EP0240819A2 - Procédé de détournement de missiles à guidage radar ou infrarouge, en particulier pour la défense des navires et unités navales, et dispositif pour la mise en oeuvre du procédé - Google Patents
Procédé de détournement de missiles à guidage radar ou infrarouge, en particulier pour la défense des navires et unités navales, et dispositif pour la mise en oeuvre du procédé Download PDFInfo
- Publication number
- EP0240819A2 EP0240819A2 EP19870104219 EP87104219A EP0240819A2 EP 0240819 A2 EP0240819 A2 EP 0240819A2 EP 19870104219 EP19870104219 EP 19870104219 EP 87104219 A EP87104219 A EP 87104219A EP 0240819 A2 EP0240819 A2 EP 0240819A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- deflection
- missile
- throwing
- deflection curve
- predetermined
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
- F41G7/224—Deceiving or protecting means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
Definitions
- the invention relates to a method for deflecting missiles guided by radar and / or infrared radiation, in particular for the protection of seagoing vessels and ship groups, in which projectiles producing mock targets are ignited in or in front of the target area of the missile.
- the object underlying the invention was to develop a method of the type mentioned in the preamble of claim 1 in such a way that the approaching missile is deflected in a predetermined deflection direction, which can be determined so that the missile no longer moves after its deflection is able to switch to an alternative destination.
- the invention further relates to a device for carrying out the method according to the invention with the features from patent claim 6, an advantageous embodiment of this device being described in patent claim 7.
- the method according to the invention is primarily intended to protect ship groups, but it can also be used to protect individual ships, for example in the form that ships in crisis areas, for example tankers, can be equipped with a device according to the invention in order to counteract the To be protected by missiles and to protect other tankers traveling in a convoy.
- the device according to the invention When using the method according to the invention for the protection of ship groups, it may also be advantageous to install the device according to the invention on unmanned escort ships, so that the diversion can be carried out at a relatively great distance from the ship group, where there is sufficient space for fixing the direction of deflection is available.
- Conventional throwing bodies can be used as throwing bodies, which, for example, for generating an infrared glow target contain a certain effective mass known per se, due to which after ignition of the throwing body an infrared radiation-imitating cloud arises which has a low sinking speed with a large radiation area and thus has a ship-like characteristic.
- Throwing bodies can be used to deflect radar-controlled missiles which contain a so-called "double active mass" which is released after the firing body has been ignited.
- double active mass a so-called "double active mass" which is released after the firing body has been ignited.
- the method according to the invention can be used in many different ways.
- the device according to the invention can be used both to protect the association and to protect the support boat itself.
- the device for carrying out a method for deflecting missiles guided by radar and / or infrared radiation basically has the following individual devices:
- This locating device can contain, in a manner known per se, a radar device and additional devices such as a periscope, a night vision device and / or an optical distance measuring device. Furthermore, it contains devices known per se for generating electrical data representing the determined values. This data is fed to a data processing system 2, which is also constructed in a manner known per se and, based on corresponding programs, calculates a deflection curve for the missile from the determined data based on a predetermined deflection direction, in the manner in which this is explained in more detail below.
- the data processing system 2 also generates electrical control signals which are fed to a control device 3 to which a throwing pillar 4 is connected, which is also explained in more detail below.
- Throwing pillars 4 are fired by means of the throwing column 4, specifically with respect to the firing direction and firing sequence in such a way that at the end of the trajectory of the throwing body, after firing, apparent targets appear which lie at predetermined points of the calculated deflection curve. The conditions that occur here are explained in more detail below with reference to FIGS. 4 and 5.
- a device according to FIG. 1 is installed on a ship S, for example an escort boat of a ship association.
- a missile FK controlled for example, by infrared radiation is located, the direction of flight FB1 of which is determined together with the flight speed and possibly the type of missile. Furthermore, a deflection direction FB2 is specified and a deflection curve AK is calculated, which can be part of a parabola, for example, one branch of which connects to the approach path FB1 and the other branch to the deflection direction FB2.
- corresponding throwing bodies On the basis of the evaluated data, corresponding throwing bodies have to be fired from the ship S on ballistic tracks P1, P2, P3, P4, P5 and P6 in such directions and in a predetermined time sequence that the apparent targets Z1, Z2, Z3, Z4 are successively on the deflection curve AK , Z5 and Z6 arise so that the missile FK is successively oriented towards these apparent targets and thereby changes its trajectory overall in such a way that it continues to fly on the deflection curve AK and is finally deflected in the deflection direction FB2.
