EP1651389A1 - Outil composite pour des contraintes de percusion et/ou d'abrasion - Google Patents

Outil composite pour des contraintes de percusion et/ou d'abrasion

Info

Publication number
EP1651389A1
EP1651389A1 EP04763716A EP04763716A EP1651389A1 EP 1651389 A1 EP1651389 A1 EP 1651389A1 EP 04763716 A EP04763716 A EP 04763716A EP 04763716 A EP04763716 A EP 04763716A EP 1651389 A1 EP1651389 A1 EP 1651389A1
Authority
EP
European Patent Office
Prior art keywords
composite tool
tool according
base
base body
molded body
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
Application number
EP04763716A
Other languages
German (de)
English (en)
Other versions
EP1651389B1 (fr
Inventor
Bruno Mayer
Stephan O. Mayer
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.)
Stahlwerke Bochum GmbH
Original Assignee
Stahlwerke Bochum GmbH
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 Stahlwerke Bochum GmbH filed Critical Stahlwerke Bochum GmbH
Publication of EP1651389A1 publication Critical patent/EP1651389A1/fr
Application granted granted Critical
Publication of EP1651389B1 publication Critical patent/EP1651389B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25DPERCUSSIVE TOOLS
    • B25D17/00Details of, or accessories for, portable power-driven percussive tools
    • B25D17/02Percussive tool bits
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/06Casting in, on, or around objects which form part of the product for manufacturing or repairing tools
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25DPERCUSSIVE TOOLS
    • B25D2222/00Materials of the tool or the workpiece
    • B25D2222/21Metals
    • B25D2222/42Steel

