EP3091095B1 - Superalliage à base de nickel sans rhénium à faible densité - Google Patents

Superalliage à base de nickel sans rhénium à faible densité Download PDF

Info

Publication number
EP3091095B1
EP3091095B1 EP15166317.6A EP15166317A EP3091095B1 EP 3091095 B1 EP3091095 B1 EP 3091095B1 EP 15166317 A EP15166317 A EP 15166317A EP 3091095 B1 EP3091095 B1 EP 3091095B1
Authority
EP
European Patent Office
Prior art keywords
nickel
nickel base
base alloy
rhenium
alloy according
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
EP15166317.6A
Other languages
German (de)
English (en)
Other versions
EP3091095A1 (fr
Inventor
Thomas GÖHLER
Ralf RETTIG
Robert F. Singer
Steffen Neumeier
Nils Ritter
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.)
MTU Aero Engines AG
Original Assignee
MTU Aero Engines AG
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 MTU Aero Engines AG filed Critical MTU Aero Engines AG
Priority to ES15166317.6T priority Critical patent/ES2682362T3/es
Priority to EP15166317.6A priority patent/EP3091095B1/fr
Priority to US15/142,068 priority patent/US20170058383A1/en
Publication of EP3091095A1 publication Critical patent/EP3091095A1/fr
Application granted granted Critical
Publication of EP3091095B1 publication Critical patent/EP3091095B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/057—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being less 10%
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/02—Making non-ferrous alloys by melting
    • C22C1/023—Alloys based on nickel
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon

