EP1637829B1 - Pack of heat-generating countermeasures - Google Patents

Pack of heat-generating countermeasures Download PDF

Info

Publication number
EP1637829B1
EP1637829B1 EP04445095.5A EP04445095A EP1637829B1 EP 1637829 B1 EP1637829 B1 EP 1637829B1 EP 04445095 A EP04445095 A EP 04445095A EP 1637829 B1 EP1637829 B1 EP 1637829B1
Authority
EP
European Patent Office
Prior art keywords
bodies
pack
heat
joined
oxidizing
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.)
Not-in-force
Application number
EP04445095.5A
Other languages
German (de)
French (fr)
Other versions
EP1637829A1 (en
Inventor
Christer ZÄTTERQVIST
Johan Friede
Martin Ringstedt
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.)
Saab AB
Original Assignee
Saab AB
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 Saab AB filed Critical Saab AB
Priority to DK04445095.5T priority Critical patent/DK1637829T3/en
Priority to EP04445095.5A priority patent/EP1637829B1/en
Priority to ES04445095.5T priority patent/ES2638241T3/en
Publication of EP1637829A1 publication Critical patent/EP1637829A1/en
Application granted granted Critical
Publication of EP1637829B1 publication Critical patent/EP1637829B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B4/00Fireworks, i.e. pyrotechnic devices for amusement, display, illumination or signal purposes
    • F42B4/26Flares; Torches
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J2/00Reflecting targets, e.g. radar-reflector targets; Active targets transmitting electromagnetic or acoustic waves
    • F41J2/02Active targets transmitting infrared radiation

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Packages (AREA)
  • Air Bags (AREA)

