03-18 Greene Ben A. Autonomous weapon system
DE10059313A1 (de) 2000-11-29 2002-06-13 Bosch Gmbh Robert Anordnung und Verfahren zur Überwachung des Umfelds eines Fahrzeugs
US6396235B1 (en) 2001-01-05 2002-05-28 Engineered Support Systems, Inc. Stabilized common gimbal
WO2003054471A1 (en) 2001-11-19 2003-07-03 Bofors Defence Ab Weapon sight
US20100269680A1 (en) 2001-11-19 2010-10-28 Bae Systems Bofors Ab Weapon Sight
EP1467237B1 (de) 2003-04-11 2008-05-07 Carl Zeiss Optronics GmbH Periskop für ein gepanzertes Fahrzeug und gepanzertes Fahrzeug
DE10333647A1 (de) 2003-07-24 2005-02-10 Krauss-Maffei Wegmann Gmbh & Co. Kg Sichteinrichtung an einem Kampffahrzeug, insbesondere einem Kampfpanzer
DE102004003476A1 (de) 2004-01-22 2005-08-18 Rheinmetall Landsysteme Gmbh Vorrichtung für Aufbau und Halterung einer Waffenstation
WO2007086874A2 (en) 2005-01-31 2007-08-02 David Ehrlich Grober Stabilizing mount for hands-on and remote operation of cameras, sensors, computer intelligent devices and weapons
EP1793195B1 (de) 2005-12-05 2009-09-02 FN HERSTAL, société anonyme Verbesserte Vorrichtung zur Waffensteuerung auf Abstand
EP1793195A2 (de) 2005-12-05 2007-06-06 FN HERSTAL, société anonyme Improved device for remote control of a weapon
US7870816B1 (en) 2006-02-15 2011-01-18 Lockheed Martin Corporation Continuous alignment system for fire control
US20070208459A1 (en) 2006-03-03 2007-09-06 Samsung Techwin Co., Ltd. Sentry robot
EP1923657A1 (de) 2006-11-16 2008-05-21 Saab Ab Eine kompakte und vollstabilisierte, mit vier Achsen ausgerüstete, Fernwaffestelle mit unabhängiger Visierlinie
DE102007002976A1 (de) 2007-01-19 2008-07-24 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren zur Fernsteuerung eines Waffensystems
US7614333B2 (en) 2007-05-24 2009-11-10 Recon/Optical, Inc. Rounds counter remotely located from gun
US20090086015A1 (en) 2007-07-31 2009-04-02 Kongsberg Defence & Aerospace As Situational awareness observation apparatus
US20090251530A1 (en) 2008-01-29 2009-10-08 Andrew Cilia Omnidirectional camera for use in police car event recording
US20090200978A1 (en) 2008-02-08 2009-08-13 Fanuc Ltd Robot controller having component protecting function and robot control method
US20120177219A1 (en) 2008-10-06 2012-07-12 Bbn Technologies Corp. Wearable shooter localization system
WO2011033514A1 (en) 2009-09-17 2011-03-24 Israel Military Industries Ltd. Multi-weapons system
EP2306137A1 (de) 2009-10-01 2011-04-06 NEXTER Systems Turm zur Montage von Ausrüstung, insbesondere eine Sekundärwaffe
WO2011061562A1 (es) 2009-11-19 2011-05-26 La Nacion, Ministerio De Defensa, Fuerza Aerea Colombiana Sistema electrónico de disparo teledirigido
US20110181722A1 (en) 2010-01-26 2011-07-28 Gnesda William G Target identification method for a weapon system
US20110288804A1 (en) 2010-05-19 2011-11-24 In Jung Sighting Apparatus for Remote-Control Shooting System and Sight Alignment Method Using the Same
US20120024143A1 (en) 2010-07-27 2012-02-02 Raytheon Company Weapon Station and Associated Method
FR2964818A1 (fr) 2010-09-14 2012-03-16 Thales Sa Systeme optronique a vision supra hemispherique
US20120191292A1 (en) 2011-01-21 2012-07-26 Control Solutions LLC Customizable control apparatus and method for a vehicle turret
US20130192451A1 (en) 2011-06-20 2013-08-01 Steven Gregory Scott Anti-sniper targeting and detection system
WO2013058856A2 (en) 2011-08-09 2013-04-25 Raytheon Company Weapon posturing system and methods of use
DE102012102325B3 (de) 2012-03-20 2013-07-18 OxiMa Tec GmbH Elektrode zur Bearbeitung eines Werkstückes

