EP1407215B1 - Waffenlagerungsrichtsystem - Google Patents

Waffenlagerungsrichtsystem Download PDF

Info

Publication number
EP1407215B1
EP1407215B1 EP02770026A EP02770026A EP1407215B1 EP 1407215 B1 EP1407215 B1 EP 1407215B1 EP 02770026 A EP02770026 A EP 02770026A EP 02770026 A EP02770026 A EP 02770026A EP 1407215 B1 EP1407215 B1 EP 1407215B1
Authority
EP
European Patent Office
Prior art keywords
weapon
axis
around
laying system
integral
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.)
Expired - Lifetime
Application number
EP02770026A
Other languages
English (en)
French (fr)
Other versions
EP1407215A1 (de
Inventor
Emile Urvoy
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.)
Giat Industries SA
Original Assignee
Giat Industries 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 Giat Industries SA filed Critical Giat Industries SA
Publication of EP1407215A1 publication Critical patent/EP1407215A1/de
Application granted granted Critical
Publication of EP1407215B1 publication Critical patent/EP1407215B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/06—Mechanical systems
    • F41A27/22—Traversing gear
    • 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
    • F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/06—Mechanical systems
    • F41A27/08—Bearings, e.g. trunnions; Brakes or blocking arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G5/00—Elevating or traversing control systems for guns
    • F41G5/14—Elevating or traversing control systems for guns for vehicle-borne guns
    • F41G5/24—Elevating or traversing control systems for guns for vehicle-borne guns for guns on tanks