Description

  • In accordance with the preamble of independent claim 1, the present invention relates to a pack of heat-generating countermeasures comprising a container with a lid forming a tight-closing pack and accommodating heat-generating countermeasures in the form of material which oxidizes on contact with oxygen and thus generates heat, which is intended to be dispensed from sea, land or air-based systems, heat being generated when the pack, on being dispensed, is opened so that the contents of the pack come into contact with the oxygen in the air and are oxidized. Packs of this kind are used for generating decoys to counter heat-seeking homing missiles.
  • A common type of decoy to counter heat-seeking homing missiles is hot bodies which are placed in the field of vision of the missile and are intended to disrupt the target seeker. Conventionally, pyrotechnic magnesium-based flares have been used. These maintain a relatively high temperature, which means that the ratio between the heat signature of the flare and the signature of the aircraft tends to be greater than one, which is normally attractive to a thermal-target seeker. More modern thermal-target seekers may be equipped with filters and other devices which, using various techniques, distinguish such flares. It is therefore of interest instead to make use of oxidizing heat-generating material with a lower temperature and a larger radiating area, which can obtain a ratio between the oxidizing heat-generating material and the heat signature of the aircraft which is greater than one without activating these filters and other devices.
  • In this connection, it is previously known from our Swedish patent application 0300322-5 to use oxidizing material in the form of oxidizing iron sulphide in powder form or coated on a substrate, for example a metal strip. In the latter case, the substrate is heated by the oxidizing material and acts as a black or grey body radiator. In this connection, black body means an ideal heat radiator which behaves according to Planck's law, while a grey body is a body of which the radiation properties have the same spectral distribution as a black body but not the same intensity. The substrate therefore acts as both a carrier and a grey body radiator in the form of a heat buffer but not as a heat generator.
  • In utilization of the technique with oxidizing heat-generating material, it is inter alia desirable to:
    1. 1. maximize the quantity of oxidizing material in a given volume.
    2. 2. adapt the oxidation properties of the oxidizing material to the situation in which it is to be used, for example to the heat signature of the platform or to the characteristics of the expected threat.
    3. 3. minimize the quantity of material which lands on the ground after use. This is of particular importance when used in civil aviation.
  • The object of the present invention is to produce a pack of heat-generating countermeasures which satisfies the wishes referred to above better than previously known constructions. The object of the invention is achieved in accordance with the characterizing part of independent claim 1 by a pack characterized in that the oxidizing material consists essentially of oxidizing powder joined together to form one or more joined-together bodies. The oxidizing heat-generating bodies are therefore completely or virtually completely constructed from oxidizing material, which means that they act as carrier, heat generator and grey body radiator at one and the same time. By using the oxidizing material as a grey radiator, a greater quantity of oxidizing material can be enclosed within a given volume. This can be utilized in order, for example, to generate a longer burning time or alternatively a greater radiating area per given volume. Moreover, the maximum operating temperature and rise time of the bodies can be controlled and adapted to the situation in which they are to be used. After use, the oxidizing heat-generating bodies will have burned up completely or virtually completely before they reach the ground, which minimizes contamination on the ground or platform.
  • According to an advantageous embodiment of the invention, the joined-together bodies formed by joining the oxidizing powder together consist essentially of iron sulphide. The joining-together can be effected by, for example, a sintering process to form a body of suitable shape and mass.
  • Alternatively, the joined-together bodies can consist essentially of a pure metal such as iron or aluminium.
  • In order to hold the bodies formed by the joined-together powder together, the bodies can, according to another advantageous embodiment, comprise binder. Alternatively, the bodies can comprise reinforcement or binder and reinforcement in combination. The reinforcement can be in the form of, for example, glass fibre, and the binder can be in the form of, for example, potassium bromide.
  • According to another advantageous embodiment, the bodies include substances which, when oxidation of the oxidizing material takes place, give off exhaust-gas-like gases, such as, for example, CO, CO2 or H2O. By imitating the gases which are found in proximity to the exhaust discharge of an engine while generating heat radiation in certain frequency bands, it is possible to make it more difficult for certain advanced heat-seeking homing missiles to distinguish the oxidizing heat-generating bodies as decoys.
  • The decisive factors for the action of the oxidizing heat-generating bodies against a heat-seeking homing missile are their temperature, their emissivity, their number, the spread of the bodies in the space within the field of vision of the target seeker and their radiating area projected in the field of vision of the missile. The time it takes for the body to reach its operating temperature from ambient temperature and how long the body is capable of maintaining this temperature also have an effect. The design of the body will also control the way in which the body is cooled by conduction and convection and influence its aerodynamic qualities. It is therefore desirable for it to be possible to vary the design of the bodies according to application, that is to say according to the platform to be protected and according to the threat which can be expected.