Definitions

  • the invention relates to a composite tool for impact loads.
  • Such tools are used, for example, to shred metal, rock or demolition materials.
  • the tools are exposed to extreme loads both in the area of their surfaces that come into direct contact with the material to be shredded and in the area in which they are held in the respective shredding machine.
  • a disadvantage of the simple monoblock tools explained above is that they have a consistently low base hardness or are made from impact-hardening materials. As a rule, they show insufficient wear resistance. With highly or differentiated, over several sections differently hardened monoblock tools, on the other hand, often run the risk of breaking in zones that are particularly hard and, with it, have low ductility.
  • Tools for impact loads which are produced by composite casting are also known.
  • the lock-resistant molded body is generally held in the material of the base body by a material connection.
  • a disadvantage of these tools is the high cost of their manufacture, which results from the high cost of materials and complex process control.
  • Tools of this type are known for example from DE-PS 592 580.
  • the invention proposes a composite tool for impact loads that comprises a base body produced from a highly ductile, impact-hardening iron-based alloy and at least one base body cast into the base body, largely excluding one Has cohesive connection form-fitting molded body which is arranged in the area of the composite tool directly exposed to the impact load and is prefabricated as a solid body from a highly wear-resistant metal material which differs from the iron material of the base body.
  • the tool according to the invention essentially consists of a base body which is produced from a cast, highly ductile material.
  • a shaped body is placed in the zone of this base body, which is impacted and / or abrasively during operation, and is made of a high-strength, also metallic, preferably iron-based alloy.
  • the shape of the shaped body is selected so that the shaped body is securely held in a form-fitting manner in the material of the base body surrounding it.
  • the materials of the base body and molded body are matched to one another in such a way that there is no significant material connection between the molded body and the base body. It is also not provided according to the invention that the shaped body is replaced by additional mechanically acting 'resource is held in the base body.
  • the invention provides a tool which can be used universally in comminution machines and is particularly easy to produce, which has a high wear resistance in its working zone exposed to primary wear due to the molded body arranged there and at the same time has a significantly reduced sensitivity to breakage. Since the high impact or abrasive loads are absorbed by the molded body made of hard, wear-resistant material, the base body material and the heat treatments used in its processing can be designed for the highest possible ductility of the base body regardless of the loads occurring in practical operation.
  • the heat treatment used in the production of composite tools according to the invention provides that the heat control during the manufacturing process takes into account the necessary parameters for the two materials to be combined.
  • the aim is to produce the highest possible ductility in the base body and the highest possible hardness in the molded body. This is achieved by treatment in the high temperature range of 950 - 1100 ° C. This is followed by broken liquid hardening in the range of 350 - 600 ° C, which is then followed by cooling in air and subsequent relaxation at temperatures of 300 - 400 ° C.
  • the molded body can be prefabricated in any inexpensive manner. This can be the case with the molded body cast into the tool according to the invention for example, a forged part, a stamped part, a cut part, a fired part, a sintered part or a casting.
  • the stamped part, burned or cut part can be made from a flat material.
  • the selection of the materials used for the base body and the molded body ensures that the specific mechanical-technological properties of both materials, namely on the one hand highly wear-resistant for the molded body and on the other hand highly ductile for the base body, are retained both during the manufacturing process itself and in practical use.
  • An iron alloy that (in% by weight) 8.0 - 22.0% Mn, 0.2 - 2.8% Cr, 0.5 has proven to be a suitable material for the production of the base body, which fulfills these requirements - 1.5% C and the rest contains Fe and unavoidable impurities.
  • an iron alloy that enables a high hardness of the molded body contains (in% by weight) 6.0-16.0% Cr, 0.3-1.5% Mo, 0.3-1.4% W, 0.6 - 2.2% C and the balance Fe and unavoidable impurities. Supported by a heat treatment tailored to the respective material compositions, these alloys can be used to produce particularly long-lasting, robust tools that can withstand even the toughest loads over the required service life. ' The materials of the base body and molded body can be matched to one another within the alloy specified according to the invention in such a way that the molded body is permanently clamped in the tool during and as a result of the use stress.
  • the invention is characterized in that in the area in which the iron material of the base material laterally surrounds the molded body, the ratio of the average thickness of the base material measured in a first axis to the average thickness of the cast molded body measured in the same axis is 0.2 to 1.0 If this range of strength ratios is taken into account, a high level of security against breakage is guaranteed, even with strongly changing loads in the area of the clamping and storage zone of the tool.
  • a tool according to the invention is deliberately produced in such a way that there is no substantial metallic bond between the molded body and the base body at least partially surrounding it.
  • the molded body is rather designed such that the molded body is embedded in a form-fitting manner in the material of the base body.
  • the molded body can have a shape tapering from a base surface in the direction of its end surfaces opposite the base surface and the end surface can be assigned to the area of the composite tool that is directly exposed to the impact.
  • Such a shape is given, for example, when the shaped body has the basic shape of a truncated pyramid. In the case of such a shape tapering essentially conically from the base to the end face, it is ensured in a simple manner that the molded body is held securely in the base body even after a long operating time.
  • the form-fitting hold of the shaped body can also be achieved in that depressions are formed in the side surfaces of the shaped body. Alternatively or in addition, elevations can be formed on the side surfaces of the shaped body.