Definitions

  • the technical sector of the present invention is that of the pointing systems of a weapon ensuring its stabilization.
  • a first method consists in measuring the disturbing angular velocity, for example by means of a gyrometric type, and using it to control the speed of rotation of the motorization system placed between the support and the weapon. It is therefore an anticipation control placed in parallel with a servo control of the position of the weapon on an inertial reference whose efficiency is low to attenuate the amplitude of the angular disturbances for medium frequencies. For example, reference may be made to FR-A-2 466 741.
  • Another method is to provide a motor for controlling the torque applied to the load. This principle is used to improve the efficiency of reducing the effects of angular rate disturbances. This method is suitable for disturbances of angular velocities around the axis of rotation in the bearing of the turret. For example, reference can be made to US-4387624.
  • Yet another method is to measure the gyrometric rate of roll and to control an angular speed of the turret proportional to this speed, through a coefficient depending on the site of the weapon.
  • the object of the present invention is to propose a system making it possible to exceed the limits imposed by the orientation of the weapon in the bearing and to increase significantly the possible compensation area of the roll disturbances.
  • the invention therefore relates to a pointing system in the field of a weapon secured to an articulated frame bearing in relation to a support along a large deflection in a bearing around a first axis of rotation (Gl), characterized in that it comprises a means of positioning the weapon integral with the frame or turret to ensure a low lateral movement of the weapon around a second axis of rotation (G2) passing through the center of gravity of the weapon and perpendicular respectively to the longitudinal axis of the weapon and to the orientation axis in site.
  • G2 second axis of rotation
  • the first axis of rotation (G1) is located behind the center of gravity of the weapon.
  • the lateral deflection around the second axis is of the order of 2 °.
  • the positioning means comprises a mask supporting the weapon and secured to the frame and means for controlling the rotation.
  • the weapon is mounted via a hinge relative to the mask, the positioning means ensuring the rotation of the weapon relative to the mask around the second axis (G2).
  • the articulation is of the mechanical or elastic type.
  • the mechanical articulation is constituted by a journal integral with a cradle interposed between the weapon and the mask and bearings secured to the mask.
  • control means is a cylinder whose body is secured to the mask and whose rod is connected to the weapon.
  • control means is a jack whose body is secured to the weapon and whose rod is connected to the mask.
  • the elastic articulation is formed by two integral journals of the cradle and connected to the mask by an elastic means having a low angular stiffness around the axis G2 and a high stiffness around the axis of the site.
  • the secondary articulation means around the axis G2 is obtained by the displacement in opposite directions of two eccentrics.
  • control means consists of two jacks operating in opposite directions whose bodies are fixed on the cradle and the rods respectively on each of the eccentrics, the minimum elasticity of this motorization being achieved by the radial stiffness of crowns. elastomer.
  • a first advantage of the system according to the invention resides in the respect of the needs for quality of absolute orientation to impose on the weapon by the adoption of a second articulation at the center of gravity allowing a lateral angular displacement of the body. weapon relative to the turret.
  • Another advantage lies in the control of the bearing orientation of the weapon without disturbing the order in site.
  • Another advantage lies in the fact that the disturbing torques applied between the mask and the weapon via the second axis of rotation G2 are limited to the driving torque and the torque caused by the sealing system between the mask and the cradle of the vehicle. 'armed.
  • the relative movement mask cradle being limited specific means of sealing (bellows type for example) can be used to minimize parasitic stress.
  • An additional advantage is that maintaining the orientation of the weapon on the target no longer requires the precise rotation of the turret with the associated constraints, the quality of the control and the maximum torque available.
  • Another advantage is to be able to use, for motorizing the additional axis of rotation G2 the principle described in the US patent with the associated advantages on the positioning quality of the weapon.
  • the corresponding motorization can be either electric or hydraulic.
  • Another additional advantage of the invention is that the quality of the stabilization of the turret in the field can be degraded, the residual errors of the turret being taken up by the additional lateral orientation system.
  • a weapon mounted on an armored vehicle conventionally comprises a cradle mounted fixed relative to a mask itself articulated about a journal axis relative to the turret or frame.
  • the weapon therefore has a receding mass that slides longitudinally in the cradle with each shot.
  • This structure offers a possibility of rotation around an axis perpendicular to the axis of the weapon and the axis of rotation in site, because the weapon is disengaged from the drive in roll by the turret and we give our the means of accessing stabilization performance accessible to a system that can benefit from inertial stabilization.
  • the motorization of the main bearing of the turret being limited in acceleration torque, when this saturation is reached, the stabilization can be kept within the limit of the displacement set up at the level of the second articulation allowing angular mobility. secondary side mentioned above.
  • the secondary axis of articulation is placed axially at the center of gravity of the laterally articulated mass to limit the disturbance given by the radial acceleration and to limit the dimensioning of the secondary motorization.
  • the invention consists in providing an additional articulation of the weapon relative to its frame.
  • a first articulation, or main articulation makes it possible to orient the weapon in a conventional manner. This articulation allows to position the weapon without any angular limitation.