  • The oxidizing heat-generating bodies are of the nature of a pellet. The shape of the bodies can therefore be adapted so that all the characteristics mentioned above are adapted to the demands made in an operational situation. An important parameter controlled by the shape is the ratio between surface area and volume. The larger the surface area exposed to air, the greater the effect produced. A higher ratio therefore gives a higher temperature but a shorter burning time for a given volume (mass). Generally, it can also be said that cooling and air resistance increase as the ratio increases. A typical design of the oxidizing heat-generating bodies which tends to give a high burning temperature is a rectangular or square body with a thin cross section. Such a body is suitable for protecting a platform with high heat radiation of its own. Such a body also has an extent and shape suitable for packing in a box. By increasing the thickness of the body, but retaining the same basic shape, a lower burning temperature and a smaller radiating area but a longer burning time are obtained. Such a body is suitable for protecting a platform with a lower heat radiation of its own and a lower speed, which means that the body will remain in the field of vision of the target seeker for a longer time, for which reason a longer burning time is desirable. A typical such platform is a slow-moving transport aircraft or a civil passenger aircraft.
  • It is clear from the above that the joined-together bodies can have a varying shape depending on the requirements in an operational situation. In this context, however, two shape types are indicated.
  • In this connection, according to a first advantageous embodiment of the pack, the bodies are designed with an essentially spherical shape. By virtue of their spherical shape, good strength and a slow oxidization process are obtained.
  • According to a second advantageous embodiment, the bodies are designed with an essentially flat rectangular shape. The shape allows the space in standardized flat containers for countermeasures to be filled efficiently. By changing the thickness, for example, the burning time and burning temperature can be adjusted.
  • The invention will be described in greater detail below by means of an illustrative embodiment with reference to accompanying drawings, in which:
    • Figure 1 shows diagrammatically in a longitudinal section a dispenser loaded with packs of countermeasures according to the invention;
    • Figure 2 shows diagrammatically a pack of heat-generating countermeasures according to the invention;
    • Figures 3a-c show three examples of suitable shapes for the joined-together bodies which constitute the oxidizing material of the pack, and
    • Figure 4 shows examples of burning profile based on burning temperature as a function of time.
  • The dispenser 1 shown diagrammatically in Figure 1 is filled with packs 2 which, when opened, generate heat. A spring-loaded piston 3 displaces the packs towards the opening 4 of the dispenser 1 where a mechanical launching mechanism 5 launches one pack at a time through the opening 4. Adjacent to the opening 4 is an opening mechanism 6 for opening the packs in connection with their being launched or dispensed. The opening mechanism 6 can comprise some form of gripping means which takes hold of and pulls off an openable part of the pack. Alternatively, the opening mechanism can comprise some form of cutting means, for example a knife, which cuts open the pack in connection with it leaving the dispenser.
  • The pack 2 shown in Figure 2 comprises a container 7 consisting of a bottom plate 8 and four side walls 9-12. The container is closed by a lid 13 which can be, for example, glued firmly to the edges of the side walls 9-12 facing the lid 13. The container accommodates joined-together bodies 14 indicated by broken lines which constitute oxidizing material and thus react with oxygen, generating heat, when the pack is opened and the air is given access. In this example, the bodies are indicated as having a flat rectangular shape, but there are many other possible shapes.
  • Examples of shapes which may be suitable for the joined-together bodies are shown in Figure 3. Figure 3a shows a spherical shape. The spherical shape has a small surface area in relation to volume and can advantageously be used if a long burning time is required. The spheres can be given a larger or smaller diameter depending on the desired effect. It may also be suitable to mix different sizes. The bodies 14 shown in Figures 3b and 3c have two plane opposite rectangular main surfaces 19, 20, and the one shown in Figure 3c is more elongate than the one shown in Figure 3b. By varying the thickness of the bodies, for example, the burning time and burning temperature can be changed. In principle, it can be said that a thicker body with the same volume as a thinner one gives a lower burning temperature and longer burning time. The shapes shown in Figures 3b and 3c lend themselves especially well to being packed in the type of pack shown in Figure 2. The bodies can relatively easily be dimensioned so that they fill the entire interior of the pack.
  • Figure 4 shows examples of how the burning temperature T can vary as a function of time t. In this connection, the upper curve 15 shows a burning profile with a relatively high burning temperature and short burning time, while the lower curve 16 shows a burning profile with a relatively low burning temperature and long burning time. It can be useful if the front flanks 17, 18 of the curves are relatively steep so that the countermeasures work with full force quickly.
  • The invention is not limited to the embodiments shown as examples above but can undergo modifications within the scope of the patent claims below.