- the throwing bodies are preferably shot in such a way that the ballistic tracks P1 to P6 are all the same Have an elevation angle of 45 °.
- the clouds emitting infrared radiation representing the apparent targets Z1 to Z6 lie essentially in a horizontal plane, so that the missile FK is deflected on a horizontal path.
- the missile FK is deflected by approximately 90 ° from its approach direction.
- six apparent targets are sufficient in the described method, for example.
- the deflection curve AK to be built up by the six apparent targets Z1 to Z6 is designed in such a way that the missile FK can follow this curve in any case, taking into account its own maneuverability and viewing window size.
- the deflection curve AK can also be constructed mirrored on the approach direction FB1, so that the deflection in FIG. 4 does not take place to the right but to the left.
- FIG. 1 the launching column 4 shown in FIG. 1 is shown in somewhat more detail.
- the throwing pillar 4 shown has a basic device 4.1, which is connected to the control device 3 in the manner shown in FIG. 1.
- a base plate 4.2 is arranged above the basic device, on which a two-part column 4.3-4.4 is rotatably arranged in a controllable manner.
- twelve throwing devices are arranged at an elevation angle of 45 ° in six rows arranged one above the other on the circumference.
- On the upper part 4.4 of the column there are twelve throwing devices in three rows arranged on the circumference, which are also at an elevation angle of 45 °.
- the throwing devices 4.31 to 4.36 arranged in the lower part 4.3 of the column serve to produce deflection curves which are intended to protect a ship's association, while the throwing bodies arranged in the upper part 4.4 of the column are intended for the self-protection of the escort ship.
- Rows 4.31 to 4.36 and 4.41 to 4.43 can each be equipped with combined IR and radar dummy targets, which have different ranges and disassembly times. With the help of these different ranges and dismantling times, the predicted deflection curves can be produced in connection with the side-aiming of the throwing pillar and a certain firing rate by the dummy targets.
- the deflection measure can be carried out twelve times with the lower part of the launcher column 4.3 before it is necessary to reload the launcher column.
- the twelve groups of throwing devices, each with six different throwing bodies, are loaded from top to bottom in row 4.36 with the throwing body that has the shortest range and ending in row 4.31 with the throwing body that has the greatest range (recoil) and therefore to avoid large ones Moments close to the turntable of the thrower column is arranged.
- the upper part 4.4 of the launcher column can be used correspondingly equipped rows 4.41 to 4.43 missiles are fired, which create false targets, which are intended to protect the escort boat itself.
- the creation of a certain deflection curve may be dispensed with, and it is only intended to prevent the escort ship itself from being hit by the apparent targets generated.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3612183 | 1986-04-11 | ||
DE19863612183 DE3612183A1 (de) | 1986-04-11 | 1986-04-11 | Verfahren zur ablenkung von durch radar- und/oder infrarotstrahlung gelenkten flugkoerpern, insbesondere zum schutz von seeschiffen und schiffsverbaenden sowie einrichtung zur durchfuehrung des verfahrens |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0240819A2 true EP0240819A2 (fr) | 1987-10-14 |
EP0240819A3 EP0240819A3 (en) | 1989-03-22 |
EP0240819B1 EP0240819B1 (fr) | 1993-09-15 |
Family
ID=6298452
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP87104219A Expired - Lifetime EP0240819B1 (fr) | 1986-04-11 | 1987-03-21 | Procédé de détournement de missiles à guidage radar ou infrarouge, en particulier pour la défense des navires et unités navales, et dispositif pour la mise en oeuvre du procédé |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0240819B1 (fr) |