  • a second articulation allows to orient a limited range of the weapon in zero-site deposit and more generally laterally.
  • the advantage of such a system according to the invention lies in the fact that the secondary clearance between the weapon and the mask for example is limited to the stabilization errors around the first axis, resulting in a simple realization.
  • the dimensioning of the second motorization being linked only to the inertia of the weapon to steer, a high-performance torque control can be achieved without specific constraints.
  • FIG 1 there is shown schematically in vertical section a weapon 1 mounted on a frame 2 itself mounted on a support 3 by means of a bearing 4 of large diameter.
  • the support 3 is represented for example by the roof of an armored vehicle crawler or wheeled.
  • the frame 2, or turret is the interface between the weapon and the support and it supports the weapon via a pin 5 whose location is visible in the figure.
  • the weapon is mounted in a mask 6a with respect to which it slides with each shot inside a cradle 6b.
  • the weapon is thus connected to this mask by a number of mechanisms, including brakes, known in themselves and that it is not necessary to describe more completely for the understanding of the invention.
  • the weapon is movable in a known manner relative to the journal 5 for example by means of a jack 7 connecting the mask to the frame 2. It is also movable deposit around a main axis G1 relative to the support 3.
  • the weapon 1 is rotatable about an axis G2 with respect to the mask 6a.
  • the axis G2 is shown passing through the center of gravity of the weapon and the axis G1 is located behind the center of gravity. This arrangement is chosen preferentially, but it goes without saying that the axis G1 can occupy any intermediate position.
  • FIG 2 there is shown a top view of the weapon 1 in a section made along its longitudinal axis XX '.
  • the trace 8 of the raceway of the frame 2 or turret relative to the support This turret can be mobile in rotation around the G1 axis at an angle of 360 °.
  • the turret thus drives the weapon 1 to orient it in a zero-site deposit or laterally.
  • a motor 9 drives the turret 2 via a gearbox 10.
  • the weapon 1 is thus mounted on the frame 2 via a mask 6a itself connected to the frame using of two bearings 11a and 11b.
  • the bearings 11a and 11b define a site axis S of the weapon around which the latter is rotated with the aid of a geared motor.
  • the second bearing axis G2 is provided around which the weapon will be actuated in order to orient it very finely.
  • This means can be, for example, a motor or a jack.
  • the body of the jack can be integral with the mask and its rod is connected to the weapon or the cylinder body is secured to the weapon and its rod mask.
  • FIG 3 there is shown a schematic view of the lateral secondary articulation means of the weapon 1 relative to the frame 2 and the bearings 11a and 11b of the mask connection.
  • the figure illustrates the articulation between the cradle 6b and the mask 6a.
  • cradle 6b supporting the weapon 1 is connected to the mask 6a via a hinge 15 to ensure the secondary rotation of said weapon relative to the mask around the second axis G2.
  • the articulation is of the mechanical type and comprises a pin 16 engaged in two bearings 17 and 18.
  • the joint can be of the elastic type.
  • FIG. 4 an exemplary embodiment of an elastic articulation is shown. This is constituted by a metal cylinder 19 in which the cradle is fixed and which is connected by elastomer plates 20 to the mask 6a via an appropriate complementary part 21.
  • the part 21 is made in two separate parts 21a and 21b for mounting questions and which are fixed rigidly to the mask 6a.
  • the elastic plates 20 are defined by their material on the one hand to have a high stiffness and resistance to withstand the axial forces of recoil of the weapon and on the other hand to present a stiffness reduced relative to the angular deflection in the deposit up to about 2 °.
  • the stiffness associated with this degree of freedom corresponds approximately to a maximum effort which must be limited between 10 and 20% of the maximum effort of the associated secondary motorization. It also specifies a radial lateral stiffness, parallel to the journal axis of the mask, sufficient to minimize its effect on the torque dynamics of the secondary side engine.
  • any means of articulation may be provided between the cradle and the mask for allowing a small angular rotation around the axis G2.
  • This means must have a limited torque in the range of travel around this axis, and must be able to transmit to the mask the force of recoil of the weapon and to present a high angular stiffness around the axis of site between the mask and cradle.
  • FIGS. 5 and 6 which are sections along the longitudinal axis XX 'of the weapon illustrate this embodiment.
  • the weapon 1 is mounted on a turret 25 by means of a cradle / mask assembly 26 by means of two bearings 27 and 28 separated by an eccentric 29.
  • the outer bearing 27 is of large size and surrounds the bearing 28.
  • the bearing 28 makes it possible to connect the cradle 26 via the journal 30, the bearing 28 being itself supported by the bearing 27 fixed to the turret 25 by means of a ring 31 of elastomer.
  • This resilient ring works in shear to allow the axis of the bearings 27 and 28 to remain in a plane perpendicular to the axis of the weapon.
  • the radial stiffness of these elastic links relatively greater than the tangential stiffness is used to impose an angular functional stiffness in the chain of relative lateral motorization between the weapon and the turret.
  • the eccentric is in the form of an annular piece whose outer wall constitutes the inner race of the bearing 27 and whose inner wall constitutes the outer cage of the bearing 28.
  • an inertial sensor absolute position consists of a gyroscope that serves as a reference to both the line of sight, the weapon and the mask.
  • the gyro sensor is preferably mounted on the mask and can be replaced by a gyro that measures the angular velocity of the mask, which speed is integrated to materialize the reference gyroscopic position.
  • the absolute position of the cradle is calculated from a linear position measurement made in the vicinity of the actuator for exerting a torque on the weapon.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Telescopes (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Geophysics And Detection Of Objects (AREA)