Claims (8)

  1. Pack of heat-generating countermeasures comprising a container with a lid forming a tight-closing pack and accommodating heat-generating countermeasures in the form of material which oxidizes on contact with oxygen and thus generates heat, which pack is intended to be dispensed from sea, land or air-based systems, heat being generated when the pack, on being dispensed, is opened so that the contents of the pack come into contact with the oxygen in the air and are oxidized, characterized in that the oxidizing material consists essentially of oxidizing powder joined together to form one or more joined-together bodies, the oxidizing heat-generating bodies being completely or virtually completely constructed from oxidizing material, wherein said bodies act as carrier, heat generator and grey body radiator at one and the same time.
  2. Pack according to patent claim 1, characterized in that the joined-together bodies formed by joining the powder together consist essentially of iron sulphide.
  3. Pack according to patent claim 1, characterized in that the joined-together bodies consist essentially of pure metal such as iron or aluminium.
  4. Pack according to any one of the preceding patent claims, characterized in that the bodies formed by the joined-together powder comprise binder in order to hold the individual body together.
  5. Pack according to any one of the preceding patent claims, characterized in that the bodies formed by the joined-together powder comprise reinforcement in order to hold the individual body together.
  6. Pack according to any one of the preceding patent claims, characterized in that the bodies include substances which, when oxidation of the oxidizing material takes place, give off exhaust-gas-like gases, such as, for example, CO, CO2 or H2O.
  7. Pack according to any one of the preceding patent claims, characterized in that the bodies are designed with essentially spherical shape.
  8. Pack according to any one of preceding patent claims 1-6, characterized in that the bodies are designed with an essentially flat rectangular shape.
EP04445095.5A 2004-09-15 2004-09-15 Pack of heat-generating countermeasures Not-in-force EP1637829B1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DK04445095.5T DK1637829T3 (en) 2004-09-15 2004-09-15 Package of heat-generating countermeasures
EP04445095.5A EP1637829B1 (en) 2004-09-15 2004-09-15 Pack of heat-generating countermeasures
ES04445095.5T ES2638241T3 (en) 2004-09-15 2004-09-15 Heat generating countermeasures package

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP04445095.5A EP1637829B1 (en) 2004-09-15 2004-09-15 Pack of heat-generating countermeasures

Publications (2)

Publication Number Publication Date
EP1637829A1 EP1637829A1 (en) 2006-03-22
EP1637829B1 true EP1637829B1 (en) 2017-05-31

Family

ID=34932997

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04445095.5A Not-in-force EP1637829B1 (en) 2004-09-15 2004-09-15 Pack of heat-generating countermeasures

Country Status (3)

Country Link
EP (1) EP1637829B1 (en)
DK (1) DK1637829T3 (en)
ES (1) ES2638241T3 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2396221A4 (en) * 2009-02-11 2014-03-12 Saab Ab Decoy material package, a dispenser and a method for dispensing decoy material
US8403253B1 (en) 2009-03-18 2013-03-26 Israel Aerospace Industries Ltd. Active IR signature target simulation system and a method thereof
EP4070030B1 (en) * 2019-12-05 2024-05-15 Saab Ab System for ejection of countermeasure boxes

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE757673A (en) * 1969-11-05 1971-04-01 France Etat PYROTECHNIC COMPOSITION WITH HIGH LUMINOUS POWER AND ITS MANUFACTURING PROCESS
US4978400A (en) * 1989-11-17 1990-12-18 General Sciences, Inc. Synergistic composite pyrotechnic material
US5472533A (en) * 1994-09-22 1995-12-05 Alliant Techsystems Inc. Spectrally balanced infrared flare pyrotechnic composition
GB9612655D0 (en) * 1996-06-17 2003-05-28 Secr Defence Infra-red emitting decoy flare
AU5243598A (en) * 1996-11-15 1998-06-22 Cordant Technologies, Inc. Extrudable black body decoy flare compositions and methods of use
US6427599B1 (en) * 1997-08-29 2002-08-06 Bae Systems Integrated Defense Solutions Inc. Pyrotechnic compositions and uses therefore
US6055909A (en) * 1998-09-28 2000-05-02 Raytheon Company Electronically configurable towed decoy for dispensing infrared emitting flares
SE525519C2 (en) * 2003-02-10 2005-03-01 Saab Ab Process for producing heat-generating countermeasures, as well as packaging with heat-generating countermeasures

Also Published As

Publication number Publication date
ES2638241T3 (en) 2017-10-19
EP1637829A1 (en) 2006-03-22
DK1637829T3 (en) 2017-08-28