Definitions

  • the present invention relates to a nickel-base alloy which is substantially free of rhenium but at the same time achieves the creep resistance properties of the second-generation nickel-based superalloys and has a reduced density compared to comparable alloys.
  • nickel-base superalloys are used for example as blade materials, since these materials still have sufficient strength for the high mechanical loads even at high operating temperatures.
  • turbine blades are exposed in stationary gas turbines or jet engines in commercial aircraft exhaust gas flow at temperatures of up to 1500 ° C and are subject to very high mechanical loads due to centrifugal forces. Under these conditions, it is particularly important that the creep resistance of the material used meets the requirements.
  • turbine blades In order to increase creep resistance, turbine blades have also been produced monocrystalline for several decades in order to further improve creep resistance by avoiding grain boundaries.
  • the alloys In the nickel-base superalloys of the so-called second and third generation currently in use, the alloys usually have the chemical element rhenium in a proportion of three or six percent by weight, since rhenium further improves the creep resistance.
  • the EP 2 725 110 A1 a nickel-based alloy which is substantially free of rhenium and has a solidus temperature of higher than 1320 ° C, wherein at temperatures of 1050 ° C to 1100 ° C excretions of a y 'phase in a ⁇ matrix in a proportion of 40 to 50 Vol .-% are present, the ⁇ / ⁇ 'mismatch at temperatures of 1050 ° C to 1100 ° C in the range of -0.15% to -0.25% and the tungsten content in the ⁇ -matrix is greater than in the excreted y'-phases.
  • the alloy has the following chemical composition: aluminum of 11 to 13 at.%, Cobalt of 4 to 14 at.%, Chromium of 6 to 12 at.%, Molybdenum of 0.1 to 2 at.%, Tantalum from 0.1 to 3.5 at .-%, titanium from 0.1 to 3.5 at .-%, tungsten from 0.1 to 3 at .-%, and the balance nickel and unavoidable impurities.
  • the alloy should have the lowest possible density and good solution heatability, be economical and efficient to produce and monocrystalline or directionally solidified and compared to the in EP 2 725 110 A1 Reinforced rhenium-free nickel-based alloy improved with comparable creep resistance Have properties, in particular a lower density, a lower proportion of Resteutikikum and improved Amsterdamsglühbarkeit.
  • a nickel-base alloy may have the following chemical composition: aluminum of 4.1 to 7.7 wt%, cobalt of 0 to 16.8 wt%, chromium of 6 to 11.8 wt% , Molybdenum from 3.6 to 11.3 wt%, tantalum from 0 to 3.9 wt%, titanium from 0 to 3.6 wt%, tungsten from 0 to 11.3 wt% , Carbon of 0 to 0.05 wt.%, Phosphorus of 0 to 0.015 wt.%, Copper of 0 to 0.05 wt.%, Zirconium of 0 to 0.015 wt.%, Silicon of 0 to 0 , 01% by weight, sulfur from 0 to 0.001% by weight, iron from 0 to 0.15% by weight, manganese from 0 to 0.05% by weight, boron from 0 to 0.003% by weight , Hafnium from 0 to 0.15 wt .
  • a nickel-based alloy according to the present invention may have the following chemical composition: aluminum of 4.7 to 5.7% by weight, cobalt of 2.6 to 13.6% by weight, chromium of 6.3 to 7.3% by weight, molybdenum from 3.7 to 4.7% by weight, tantalum from 0 to 0.5% by weight, titanium from 2.8 to 3.6% by weight, tungsten from 7.4 to 8.4 wt .-%, carbon from 0 to 0.05 wt .-%, phosphorus from 0 to 0.015 wt .-%, copper from 0 to 0.05 wt .-%, zirconium from 0 to 0.015% by weight, silicon from 0 to 0.01% by weight, sulfur from 0 to 0.001% by weight, iron from 0 to 0.15% by weight, manganese from 0 to 0.05% by weight. %, Boron from 0 to 0.003% by weight, hafnium from 0 to 0.15% by weight, yttrium from
  • a nickel-based alloy according to the present invention may have the following chemical composition: aluminum of 5.0 to 5.4 wt .-%, cobalt of 2.9 to 13.3 wt .-%, chromium of 6.6 to 7% by weight, molybdenum from 4 to 4.4% by weight, tantalum from 0 to 0.2% by weight, titanium from 3.1 to 3.5% by weight, tungsten from 7.7 to 8.1% by weight, carbon from 0 to 0.05% by weight, phosphorus from 0 to 0.015% by weight, copper from 0 to 0.05% by weight, zirconium from 0 to 0.015% by weight.