  • the composite tools 1, 11, 21, 31 shown in FIG. 1 each have a cuboid-shaped base body 2, which is cast from a highly ductile iron material. Starting from its one narrow end face 2a, the base body 2 is in a working section 2b, which in practical use is exposed to direct contact with the material to be shredded and extends over about a third of the total length L of the base body 2, a clamping section adjoining the working section 2b 2c, on which, when the composite tool 1, 11, 21, 31 is mounted, the clamping device (not shown) of a comminution machine, also not shown, engages and divides a bearing section 2d adjoining the clamping section 2c, on which the tool 1 in the assembled position in the comminution machine is supported.
  • a molded body 3 made of a high-strength, hard iron material is cast into the working section of the base body 1.
  • the molded body 3 has a hexagonal base surface 3a with two opposing long sides, which are connected at their ends by two short sides meeting at an obtuse angle that is open towards the inner surface. Based on that shaped base 3a, the molded body 3 tapers in the direction of the end face 2a of the base body 2.
  • a shape of the molded body 3 that tapers conically starting from the base surface 3a in the direction of the end surface 3b of the molded body 3 assigned to the end surface 2a of the base body 2 is formed.
  • the shaped body 3 shaped in this way is completely surrounded laterally in the new state of the tool 1 and in the area of its base 3a by the material of the base body 2.
  • the mean thickness d G ⁇ of the wall 2f of the base body 2, which extends parallel to the end face 2a in the direction of the wider side faces of the base body 2 and is oriented perpendicularly to the measurement body X, is selected such that the The ratio of the average thickness d G ⁇ to the average thickness d F ⁇ of the shaped body 3 measured in the same measuring axis X is approximately 0.3.
  • the thickness d G2 of the wall 2e of the base body 2 which is laterally surrounding the shaped body 3 in the width direction and measured in a measuring axis Y oriented transversely to the measuring axis X, is selected such that the ratio of the average thickness d G2 to the average thickness measured in the same measuring axis Y d F2 of the shaped body 3 is approximately 0.2.
  • a molded body 13 made from a high-hard iron material.
  • the material of the base body 2 completely surrounds the molded body 2 when the tool 11 is new.
  • the molded body 13 of the tool 11 has a tapering shape, starting from its base 13a in the direction of its front side 13b assigned to the front side 2a of the base body 2.
  • the base surface 13a and, accordingly, the end face 13b of the molded body are also hexagonal, the surfaces 13a, 13b in this case being delimited by two short, mutually opposite sides, each of which is opened by a blunt one to the respective surface 13a, 13b Longer sides that meet at angles are connected to one another.
  • the essentially conical shape of the solid molded body 13, which tapers from the base surface 13a and the embedding of the molded body 13 in the material of the base body 12 ensures that the molded body 13 is still securely in the base body even after a long period of operation 2 held and is able to absorb the striking load directly striking the tool 11 just as securely.
  • the working section 2b of the base body 2 is in turn off cast a solid metal material produced, solidly formed molded body 23.
  • the material of the base body 2 completely surrounds the molded body 23 when new.
  • the molded body 23 has a truncated pyramid-shaped basic shape, which has four side surfaces 23c, 23d, 23e, 23f, the base surface 23a of which is larger than its end surface 23b assigned to the end surface 2a of the base body 2.
  • channel-like depressions 23g are formed at regular intervals and extending over the length of the molded body 23, while knob-like projections 23h are formed on the two other opposite side surfaces 23e, 23f in an irregular arrangement.
  • the depressions 23g and the projections 23h in combination with the shape of the shaped body 23 tapering starting from the base area 23a in the direction of the end face 23b, support its secure, form-fitting hold in the material of the base body 2.
  • the composition of the iron material of the base body 2 is so matched to the composition of the iron material from which the molded body 23 is made, that the molded body 23 is additionally non-positively held in the base body 2 under tension after the completion of the composite tool 21 due to the different thermal expansion behavior of the two materials.
  • three molded bodies 33 ', 33''and33''' are cast in.
  • the shaped bodies 33 ', 33'',33''' are each formed in the shape of a truncated pyramid and run from their rectangular base surface 33a in Direction of the end face 2a of the base body 2 of the tool 31 assigned and in the new state flush with this aligned end face 33b.
  • the length of the shaped body 33 '' arranged between the two outer shaped bodies 33 ', 33''' is approximately . half the length of the other two shaped bodies 33 'and 33'''.
  • the shaped bodies 33 ', 33''and33''' are arranged at a distance that both the ratio of the average thickness d Gi measured in the direction of the measuring axis X of the shaped bodies 33 ', 33''and33''' in each case in the thickness direction of the material of the base body 2 to the mean thickness d F ⁇ of the shaped bodies 33 ', 33'',33''' measured in the same measuring axis X and the ratio of the mean thickness d G2 measured in the direction of the measuring axis Y of the shaped bodies 33 ', 33''and33''' in the width direction of the material of the base body 2 in relation to the average thickness d F2 of the shaped bodies 33 ', 33'',33''' measured in the same measuring axis Y in the range from 0.2 to 1 , 0 lies.
  • this allows the wall thicknesses d G ⁇ bz to be matched to the thickness d F ⁇ , d F ⁇ of the shaped body 33 ', 33'',33''' , ' d G2 ensures that the molded bodies 33', 33 '', 33 '''are held in the ductile iron material of the base body 2 in the tool 31 in a manner which is sufficiently elastic for a permanently secure hold, even under the hard loads occurring in practical use ,
  • An important advantage of the composite tool 31 shown in FIG. 4 is that with the introduction of several harder shaped bodies 33 ', 33'',33''' into the highly ductile base body 2 by the between the individual shaped bodies 33 ', 33'',33''' existing ductile base material, the risk of breakage in practical use is significantly minimized.
  • the different length of the Shaped body 33 ', 33'',33''' takes into account the limitation of the desired increased wear resistance to zones of the main wear stress.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Earth Drilling (AREA)
  • Polishing Bodies And Polishing Tools (AREA)
  • Laminated Bodies (AREA)
  • Percussive Tools And Related Accessories (AREA)
  • Forging (AREA)
EP04763716A 2003-08-07 2004-08-02 Outil composite pour des contraintes de percusion et/ou d'abrasion Not-in-force EP1651389B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10336169A DE10336169B4 (de) 2003-08-07 2003-08-07 Komposit-Werkzeug für schlagende und/oder abrasive Belastungen
PCT/EP2004/008648 WO2005014238A1 (fr) 2003-08-07 2004-08-02 Outil composite pour des contraintes de percusion et/ou d'abrasion