Similar Documents

Publication Publication Date Title
US8783183B2 (en) Active body
EP2464944B1 (en) Projectile with a multi-spectral marking plume
US5445078A (en) Apparatus and method for dispensing payloads
EP3153811B1 (en) Decoys for infra-red radiation seeking missiles and methods of producing and using the same
US7421950B2 (en) Decoys for infra-red radiation seeking missiles and methods of producing and using the same
US8813649B1 (en) Low foreign object damage (FOD) weighted nose decoy flare
US7343861B1 (en) Device and method for producing an infrared emission at a given wavelength
US20090166568A1 (en) Method and Apparatus For Electromagnetic Emission By Reactive Composite Materials
IL192920A (en) System for protection against infrared and/or radar-guided threats, in particular for large flying objects
AU2010265108B2 (en) Active body
EP1637829B1 (en) Pack of heat-generating countermeasures
US7441503B1 (en) Expendable infra-red radiating means
US9067844B2 (en) Decoy countermeasures
JP2002540375A (en) Pyrotechnic smoke screen generating unit aerosol impermeable in the visible, infrared and millimeter wave range
GB2266944A (en) Flare arrangements
Bruce Expendable decoys
ZA200410264B (en) Smoke projectile
SE0901393A1 (en) A method for combating explosives-loaded weapons units and projectiles is therefore provided
CA2207451C (en) Expendable infra-red radiating means
KR20220071964A (en) Active elements and methods of igniting active elements
Ramamurthi Unanticipated Thermal Ignition Sources
Graswald et al. Novel insensitive precision guided bombs using TDWs low-cost scalable effects technology
ES2196929B1 (en) FUNGIBLE INFRARED RADIATION MEDIA.
Fulghum Lattice Fin Design Key to Small Bombs
CA2251975A1 (en) Munitions for mine clearance

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: 20050316

AK Designated contracting states

Kind code of ref document: A1

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

AX Request for extension of the european patent

Extension state: AL HR LT LV MK

AKX Designation fees paid

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

17Q First examination report despatched

Effective date: 20071127

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

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

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

Free format text: STATUS: EXAMINATION IS IN PROGRESS

INTG Intention to grant announced

Effective date: 20161110

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: 20161216

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

AK Designated contracting states

Kind code of ref document: B1

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

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 897882

Country of ref document: AT

Kind code of ref document: T

Effective date: 20170615

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602004051323

Country of ref document: DE

REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

Effective date: 20170821

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 14

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20170531

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 897882

Country of ref document: AT

Kind code of ref document: T

Effective date: 20170531

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2638241

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20171019

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

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: 20170531

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: 20170901

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: 20170531

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: 20170531

Ref country code: SE

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: 20170531

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: 20170831

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: 20170531

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: 20170531

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: 20170531

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: 20170531

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

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: 20170531

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602004051323

Country of ref document: DE

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

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

26N No opposition filed

Effective date: 20180301

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: 20170531

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: 20170531

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20170930

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: 20170915

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

Ref country code: CH

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

Effective date: 20170930

Ref country code: LI

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

Effective date: 20170930

Ref country code: IE

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

Effective date: 20170915

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

Ref country code: BE

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

Effective date: 20170930

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 15

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: 20040915

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 NON-PAYMENT OF DUE FEES

Effective date: 20170531

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: 20170531

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: 20170531

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

Ref country code: FR

Payment date: 20200918

Year of fee payment: 17

Ref country code: DE

Payment date: 20200922

Year of fee payment: 17

Ref country code: DK

Payment date: 20200916

Year of fee payment: 17

Ref country code: GB

Payment date: 20200921

Year of fee payment: 17

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

Ref country code: ES

Payment date: 20201001

Year of fee payment: 17

Ref country code: IT

Payment date: 20200924

Year of fee payment: 17

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602004051323

Country of ref document: DE

REG Reference to a national code

Ref country code: DK

Ref legal event code: EBP

Effective date: 20210930

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20210915

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: 20210915

Ref country code: FR

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

Effective date: 20210930

Ref country code: DE

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

Effective date: 20220401

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20221028

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: 20210915

Ref country code: DK

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

Effective date: 20210930

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 NON-PAYMENT OF DUE FEES

Effective date: 20210916