Non-Patent Citations (6)

* Cited by examiner, † Cited by third party
Title
"Modélisation et analyse des systèmes asservis", TECHNIQUES DE L'INGÉNIEUR, March 2003 (2003-03-01), XP055558523
FACHBUCH: "Elektrische Antriebstechnik", J. WEI- DAUER, ISBN: 978-3-89578-431-6
PAOLO VALPOLINI: "Acoustic gunshot Détection systems", ARMADA INTERNATIONAL, April 2013 (2013-04-01), pages 38 - 49, XP055558501
PAOLO VALPOLINI: "Light remotely controlled weapon stations", ARMADA INTERNATIONAL, 1 February 2013 (2013-02-01), pages 38 - 45, XP055558490
VALPOLINI P: "LIGHT REMOTELY CONTROLLED WEAPON STATIONS", ARMADA INTERNA- TIONAL, 1 February 2013 (2013-02-01), ZÜRICH, CH, pages 38 - 45, XP001580034, ISSN: 0252-9793
YANN TORREBEN: "Les nouveautés du renseignement", EUROSATORY 2012, no. 316, September 2012 (2012-09-01), XP055558517

Also Published As

Publication number Publication date
AU2015238173B2 (en) 2018-12-13
CA2943372A1 (fr) 2015-10-01
CA2943372C (fr) 2018-10-02
EP3123097A1 (de) 2017-02-01
RU2016142400A (ru) 2018-04-28
NO3123097T3 (de) 2018-10-06
WO2015144937A1 (fr) 2015-10-01
RU2672454C2 (ru) 2018-11-14
RU2016142400A3 (de) 2018-04-28
AU2015238173A1 (en) 2016-10-20
FR3019279A1 (fr) 2015-10-02
FR3019279B1 (fr) 2018-06-22

Similar Documents

Publication Publication Date Title
US9121670B2 (en) Operational control logic for harmonized turret with gimbaled sub-systems
EP3123100B1 (de) Optoelektronischer sucher mit modularer abschirmung
KR101569735B1 (ko) 멀티 무기시스템
EP3123097B1 (de) Optoelektronischer geschützturm
EP2852810A1 (de) Ferngesteuertes zielverarbeitungssystem
FR2761463A1 (fr) Dispositif de conduite de tir pour systeme de defense antiaerienne, notamment mobile
EP1448947B1 (de) Beobachtungs- und kampfsystem
EP2932183B1 (de) Verfahren zur erfassung der koordinaten einer geschossabfeuerungsstelle und feuerleitanlage unter verwendung solch eines verfahrens
EP2672217A1 (de) Motorisierte Drehscheibe für Revolverkopf-Zusatzelemente
EP3839411B1 (de) Intelligentes system für die kontrolle der funktionen in einem drehkranz eines kampffahrzeugs
EP3155358B1 (de) System zum lenken von raketen für fahrzeuge und bewegliche ziele
FR2780774A1 (fr) Dispositif d'autoprotection passive pour engin mobile tel qu'un helicoptere
EP1866597B1 (de) System zur zielbestimmung und/oder -beleuchtung und für die luftaufklärung
EP2929284B1 (de) Optronische vorrichtung
FR2788845A1 (fr) Conduite de tir pour projectiles non guides
EP3712551B1 (de) Verfahren zur zielerfassung und ausrichtung für eine plattform, gondel und vorrichtung zur umsetzung dieses verfahrens
FR2929700A1 (fr) Dispositif decentralise d'autodefense comprenant un pointeur portable et mobile apte a assurer en urgence la defense rapprochee d'un navire ou d'une plate-forme en mer contre une menace de surface.
WO2021048474A1 (fr) Système de défense autonome et intelligent
WO2020144418A1 (fr) Titre de l'invention : fusil permettant une simulation précise d'une séquence de tir avec calcul du point d'impact du ou des projectiles
FR2914054A1 (fr) Dispositif de protection rapprochee
FR2737776A1 (fr) Arme comprenant un dispositif de lancement et un projectile a propulser