Publications (2)

Publication Number Publication Date
EP1651389A1 true EP1651389A1 (fr) 2006-05-03
EP1651389B1 EP1651389B1 (fr) 2010-12-29

Family

ID=34129501

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04763716A Not-in-force EP1651389B1 (fr) 2003-08-07 2004-08-02 Outil composite pour des contraintes de percusion et/ou d'abrasion

Country Status (6)

Country Link
EP (1) EP1651389B1 (fr)
AT (1) ATE493233T1 (fr)
DE (3) DE20321302U1 (fr)
DK (1) DK1651389T3 (fr)
ES (1) ES2358594T3 (fr)
WO (1) WO2005014238A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8651407B2 (en) 2008-09-19 2014-02-18 Magotteaux International S.A. Composite impactor for impact crusher

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4155031A1 (fr) * 2021-09-23 2023-03-29 Sandvik Mining and Construction Oy Outil de rupture, marteau de rupture et procédé de maintien de la forme de l'outil de rupture

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE592580C (de) * 1934-02-10 Walter Huelsbruch Dr Ing Spitzeisen oder Meissel, vornehmlich fuer den Bergbau
GB643790A (en) * 1947-10-27 1950-09-27 Rip Bits Ltd Improvements in or relating to drill-bits or drill-steels having hard metal tips suitable for rock drilling
DE1133089B (de) * 1954-12-07 1962-07-12 Georg Hufnagel Fa Verfahren zum Herstellen von Werkzeugen fuer die spanabhebende Bearbeitung durch Umgiessen gesinterter Koerper, insbesondere Hartmetallkoerper
AT319149B (de) * 1972-11-24 1974-12-10 Boehler & Co Ag Geb Baggereimer
DE2829847C2 (de) * 1978-07-07 1983-05-05 Edelstahl GmbH & Co KG Techn. Beratung-Entwicklung-Verkauf, 4000 Düsseldorf Stahlmeißel
US4314616A (en) * 1980-01-28 1982-02-09 Acme-Cleveland Corporation Die-cast masonry drill with leading hard insert
DE3347501C3 (de) * 1983-12-29 1993-12-02 Uwe Christian Seefluth Bohrwerkzeug mit Hartmetalleinsatzkörper, Herstellverfahren für Hartmetalleinsatzkörper
GB2167438B (en) * 1984-10-17 1988-11-23 Bradley & Foster Ltd A method of heat treating high chromium cast ferrous-based alloys and a wearing element formed of a high chromium cast ferrous based alloy
US5238046A (en) 1990-09-20 1993-08-24 Magotteaux International Method of manufacturing a bimetal casting and wearing part produced by this method
US6216805B1 (en) * 1999-07-12 2001-04-17 Baker Hughes Incorporated Dual grade carbide substrate for earth-boring drill bit cutting elements, drill bits so equipped, and methods
US6799648B2 (en) * 2002-08-27 2004-10-05 Applied Process, Inc. Method of producing downhole drill bits with integral carbide studs

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2005014238A1 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8651407B2 (en) 2008-09-19 2014-02-18 Magotteaux International S.A. Composite impactor for impact crusher

Also Published As

Publication number Publication date
ATE493233T1 (de) 2011-01-15
EP1651389B1 (fr) 2010-12-29
DE20321302U1 (de) 2006-09-14
ES2358594T3 (es) 2011-05-12
DK1651389T3 (da) 2011-03-28
DE502004012067D1 (de) 2011-02-10
DE10336169B4 (de) 2006-11-09
DE10336169A1 (de) 2005-03-10
WO2005014238A1 (fr) 2005-02-17