Claims (12)

  1. System zum Richten einer Waffe (1) in horizontaler Richtung, die mit einem Gestell (2) fest verbunden ist, das in Bezug auf einen Träger (3) entsprechend eines großen Ausschlages in horizontaler Richtung um eine erste Drehachse (G1) in horizontaler Richtung schwenkbar ist, dadurch gekennzeichnet, dass es ein fest mit dem Gestell (2) verbundenes Mittel zur Positionierung (6a, 6b, 14) der Waffe (1) umfasst, um einen geringen seitlichen Ausschlag der Waffe um eine zweite Drehachse (G2) zu gewährleisten, die durch den Schwerpunkt der Waffe und jeweils senkrecht zur Längsachse XX' der Waffe und zur Achse zur vertikalen Ausrichtung verläuft.
  2. Richtsystem nach Anspruch 1, dadurch gekennzeichnet, dass die erste Drehachse (G1) hinter dem Schwerpunkt der Waffe (1) angeordnet ist.
  3. Richtsystem nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass der seitliche Ausschlag der Waffe um die zweite Achse (G2) in der Größenordnung von 2° liegt.
  4. Richtsystem nach Anspruch 3, dadurch gekennzeichnet, dass das Positioniermittel eine Blende (6a) und einen Schlitten (6b) umfasst, welche die Waffe (1) tragen und fest mit dem Gestell (2) verbunden sind, und ein Mittel zur Steuerung (14) der Drehung.
  5. Richtsystem nach Anspruch 4, dadurch gekennzeichnet, dass die Waffe (1) mit Hilfe eines Gelenkes (15) in Bezug auf die Blende (6a) montiert ist, wobei das Positioniermittel (14) die Drehung der Waffe (1) in Bezug auf die Blende (6a) um die zweite Achse (G2) gewährleistet.
  6. Richtsystem nach Anspruch 5, dadurch gekennzeichnet, dass das Gelenk (15) von mechanischer oder elastischer Bauart ist.
  7. Richtsystem nach Anspruch 6, dadurch gekennzeichnet, dass das mechanische Gelenk von einem Drehzapfen (16), der fest mit einem zwischen die Waffe (1) und die Blende (6a) eingefügten Schlitten (6b) verbunden ist, und von den fest mit der Blende (6a) verbundenen Lagern (17, 18) gebildet wird.
  8. Richtsystem nach irgendeinem der Ansprüche 5 bis 7, dadurch gekennzeichnet, dass das Steuermittel (14) ein Zylinder ist, dessen Körper fest mit der Blende (6a) verbunden ist und dessen Stange mit der Waffe (1) verbunden ist.
  9. Richtsystem nach irgendeinem der Ansprüche 5 bis 7, dadurch gekennzeichnet, dass das Steuermittel (14) ein Zylinder ist, dessen Körper fest mit der Waffe (1) verbunden ist und dessen Stange mit der Blende (6a) verbunden ist.
  10. Richtsystem nach Anspruch 6, dadurch gekennzeichnet, dass das elastische Gelenk aus zwei Drehzapfen gebildet wird, die fest mit dem Schlitten (6b) verbunden sind und mittels eines elastischen Mittels, das eine geringe Winkel-Steifigkeit um die Achse G2, aber eine große Steifigkeit um die Achse zur Elevation S aufweist, mit der Blende (6a) verbunden sind.
  11. Richtsystem nach Anspruch 10, dadurch gekennzeichnet, dass das sekundäre Mittel zum Schwenken um die Achse G2 durch die Verlagerung in umgekehrter Richtung zweier Exzenter (29a, 29b) erzielt wird.
  12. Richtsystem nach Anspruch 10 oder 11, dadurch gekennzeichnet, dass das Steuermittel von zwei Zylindern (32, 33) gebildet wird, die in entgegen gesetzter Richtung arbeiten, deren Körper an dem Schlitten (26) und die Stangen jeweils an einem der Exzenter (29a, 29b) befestigt sind, wobei die minimale Elastizität dieses Antriebes durch die seitliche Steifigkeit von elastomeren Kränzen (31) bewerkstelligt wird.
EP02770026A 2001-07-17 2002-07-15 Waffenlagerungsrichtsystem Expired - Lifetime EP1407215B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0109509 2001-07-17
FR0109509A FR2827667B1 (fr) 2001-07-17 2001-07-17 Systeme de pointage en gisement d'une arme
PCT/FR2002/002506 WO2003008894A1 (fr) 2001-07-17 2002-07-15 Systeme de pointage en gisement d'une arme

Publications (2)

Publication Number Publication Date
EP1407215A1 EP1407215A1 (de) 2004-04-14
EP1407215B1 true EP1407215B1 (de) 2006-03-08

Family

ID=8865592

Family Applications (1)

Application Number Title Priority Date Filing Date
EP02770026A Expired - Lifetime EP1407215B1 (de) 2001-07-17 2002-07-15 Waffenlagerungsrichtsystem

Country Status (8)