DE (2) | DE3612183A1 (fr) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4115384A1 (de) * | 1991-05-10 | 1992-11-12 | Buck Chem Tech Werke | Verfahren zum schuetzen von eine ir-strahlung abgebenden objekten und wurfkoerper zur durchfuehrung des verfahrens |
EP0597233A1 (fr) * | 1992-11-11 | 1994-05-18 | Buck Werke GmbH & Co | Méthode de production d'un objet de leurre |
DE4437729C1 (de) * | 1994-10-21 | 1996-04-25 | Buck Chem Tech Werke | Verfahren zum Schützen von eine IR-Strahlung abgebenden Objekten, insbesondere Schiffen, gegen Flugkörper |
EP0811853A1 (fr) * | 1996-06-07 | 1997-12-10 | ETAT FRANCAIS représenté par le DELEGUE GENERAL pour L'ARMEMENT | Procédé de conduite et de protection d'un navire |
FR2780774A1 (fr) * | 1998-07-03 | 2000-01-07 | Alkan Sa | Dispositif d'autoprotection passive pour engin mobile tel qu'un helicoptere |
GB2374134A (en) * | 2001-04-04 | 2002-10-09 | Buck Neue Technologien Gmbh | Method and apparatus for the protection of mobile military facilities |
WO2003081167A1 (fr) * | 2002-03-27 | 2003-10-02 | Diehl Munitionssysteme Gmbh & Co. Kg | Procede pour proteger un objet |
WO2003093757A1 (fr) * | 2002-05-03 | 2003-11-13 | Raytheon Company | Procede permettant de proteger un aeronef contre une menace au moyen d'un capteur infrarouge |
EP1128152A3 (fr) * | 2000-02-23 | 2004-05-19 | Krauss-Maffei Wegmann GmbH & Co. KG | Système lançeur pour charges fumigènes et explosives monté sur un véhicule de combat |
WO2005033616A1 (fr) * | 2003-10-02 | 2005-04-14 | Rheinmetall Waffe Munition Gmbh | Procede et dispositif de protection de bateaux contre des missiles guides en phase terminale |
DE102004005105A1 (de) * | 2004-02-02 | 2005-09-01 | Buck Neue Technologien Gmbh | Objektschutzsystem und Verfahren zum Schützen von Objekten |
EP1746381A1 (fr) | 2005-07-18 | 2007-01-24 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Dispositif et méthode de protection contre des missiles et ustilisation d'un dispositif laser |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3705700A1 (de) * | 1987-02-23 | 1988-09-01 | Buck Chem Tech Werke | Werfereinheit |
DE3835887C2 (de) * | 1988-10-21 | 1997-10-02 | Rheinmetall Ind Ag | Patrone zur Scheinzielerzeugung |
FR2840977B1 (fr) | 2002-06-12 | 2004-09-03 | Giat Ind Sa | Dispositif et munition de protection d'un vehicule ou d'une plate-forme fixe contre une menace |
DE102006017107A1 (de) | 2006-04-10 | 2007-10-11 | Oerlikon Contraves Ag | Schutzeinrichtung und Schutzmaßnahme für eine Radaranlage |
DE102011014599B4 (de) * | 2011-03-22 | 2016-12-08 | Diehl Bgt Defence Gmbh & Co. Kg | Verfahren zum Schützen eines Objekts vor einem Angriff eines anfliegenden Flugobjekts |
DE102011052616A1 (de) * | 2011-03-28 | 2012-10-04 | Peter Huber | Vorrichtung und Verfahren zur Verteidigung eines Zielobjekts gegen mindestens einen angreifenden Flugkörper |
DE102020119231B4 (de) | 2020-07-21 | 2022-07-21 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Militärische Wurfanlage |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1006376A (fr) * | 1948-01-05 | 1952-04-22 | Déviation de la trajectoire d'une bombe, qui est dirigée à l'aide des photo-cellules | |
US3126544A (en) * | 1964-03-24 | Method of deception for an aircraft | ||
US3150848A (en) * | 1961-06-28 | 1964-09-29 | Samuel E Lager | Method of decoying a missile from its intended target |
FR2383419A1 (fr) * | 1977-03-07 | 1978-10-06 | Lacroix E | Valise lance-leurres pour la deception des systemes de guidage d'armes |
-
1986
- 1986-04-11 DE DE19863612183 patent/DE3612183A1/de not_active Withdrawn
-
1987
- 1987-03-21 EP EP87104219A patent/EP0240819B1/fr not_active Expired - Lifetime
- 1987-03-21 DE DE87104219T patent/DE3787391D1/de not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3126544A (en) * | 1964-03-24 | Method of deception for an aircraft | ||
FR1006376A (fr) * | 1948-01-05 | 1952-04-22 | Déviation de la trajectoire d'une bombe, qui est dirigée à l'aide des photo-cellules | |
US3150848A (en) * | 1961-06-28 | 1964-09-29 | Samuel E Lager | Method of decoying a missile from its intended target |
FR2383419A1 (fr) * | 1977-03-07 | 1978-10-06 | Lacroix E | Valise lance-leurres pour la deception des systemes de guidage d'armes |