Similar Documents

Publication Publication Date Title
DE3605520A1 (de) Einstueckig geformter hammer mit getrennten kopf- und handgriffkernkoerpern
DE102019204836B3 (de) Exzenterwalzenbrechbackensatz und Exzenterwalzenbrechanlage umfassend einen solchen Brechbackensatz
EP0841990B1 (fr) Piece d'usure et son procede de fabrication
EP2662168A1 (fr) Lame de scie avec élément de coupe fabriqué en métallurgie des poudres
DE102006017263A1 (de) Kurbelwelle und Verfahren zu deren Herstellung
EP0751234B1 (fr) Lame de scie comme scie circulaire, scies à cadre, meules tronçonneuses et de dispositifs de coupage ou de raclage
DE19757271A1 (de) Werkzeug
DE102010031313A1 (de) Meisselwerkzeug, Verfahren zur Herstellung eines Meisselwerkzeugsystems und Handwerkzeugmaschine
DE2335588B2 (de) Verfahren zum herstellen metallischer verbundgusstuecke
WO2005014238A1 (fr) Outil composite pour des contraintes de percusion et/ou d'abrasion
DE69813920T3 (de) Hochfester nicht-thermischer Frischstahl für Warmschmieden
DE10257270A1 (de) Rotor und Schweissverfahren für ein Rotorelement
EP2319625A1 (fr) Moulin à courant de Foucault et outil de broyage correspondant
DE19600883C1 (de) Vorrichtung zum Zerkleinern von festen Massen
DE19754291B4 (de) Verschleißschutz-Segment sowie verschleißgeschütztes Maschinenteil mit einer Vielzahl derartiger Segmente
EP4334053A1 (fr) Procédé de production d'un matériau de carbure cémenté ayant une phase liante renforcée
WO2022233491A1 (fr) Procédé de fabrication d'un corps en carbure métallique
DE102021128592A1 (de) Verfahren zur Herstellung eines Sinterkarbid-Körpers
EP3852931B1 (fr) Capuchon protecteur et rotor pour un dispositif de broyage pour pièces métalliques et matières de pierre en étant équipé
EP3781319B1 (fr) Outil de percussion et rotor équipé de celui-ci destiné à une machine pour fragmenter des objets métalliques ou des matériaux pierreux
AT409599B (de) Verbundkörper
WO2004020681A1 (fr) Utilisation d'un alliage de métaux durs
DE202018103096U1 (de) Verschleißfeste Auskleidungs- oder Stempelplatte für Pressvorrichtungen zum Verdichten von Reststoffen und Pressvorrichtung mit einer derartigen Platte
DE112023000190T5 (de) Ausscheidungshärtender weichmagnetischer ferritischer Edelstahl mit hervorragender Zerspanbarkeit
DE19719310C1 (de) Schlagleiste

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: 20060201

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

DAX Request for extension of the european patent (deleted)
17Q First examination report despatched

Effective date: 20080916

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 HU IE IT LI LU MC NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REF Corresponds to:

Ref document number: 502004012067

Country of ref document: DE

Date of ref document: 20110210

Kind code of ref document: P

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502004012067

Country of ref document: DE

Effective date: 20110210

REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

REG Reference to a national code

Ref country code: NL

Ref legal event code: T3

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2358594

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20110429

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

Ref country code: SI

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

Effective date: 20101229

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: 20101229

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: 20101229

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: 20101229

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: 20110329

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

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

Ref country code: 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: 20110429

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: 20101229

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: 20110330

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: 20101229

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: 20101229

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: 20101229

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: 20101229

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

Ref country code: IE

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

Effective date: 20101229

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: 20110930

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502004012067

Country of ref document: DE

Effective date: 20110930

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: 20110831

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Ref country code: CH

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

Effective date: 20110831

Ref country code: LI

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

Effective date: 20110831

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: 20110802

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: 20101229

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

Ref country code: HU

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

Effective date: 20101229

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 13

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

Ref country code: NL

Payment date: 20160824

Year of fee payment: 13

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

Ref country code: IT

Payment date: 20160825

Year of fee payment: 13

Ref country code: GB

Payment date: 20160824

Year of fee payment: 13

Ref country code: DK

Payment date: 20160823

Year of fee payment: 13

Ref country code: DE

Payment date: 20160824

Year of fee payment: 13

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

Ref country code: AT

Payment date: 20160825

Year of fee payment: 13

Ref country code: FR

Payment date: 20160829

Year of fee payment: 13

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

Ref country code: BE

Payment date: 20160830

Year of fee payment: 13

Ref country code: ES

Payment date: 20160825

Year of fee payment: 13

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502004012067

Country of ref document: DE

REG Reference to a national code

Ref country code: DK

Ref legal event code: EBP

Effective date: 20170831

REG Reference to a national code

Ref country code: NL

Ref legal event code: MM

Effective date: 20170901

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 493233

Country of ref document: AT

Kind code of ref document: T

Effective date: 20170802

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

Effective date: 20170802

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20180430

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 NON-PAYMENT OF DUE FEES

Effective date: 20170802

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20170831

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 NON-PAYMENT OF DUE FEES

Effective date: 20170901

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: 20180301

Ref country code: DK

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

Effective date: 20170831

Ref country code: GB

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

Effective date: 20170802

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: 20170831

Ref country code: IT

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

Effective date: 20170802

Ref country code: FR

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

Effective date: 20170831

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20181030

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: 20170803