Country Link
US (1) US6886448B2 (de)
EP (1) EP1407215B1 (de)
AT (1) ATE319975T1 (de)
DE (1) DE60209763T2 (de)
FR (1) FR2827667B1 (de)
IL (1) IL159711A0 (de)
WO (1) WO2003008894A1 (de)
ZA (1) ZA200301999B (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6237462B1 (en) * 1998-05-21 2001-05-29 Tactical Telepresent Technolgies, Inc. Portable telepresent aiming system
FR2824896B1 (fr) * 2001-05-17 2003-08-15 Giat Ind Sa Systeme de pointage d'une arme
FR2827668B1 (fr) * 2001-07-17 2003-10-03 Giat Ind Sa Systeme de pointage en site et en gisement d'une arme
AU2003291223A1 (en) * 2003-01-13 2004-08-10 Denel (Pty) Ltd Trunnion assembly
DE102006057564B3 (de) * 2006-12-07 2008-08-14 Diehl Bgt Defence Gmbh & Co. Kg Werfer zur Selbstverteidigung eines mobilen oder stationären Objektes
DE102009042517B4 (de) * 2009-09-16 2024-07-25 Vincorion Advanced Systems Gmbh Verfahren und Vorrichtung zur Waffenstabilisierung
IT1397431B1 (it) * 2009-12-11 2013-01-10 Oto Melara Spa Sistema di movimentazione per un'arma posta su una torretta.
US8286620B2 (en) * 2010-05-26 2012-10-16 Mark Williford Apparatus and method for adapting a pneumatic gun to fire from a fluid source
SG189561A1 (en) * 2011-10-12 2013-05-31 Promor Pte Ltd Roller assembly
CA2859209A1 (en) * 2011-12-20 2013-06-27 Map Pharmaceuticals, Inc. Excipient-free aerosol formulation
FR2997489B1 (fr) * 2012-10-31 2014-11-21 Nexter Systems Artillerie pivotante
US9194664B1 (en) * 2015-02-19 2015-11-24 The United States Of America As Represented By The Secretary Of The Army Main gun shield for battle tank
RU2735789C1 (ru) * 2020-03-03 2020-11-09 Акционерное общество "Всероссийский научно-исследовательский институт "Сигнал" Система наведения и стабилизации

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1996C (de) * 1912-10-21
US1880174A (en) * 1932-05-25 1932-09-27 Dugan Joseph Continuous aim gunfire control system
US2339508A (en) * 1940-06-25 1944-01-18 Ford Instr Co Inc Fire control system
GB633866A (en) * 1948-02-26 1949-12-30 Frank Andrew Landucci Improvements in and relating to gun aiming mechanism
FR2421362A1 (fr) * 1978-03-31 1979-10-26 Thomson Brandt Tourelle de tir et vehicule equipe d'une telle tourelle
SE434190B (sv) * 1979-10-02 1984-07-09 Bofors Ab Anordning for att hoja foljenoggrannheten hos ett riktsystem till en pjes
DE3241665A1 (de) * 1982-11-11 1984-05-17 Fried. Krupp Gmbh, 4300 Essen Panzerturm
DE3439082A1 (de) * 1984-10-25 1986-04-30 Wegmann & Co GmbH, 3500 Kassel Einrichtung zur durchfuehrung dynamischer vergleichsmessungen an feuerleitsystemen fuer gerichtete waffen
DE3908346A1 (de) * 1989-03-15 1990-09-20 Wegmann & Co Elevationslagerung fuer eine in einem panzerturm angeordnete grosskalibrige rohrwaffe
FR2737290B1 (fr) * 1995-07-27 1997-10-10 Giat Ind Sa Systeme de pointage d'une arme a feu montee sur un engin blinde par exemple

Also Published As

Publication number Publication date
DE60209763T2 (de) 2006-08-31
WO2003008894A1 (fr) 2003-01-30
DE60209763D1 (de) 2006-05-04
US20040200348A1 (en) 2004-10-14
ATE319975T1 (de) 2006-03-15
IL159711A0 (en) 2004-06-20
ZA200301999B (en) 2004-04-16
US6886448B2 (en) 2005-05-03
FR2827667A1 (fr) 2003-01-24
FR2827667B1 (fr) 2003-10-03
EP1407215A1 (de) 2004-04-14