  • Silicon from 0 to 0.01% by weight, sulfur from 0 to 0.001% by weight, iron from 0 to 0.15% by weight, manganese from 0 to 0.05% by weight, boron from 0 to 0.003% by weight, hafnium from 0 to 0.15% by weight, yttrium from 0 to 0.002% by weight, as well as the balance nickel and unavoidable impurities.
  • a nickel-based alloy according to the present invention may have a cobalt content of less than 5% by weight, preferably less than 4% by weight. Since cobalt has a lower molar mass than nickel, a relatively low cobalt content has an advantageous effect on the overall density of the nickel-based alloy, and thus also on the total weight of the target component produced from this alloy.
  • the nickel-based alloy according to the invention may also have a cobalt content of greater than 11% by weight, preferably greater than 13% by weight.
  • a correspondingly high cobalt content has a positive effect on the segregation during solidification and the microstructural stability against the undesired formation of TCP phases.
  • the nickel-based alloy according to the present invention contains at least 67 at.%, In particular at least 68 at.%, Nickel.
  • the alloy elements are to be understood, the addition of which is not intended, but which can not be prevented for technical reasons or only with extremely great effort.
  • the following elements may still be present in the form of trace elements, the content of which is limited to the following ranges: bismuth from 0 to 0.00003% by weight, selenium from 0 to 0.0001% by weight, Thallium from 0 to 0.00005 wt%, lead from 0 to 0.0005 wt%, and tellurium from 0 to 0.0001 wt%.
  • alloy according to the invention in particular articles such as components of gas turbines, preferably turbine blades, and the like can be prepared, which may be monocrystalline or directionally solidified.
  • the attached figure shows a Larson-Miller plot to illustrate the creep resistance of the alloy according to the invention compared to known alloys.
  • alloy according to the invention was produced, the composition of which can be taken from the table below (alloy 1). Alloys 2 and 3 were chosen as comparison alloys, with the alloy 3 in the chemical composition essentially corresponding to that of the rhenium-containing material CMSX-4, and the alloy 2 corresponding to that in EP 2 725 110 A1 disclosed rhenium-free nickel base superalloy is. The components of the alloys are given in the table in weight percent (balance nickel and unavoidable impurities). Alloy no. al Co Cr Not a word re Ta Ti W 1 5.2 3.1 6.8 4.2 - - 3.3 7.9 2 4.8 8.6 5.0 1.4 - 10.1 1.3 8.8 3 5.6 9.0 6.5 0.6 3.0 6.5 1.0 6.0
  • the alloy 1 according to the invention was produced in a columnar crystal structure on a laboratory Bridgman casting installation in a three-bar geometry.
  • the rods had a diameter of 12 mm each and a length of 180 mm each and showed a typical dendritic microstructure with a dendrite spacing of about 230 ⁇ m.
  • the proportion of residual eutectic is very low at 2.8% (alloys 2 and 3 have a residual eutectic of 6.5% and 9.0%, respectively).
  • alloy 1 has a typical fully cubic y'-phase morphology.
  • Alloy 1 (L1) according to the present invention has a creep resistance substantially equal to that of rhenium-free alloy 2 (L2), the creep resistances of these alloys being similar to the creep resistance of Alloy 3 (L3) corresponds to a second generation nickel base superalloy. In comparison to the alloys 2 and 3, however, the alloy 1 in particular has a lower density. Analysis of the microstructure of the inventive alloy 1 after creep revealed no TCP phase formation.
  • nickel-based superalloys can be provided by the teachings of the present invention which can dispense with the hard-to-obtain element rhenium but nevertheless provide high temperature mechanical properties such as creep resistance, such as known rhenium containing alloys, and also have lower density than known rhenium-containing and rhenium-free alloys.
  • alloy 1 may undergo one or both of the following precipitation heat treatments after solution annealing: Excretion heat treatment 1: temperature heating rate hold time 1000 ° C 4 K / min 1050 ° C 1K / min 1050 ° C 1 h 20 ° C rapid cooling Excretion heat treatment 2: temperature heating rate hold time 840 ° C 4 K / min 870 ° C 1K / min 870 ° C 24 hours 20 ° C rapid cooling