Non-Patent Citations (3)
Title |
---|
E.KRAMAR,FUNKSYSTEME FÜR ORTUNG UND NAVIGATION,VERLAG BERLINER UNION,SEITEN 18 und 25. * |
REVUE INTERNATIONALE DE DEFENSE, Band 11, Nr. 5, 1978, Seite 743, Cointrin, Genève, CH; "Un système polyvalent de leurres électromagnétiques" * |
REVUE INTERNATIONALE DE DEFENSE, Band 16, Nr. 4, 1983, Seiten 475-477, Cointrin, Genève, CH; M. HEWISH: "Le système naval de leurrage Shield de Plessey Aerospace" * |
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4115384A1 (de) * | 1991-05-10 | 1992-11-12 | Buck Chem Tech Werke | Verfahren zum schuetzen von eine ir-strahlung abgebenden objekten und wurfkoerper zur durchfuehrung des verfahrens |
EP0597233A1 (fr) * | 1992-11-11 | 1994-05-18 | Buck Werke GmbH & Co | Méthode de production d'un objet de leurre |
DE4437729C1 (de) * | 1994-10-21 | 1996-04-25 | Buck Chem Tech Werke | Verfahren zum Schützen von eine IR-Strahlung abgebenden Objekten, insbesondere Schiffen, gegen Flugkörper |
EP0811853A1 (fr) * | 1996-06-07 | 1997-12-10 | ETAT FRANCAIS représenté par le DELEGUE GENERAL pour L'ARMEMENT | Procédé de conduite et de protection d'un navire |
FR2749669A1 (fr) * | 1996-06-07 | 1997-12-12 | France Etat | Procede de conduite et de protection d'un navire |
FR2780774A1 (fr) * | 1998-07-03 | 2000-01-07 | Alkan Sa | Dispositif d'autoprotection passive pour engin mobile tel qu'un helicoptere |
WO2000002000A1 (fr) * | 1998-07-03 | 2000-01-13 | Alkan | Dispositif d'autoprotection passive pour engin mobile tel qu'un helicoptere |
EP1128152A3 (fr) * | 2000-02-23 | 2004-05-19 | Krauss-Maffei Wegmann GmbH & Co. KG | Système lançeur pour charges fumigènes et explosives monté sur un véhicule de combat |
FR2823296A1 (fr) * | 2001-04-04 | 2002-10-11 | Buck Neue Technologien Gmbh | Procede et appareil pour la protection d'installations militaires mobiles |
GB2374134A (en) * | 2001-04-04 | 2002-10-09 | Buck Neue Technologien Gmbh | Method and apparatus for the protection of mobile military facilities |
GB2374134B (en) * | 2001-04-04 | 2004-09-15 | Buck Neue Technologien Gmbh | Method and apparatus for the protection of mobile military facilities |
WO2003081167A1 (fr) * | 2002-03-27 | 2003-10-02 | Diehl Munitionssysteme Gmbh & Co. Kg | Procede pour proteger un objet |
WO2003093757A1 (fr) * | 2002-05-03 | 2003-11-13 | Raytheon Company | Procede permettant de proteger un aeronef contre une menace au moyen d'un capteur infrarouge |
AU2003223737B2 (en) * | 2002-05-03 | 2006-07-06 | Raytheon Company | Method for protecting an aircraft against a threat that utilizes an infrared sensor |
WO2005033616A1 (fr) * | 2003-10-02 | 2005-04-14 | Rheinmetall Waffe Munition Gmbh | Procede et dispositif de protection de bateaux contre des missiles guides en phase terminale |
US7886646B2 (en) | 2003-10-02 | 2011-02-15 | Rheinmetall Waffe Munition Gmbh | Method and apparatus for protecting ships against terminal phase-guided missiles |
DE102004005105A1 (de) * | 2004-02-02 | 2005-09-01 | Buck Neue Technologien Gmbh | Objektschutzsystem und Verfahren zum Schützen von Objekten |
EP1746381A1 (fr) | 2005-07-18 | 2007-01-24 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Dispositif et méthode de protection contre des missiles et ustilisation d'un dispositif laser |
DE102005034613B3 (de) * | 2005-07-18 | 2007-03-29 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Abwehrvorrichtung gegen Flugkörper, Verfahren zur Abwehr gegen Flugkörper und Verwendung einer Laservorrichtung |
Also Published As
Publication number | Publication date |
---|---|
EP0240819B1 (fr) | 1993-09-15 |
EP0240819A3 (en) | 1989-03-22 |
DE3612183A1 (de) | 1987-10-22 |
DE3787391D1 (de) | 1993-10-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0240819B1 (fr) | Procédé de détournement de missiles à guidage radar ou infrarouge, en particulier pour la défense des navires et unités navales, et dispositif pour la mise en oeuvre du procédé | |
EP1668310B1 (fr) | Procede et dispositif de protection de bateaux contre des missiles guides en phase terminale | |