Similar Documents

Publication Publication Date Title
EP1407215B1 (de) Waffenlagerungsrichtsystem
US8387740B2 (en) Motor vehicle with differential gear box providing angular movement and method therefor
EP2524816B1 (de) Drehkopplungsvorrichtung eines Drehkranzes an ein Rad, sowie mit einer solchen Vorrichtung ausgestattetes Fahrwerk eines Luftfahrzeugs
EP3665403B1 (de) Verdrehsicherung mit kabeln
EP2501960B1 (de) Sperrdifferenzial mit dynamischer schubvorrichtung
FR2875439A1 (fr) Liaison au sol pour vehicule comportant une roue et une suspension integree a la roue
EP1275534A1 (de) Kraftfahrzeugaufhängung mit veränderlichem Radsturz
FR2507726A1 (fr) Amortisseur rotatif, notamment pour vehicules a chenilles
FR2512140A1 (fr) Articulation rotative homocinetique
EP1409947B1 (de) Schusswinkel- und -lagerichtensystem
EP0279135A1 (de) Aufhängungs- und Schwenkvorrichtung von einem lenkbaren Rad eines Kraftfahrzeuges
CA2108272A1 (fr) Vehicule automobile pour prise de vues en terrains difficiles
FR2560560A1 (fr) Suspension a roues independantes a joints homocinetiques pour vehicule a moteur
CA1063388A (fr) Dispositifs de transmission de vitesse
EP0554147A1 (de) Aufhängungseinheit für ein schweres Fahrzeug, insbesondere für ein Gleiskettenfahrzeug
EP1395789B1 (de) Waffenrichtvorrichtung
EP0032079A1 (de) Gliederfahrzeug, insbesondere Gliederomnibus
FR2993331A1 (fr) Systeme mecanique a embrayage unidirectionnel et alternateur comprenant un tel systeme
FR2950310A1 (fr) Dispositif de reglage actif de voie
FR2993330A1 (fr) Systeme mecanique a embrayage unidirectionnel et alternateur comprenant un tel systeme
EP1377863B1 (de) In dem schatten eines spiegels aufgestelltes montage- und justiergerät für diesen spiegel und mit diesem gerät versehenes optisches system
WO1998009089A1 (fr) Joint de transmission tripode et procedes de montage d'un tel joint de transmission
EP3050776A1 (de) Servolenkstange, die eine rückholfeder umfasst, die mit einer dämpfenden elastomerbeschichtung ausgestattet ist
FR2484627A1 (fr) Installation de tir d'armes dirigeables
FR2760408A1 (fr) Amortisseur a friction reglable, et essieu de vehicule dote d'un tel amortisseur

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: 20040112

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 IE IT LI LU MC NL PT SE SK TR

AX Request for extension of the european patent

Extension state: AL LT LV MK RO SI

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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 IE IT LI LU MC NL PT SE SK TR

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

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: 20060308

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: 20060308

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: 20060308

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: 20060308

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: NV

Representative=s name: ING. MARCO ZARDI C/O M. ZARDI & CO. S.A.

Ref country code: CH

Ref legal event code: EP

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20060308

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: 60209763

Country of ref document: DE

Date of ref document: 20060504

Kind code of ref document: P

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

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: 20060608

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: 20060608

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: 20060619

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

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: 20060731

Ref country code: BE

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

Effective date: 20060731

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: 20060808

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

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: 20061211

BERE Be: lapsed

Owner name: GIAT INDUSTRIES

Effective date: 20060731

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

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: 20060308

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: 20060609

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: 20060308

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: 20060715

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: 20060308

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

Ref country code: CH

Payment date: 20080708

Year of fee payment: 7

Ref country code: DE

Payment date: 20080730

Year of fee payment: 7

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: 20060308

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

Ref country code: AT

Payment date: 20080714

Year of fee payment: 7

Ref country code: FR

Payment date: 20080728

Year of fee payment: 7

Ref country code: IT

Payment date: 20080719

Year of fee payment: 7

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

Ref country code: GB

Payment date: 20080630

Year of fee payment: 7

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

Ref country code: SE

Payment date: 20080626

Year of fee payment: 7

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

EUG Se: european patent has lapsed
GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20090715

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20100331

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

Ref country code: LI

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

Effective date: 20090731

Ref country code: FR

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

Effective date: 20090731

Ref country code: CH

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

Effective date: 20090731

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

Ref country code: GB

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

Effective date: 20090715

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

Ref country code: DE

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

Effective date: 20100202

Ref country code: AT

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

Effective date: 20090715

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

Ref country code: IT

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

Effective date: 20090715

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

Ref country code: SE

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

Effective date: 20090716