Claims (12)

  1. Alliage à base de nickel à haute résistance au fluage, lequel ne contient pas de rhénium ou ne contient pas plus de 0,001 % en poids de rhénium et présente la composition chimique suivante :
    aluminium de 4,1 à 7,7 % en poids,
    cobalt de 0 à 16,8 % en poids,
    chrome de 6 à 11,8 % en poids,
    molybdène de 3,6 à 11,3 % en poids,
    tantale de 0 à 3,9 % en poids,
    titane de 0 à 3,6 % en poids,
    tungstène de 0 à 11,3 % en poids,
    carbone de 0 à 0,05 % en poids,
    phosphore de 0 à 0,015 % en poids,
    cuivre de 0 à 0,05 % en poids,
    zirconium de 0 à 0,015 % en poids,
    silicium de 0 à 0,01 % en poids,
    soufre de 0 à 0,001 % en poids,
    fer de 0 à 0,15 % en poids,
    manganèse de 0 à 0,05 % en poids,
    bore de 0 à 0,003 % en poids,
    hafnium de 0 à 0,15 % en poids,
    yttrium de 0 à 0,002 % en poids,
    le reste étant du nickel et des impuretés inévitables.
  2. Alliage à base de nickel selon la revendication 1,
    caractérisé en ce que
    l'alliage présente la composition chimique suivante :
    aluminium de 4,7 à 5,7 % en poids,
    cobalt de 2,6 à 13,6 % en poids,
    chrome de 6,3 à 7,3 % en poids,
    molybdène de 3,7 à 4,7 % en poids,
    tantale de 0 à 0,5 % en poids,
    titane de 2,8 à 3,6 % en poids,
    tungstène de 7,4 à 8,4 % en poids,
    carbone de 0 à 0,05 % en poids,
    phosphore de 0 à 0,015 % en poids,
    cuivre de 0 à 0,05 % en poids,
    zirconium de 0 à 0,015 % en poids,
    silicium de 0 à 0,01 % en poids,
    soufre de 0 à 0,001 % en poids,
    fer de 0 à 0,15 % en poids,
    manganèse de 0 à 0,05 % en poids,
    bore de 0 à 0,003 % en poids,
    hafnium de 0 à 0,15 % en poids,
    yttrium de 0 à 0,002 % en poids,
    le reste étant du nickel et des impuretés inévitables.
  3. Alliage à base de nickel selon la revendication 2,
    caractérisé en ce que
    l'alliage présente la composition chimique suivante :
    aluminium de 5,0 à 5,4 % en poids,
    cobalt de 2,9 à 13,3 % en poids,
    chrome de 6,6 à 7 % en poids,
    molybdène de 4 à 4,4 % en poids,
    tantale de 0 à 0,2 % en poids,
    titane de 3,1 à 3,5 % en poids,
    tungstène de 7,7 à 8,1 % en poids,
    carbone de 0 à 0,05 % en poids,
    phosphore de 0 à 0,015 % en poids,
    cuivre de 0 à 0,05 % en poids,
    zirconium de 0 à 0,015 % en poids,
    silicium de 0 à 0,01 % en poids,
    soufre de 0 à 0,001 % en poids,
    fer de 0 à 0,15 % en poids,
    manganèse de 0 à 0,05 % en poids,
    bore de 0 à 0,003 % en poids,
    hafnium de 0 à 0,15 % en poids,
    yttrium de 0 à 0,002 % en poids,
    le reste étant du nickel et des impuretés inévitables.
  4. Alliage à base de nickel selon l'une quelconque des revendications précédentes,
    caractérisé en ce que
    l'alliage présente une teneur en cobalt inférieure à 5 % en poids, de préférence inférieure à 4 % en poids.
  5. Alliage à base de nickel selon l'une quelconque des revendications 1 à 3,
    caractérisé en ce que
    l'alliage présente une teneur en cobalt supérieure à 11 % en poids, de préférence supérieure à 13 % en poids.
  6. Alliage à base de nickel selon l'une quelconque des revendications précédentes,
    caractérisé en ce
    qu'il présente une densité inférieure ou égale à 8,5 g/cm3, de préférence inférieure ou égale à 8,4 g/cm3.
  7. Alliage à base de nickel selon l'une quelconque des revendications précédentes,
    caractérisé en ce
    qu'il présente une température de solidus supérieure à 1320 °C.
  8. Alliage à base de nickel selon l'une quelconque des revendications précédentes,
    caractérisé en ce que
    qu'il comprend un eutectique résiduel inférieur ou égal à 4 %, de préférence inférieur ou égal à 3 %.
  9. Objet, fabriqué à partir d'un alliage à base de nickel selon l'une quelconque des revendications précédentes.
  10. Objet selon la revendication 9,
    caractérisé en ce que
    l'objet est monocristallin ou à solidification dirigée.
  11. Objet selon l'une quelconque des revendications 9 et 10,
    caractérisé en ce que
    l'objet est un composant d'une turbine à gaz fixe ou d'une turbine à gaz d'aéronef, en particulier une aube de turbine.
  12. Procédé de production d'un alliage à base de nickel,
    caractérisé en ce que
    le procédé comporte la combinaison et la fusion de métaux dans des rapports quantitatifs qui résultent en un alliage selon l'une quelconque des revendications 1 à 8.
EP15166317.6A 2015-05-05 2015-05-05 Superalliage à base de nickel sans rhénium à faible densité Not-in-force EP3091095B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
ES15166317.6T ES2682362T3 (es) 2015-05-05 2015-05-05 Superaleación a base de níquel exenta de renio con baja densidad
EP15166317.6A EP3091095B1 (fr) 2015-05-05 2015-05-05 Superalliage à base de nickel sans rhénium à faible densité
US15/142,068 US20170058383A1 (en) 2015-05-05 2016-04-29 Rhenium-free nickel base superalloy of low density