DE2907590A1 (de) | Verfahren und vorrichtung zum auswerten von simulierten schiessuebungen mit einer waffe auf ein ziel | |
EP0597233B1 (fr) | Méthode de production d'un objet de leurre | |
DE2803036A1 (de) | Gelenkte bombe fuer den tiefflugeinsatz | |
DE2905422C2 (de) | Einrichtung zur Schußsimulation mit Trefferanzeige | |
DE69121427T2 (de) | Geschoss und sein Verwendungsverfahren | |
Corum | The Luftwaffe's Army Support Doctrine, 1918–1941 | |
EP1090263A1 (fr) | Procede pour combattre a distance des cibles proches du sol et/ou sur le sol | |
DE602005000222T2 (de) | Flugkörper zur Geländeaufklärung | |
DE69911608T2 (de) | Passive selbstschutzvorrichtung für bewegliche objekte wie zum beispiel einen helikopter | |
DE3421734A1 (de) | Verfahren zum schutz von infrarot-strahlenden zielen, insbesondere von schiffen, vor mit infrarot-lenksuchkoepfen ausgeruesteten flugkoerpern | |
DE2634462C1 (de) | U-Boot Waffensystem | |
DE1951622C3 (de) | Anordnung zur simulierten Darstellung von Schußbahnen | |
DE102018110241A1 (de) | Verfahren und Vorrichtung zum Schutz eines Fahrzeugs vor einer Bedrohung | |
DE2746534C2 (de) | Verfahren zur Simulation eines beweglichen Zieles | |
DE2522927C2 (de) | System zur taeuschung, ablenkung und vernichtung von lenkwaffen | |
DE3013405A1 (de) | Verfahren zum vermeiden des nachrichtens von abschussgeraeten fuer ballistische flugkoerper | |
DE3211711A1 (de) | Uebungsvorrichtung fuer die schiessausbildung an lenkflugkoerpern, insbesondere an boden-boden-flugkoerperwaffen | |
EP0913661B1 (fr) | Dispositif pour protéger des objets mobiles, en particulier des véhicules blindés, contre des projectiles | |
DE3734758C2 (fr) | ||
DE102018131524A1 (de) | Verfahren zum Schutz von beweglichen oder unbeweglichen Objekten vor sich nähernden lasergelenkten Bedrohungen | |
DE3311530C2 (de) | Unterwasserfahrzeug | |
EP0187900B1 (fr) | Avion non équipé pour la lutte contre cibles terrestres | |
DE2156974A1 (de) | Behaelter zur aufnahme von streuwaffen, die am einsatzort aus dem von einem flugzeug getragenen behaelter ausgestossen werden |
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 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): BE CH DE FR GB IT LI NL |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): BE CH DE FR GB IT LI NL |
|
17P | Request for examination filed |
Effective date: 19890829 |
|
17Q | First examination report despatched |
Effective date: 19910905 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: BUCK WERKE GMBH & CO |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: GRUNDLER, JOHANNES Inventor name: HERBST, ROLF |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): BE CH DE FR GB IT LI NL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Effective date: 19930915 |
|
REF | Corresponds to: |
Ref document number: 3787391 Country of ref document: DE Date of ref document: 19931021 |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 19930924 |
|
ITF | It: translation for a ep patent filed |
Owner name: SOCIETA' ITALIANA BREVE |
|
ET | Fr: translation filed | ||
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Effective date: 19940331 Ref country code: CH Effective date: 19940331 |
|
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 | ||
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 19960228 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 19960306 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 19960331 Year of fee payment: 10 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Effective date: 19970321 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Effective date: 19971001 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19970321 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19971128 |
|
NLV4 | Nl: lapsed or anulled due to non-payment of the annual fee |
Effective date: 19971001 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20000224 Year of fee payment: 14 |
|
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: 20020101 |
|
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;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED. Effective date: 20050321 |