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

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

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20160921

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20171121

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

RIN1 Information on inventor provided before grant (corrected)

Inventor name: BOEHM, BERNARD

Inventor name: SICRE, JEAN-PAUL

Inventor name: CURLIER, PATRICK

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM 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

Ref country code: AT

Ref legal event code: REF

Ref document number: 997970

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180515

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602015010929

Country of ref document: DE

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: NO

Ref legal event code: T2

Effective date: 20180509

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180509

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

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

Ref country code: ES

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: 20180509

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: 20180809

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: 20180509

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: 20180509

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

Ref country code: HR

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: 20180509

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: 20180509

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: 20180509

Ref country code: RS

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: 20180509

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: 20180810

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 997970

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180509

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

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: 20180509

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: 20180509

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: 20180509

Ref country code: PL

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: 20180509

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: 20180509

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: 20180509

Ref country code: DK

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: 20180509

REG Reference to a national code

Ref country code: DE

Ref legal event code: R026

Ref document number: 602015010929

Country of ref document: DE

PLBI Opposition filed

Free format text: ORIGINAL CODE: 0009260

PLBI Opposition filed

Free format text: ORIGINAL CODE: 0009260

PLAX Notice of opposition and request to file observation + time limit sent

Free format text: ORIGINAL CODE: EPIDOSNOBS2

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

Ref country code: SM

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: 20180509

26 Opposition filed

Opponent name: KRAUSS-MAFFEI WEGMANN GMBH & CO. KG

Effective date: 20190207

26 Opposition filed

Opponent name: NEXTER SYSTEMS

Effective date: 20190207

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

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: 20180509

PLBB Reply of patent proprietor to notice(s) of opposition received

Free format text: ORIGINAL CODE: EPIDOSNOBS3

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180509

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: LU

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

Effective date: 20190330

Ref country code: AL

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: 20180509

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

Ref country code: IE

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

Effective date: 20190330

Ref country code: LI

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

Effective date: 20190331

Ref country code: CH

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

Effective date: 20190331

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

Ref country code: TR

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: 20180509

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

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: 20180910

Ref country code: MT

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: 20180509

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

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: 20180509

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: 20180909

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; INVALID AB INITIO

Effective date: 20150330

PLCK Communication despatched that opposition was rejected

Free format text: ORIGINAL CODE: EPIDOSNREJ1

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

Ref country code: MK

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: 20180509

PLAB Opposition data, opponent's data or that of the opponent's representative modified

Free format text: ORIGINAL CODE: 0009299OPPO

APBM Appeal reference recorded

Free format text: ORIGINAL CODE: EPIDOSNREFNO

APBP Date of receipt of notice of appeal recorded

Free format text: ORIGINAL CODE: EPIDOSNNOA2O

APAH Appeal reference modified

Free format text: ORIGINAL CODE: EPIDOSCREFNO

R26 Opposition filed (corrected)

Opponent name: NEXTER SYSTEMS

Effective date: 20190207

APBQ Date of receipt of statement of grounds of appeal recorded

Free format text: ORIGINAL CODE: EPIDOSNNOA3O

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

Ref country code: NO

Payment date: 20230223

Year of fee payment: 9

Ref country code: FR

Payment date: 20230222

Year of fee payment: 9

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

Ref country code: SE

Payment date: 20230222

Year of fee payment: 9

Ref country code: IT

Payment date: 20230221

Year of fee payment: 9

Ref country code: GB

Payment date: 20230221

Year of fee payment: 9

Ref country code: DE

Payment date: 20230221

Year of fee payment: 9

Ref country code: BE

Payment date: 20230221

Year of fee payment: 9