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP15166317.6A EP3091095B1 (fr) 2015-05-05 2015-05-05 Superalliage à base de nickel sans rhénium à faible densité

Publications (2)

Publication Number Publication Date
EP3091095A1 EP3091095A1 (fr) 2016-11-09
EP3091095B1 true EP3091095B1 (fr) 2018-07-11

Family

ID=53039792

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15166317.6A Not-in-force EP3091095B1 (fr) 2015-05-05 2015-05-05 Superalliage à base de nickel sans rhénium à faible densité

Country Status (3)

Country Link
US (1) US20170058383A1 (fr)
EP (1) EP3091095B1 (fr)
ES (1) ES2682362T3 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2554898B (en) 2016-10-12 2018-10-03 Univ Oxford Innovation Ltd A Nickel-based alloy
WO2020129282A1 (fr) * 2018-12-17 2020-06-25 日立金属株式会社 ALLIAGE TRÈS RÉSISTANT À LA CHALEUR À BASE DE Ni
CN112760525B (zh) * 2019-11-01 2022-06-03 利宝地工程有限公司 高γ′镍基超级合金、其用途及制造涡轮发动机构件的方法
CN111235434B (zh) * 2020-03-02 2021-07-30 北京钢研高纳科技股份有限公司 一种高温使用的镍基变形高温合金轮盘锻件的制备方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6054096A (en) 1982-12-27 2000-04-25 United Technologies Corporation Stable heat treatable nickel superalloy single crystal articles and compositions
EP0962542A1 (fr) 1998-05-01 1999-12-08 United Technologies Corporation Superalliage monocrystaline à base de nickel de traitement thermique et l'article
US20130230405A1 (en) 2007-08-31 2013-09-05 Kevin Swayne O'Hara Nickel base superalloy compositions being substantially free of rhenium and superalloy articles
US8876989B2 (en) 2007-08-31 2014-11-04 General Electric Company Low rhenium nickel base superalloy compositions and superalloy articles
US20100135846A1 (en) 2008-12-01 2010-06-03 United Technologies Corporation Lower cost high strength single crystal superalloys with reduced re and ru content
US8226886B2 (en) 2009-08-31 2012-07-24 General Electric Company Nickel-based superalloys and articles
US20110076182A1 (en) 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
US20110076181A1 (en) 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
US20110076180A1 (en) 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
EP2392684A1 (fr) 2010-06-02 2011-12-07 Siemens Aktiengesellschaft Alliage, couche de protection et composant
US20130129522A1 (en) 2011-11-17 2013-05-23 Kenneth Harris Rhenium-free single crystal superalloy for turbine blades and vane applications
ES2670877T3 (es) 2011-12-07 2018-06-01 Mtu Aero Engines Gmbh Superaleación a base de níquel exenta de renio o con contenido reducido de renio
EP2725110B1 (fr) 2012-10-26 2017-05-03 MTU Aero Engines GmbH Superalliage à base de nickel sans rhénium résistant au fluage

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
US20170058383A1 (en) 2017-03-02
ES2682362T3 (es) 2018-09-20
EP3091095A1 (fr) 2016-11-09

Similar Documents

Publication Publication Date Title
DE3023576C2 (fr)
EP2145967B1 (fr) Alliages d'aluminure de titane
EP1819838B1 (fr) Alliage a base d'aluminures de titane
EP3175008B1 (fr) Alliage a base de cobalt
EP2163656B1 (fr) Support d'enregistrement d'informations optiques, substrat et procédé de fabrication pour le support d'enregistrement d'informations optiques
DE3445996C2 (de) Einkristall-Gußwerkstück aus einer Nickelbasis-Legierung und Verfahren zu dessen Herstellung
DE102010037046A1 (de) Nickelbasissuperlegierungen und Artikel
DE2749080A1 (de) Einkristallsuperlegierungsgegenstand auf nickelbasis und verfahren zu seiner herstellung
DE3030962A1 (de) Ein- und polykristalline legierung auf nickel- oder kobalt-basis.
EP2402473B1 (fr) Procédé de fabrication d'un composant monocristallin constitué d'un superalliage à base de nickel
DE2223114B2 (de) Wärmebehandlungsverfahren für eine Legierung auf Nickel-Eisen-Basis
DE2445462B2 (de) Verwendung einer Nickellegierung
EP3091095B1 (fr) Superalliage à base de nickel sans rhénium à faible densité
EP2851445B1 (fr) Alliage TiAl résistant au fluage
EP3054023B1 (fr) Haute température alliage de ti-al riche en aluminium
DE2821524C2 (de) Verfahren zur Wärmebehandlung eines einkristallinen Körpers aus einer Nickel-Superlegierung
EP2354261B1 (fr) Superalliage à base de nickel ayant un comportement de dégradation amélioré
EP3133178B1 (fr) Superalliage a base de nickel optimise
DE112016003045T5 (de) Gussmaterial und Verfahren zur Herstellung eines Gussmaterials
EP2725110B1 (fr) Superalliage à base de nickel sans rhénium résistant au fluage
DE10100790C2 (de) Nickel-Basislegierung für die gießtechnische Herstellung einkristallin erstarrter Bauteile
DE2365045A1 (de) Durch ausscheidung verfestigte legierung
WO2012041276A2 (fr) Alliage tial résistant à la chaleur
DE2949158A1 (de) Waermebehandeltes nickelbasissuperlegierungserzeugnis, verfahren zum herstellen eines einkristallnickelbasissuperlegierungserzeugnisses sowie zwischenstufeneinkristallerzeugnis
DE2034607C3 (de) Verfahren zur Herstellung eines Gußstücks und Anwendung des Verfahrens

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: A1

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

AX Request for extension of the european patent

Extension state: BA ME

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20170503

RBV Designated contracting states (corrected)

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

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: 20180307

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

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1016947

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180715

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502015004987

Country of ref document: DE

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2682362

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20180920

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180711

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

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

Ref country code: 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: 20180711

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

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: 20180711

Ref country code: LT

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

Effective date: 20180711

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: 20180711

Ref country code: NO

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: 20181011

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: 20181012

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: 20181011

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: 20180711

Ref country code: RS

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

Effective date: 20180711

Ref country code: IS

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

Effective date: 20181111

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

Ref country code: HR

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

Effective date: 20180711

Ref country code: AL

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

Effective date: 20180711

Ref country code: LV

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

Effective date: 20180711

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502015004987

Country of ref document: DE

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: 20180711

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: 20180711

Ref country code: IT

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: 20180711

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: 20180711

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

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

Ref country code: DK

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

Effective date: 20180711

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: 20180711

Ref country code: SM

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

Effective date: 20180711

26N No opposition filed

Effective date: 20190412

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: 20180711

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: LI

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

Effective date: 20190531

Ref country code: CH

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

Effective date: 20190531

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: 20180711

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20190531

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: 20190505

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: 20180711

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

Ref country code: IE

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

Effective date: 20190505

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: 20190531

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: 20181111

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

Ref country code: ES

Payment date: 20200618

Year of fee payment: 6

Ref country code: DE

Payment date: 20200525

Year of fee payment: 6

Ref country code: FR

Payment date: 20200519

Year of fee payment: 6

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

Ref country code: GB

Payment date: 20200522

Year of fee payment: 6

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

Ref country code: CY

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

Effective date: 20180711

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 1016947

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200505

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: 20150505

Ref country code: MT

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

Effective date: 20180711

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: 20200505

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502015004987

Country of ref document: DE

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

Effective date: 20210505

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: 20210505

Ref country code: DE

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

Effective date: 20211201

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: 20210531

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

Ref country code: MK

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

Effective date: 20180711

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20220728

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: 20210506