EP3921113A1 - Verfahren zur trennung eines ersten mechanischen teils von einem zweiten mechanischen teil - Google Patents

Verfahren zur trennung eines ersten mechanischen teils von einem zweiten mechanischen teil

Info

Publication number
EP3921113A1
EP3921113A1 EP20709268.5A EP20709268A EP3921113A1 EP 3921113 A1 EP3921113 A1 EP 3921113A1 EP 20709268 A EP20709268 A EP 20709268A EP 3921113 A1 EP3921113 A1 EP 3921113A1
Authority
EP
European Patent Office
Prior art keywords
mechanical part
mechanical
blade
reinforcement
cooling
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.)
Pending
Application number
EP20709268.5A
Other languages
English (en)
French (fr)
Inventor
Vincent Joudon
Damien Bruno LAMOUCHE
Matthieu Patrick Jean Roger Perlin
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.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Publication of EP3921113A1 publication Critical patent/EP3921113A1/de
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • B23P19/04Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J5/00Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00Restoring or reconditioning objects
    • B23P6/002Repairing turbine components, e.g. moving or stationary blades, rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24CABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C1/00Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods
    • B24C1/10Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods for compacting surfaces, e.g. shot-peening
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24CABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C5/00Devices or accessories for generating abrasive blasts
    • B24C5/005Vibratory devices, e.g. for generating abrasive blasts by ultrasonic vibrations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26FPERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
    • B26F3/00Severing by means other than cutting; Apparatus therefor
    • B26F3/06Severing by using heat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/205Constructional features for protecting blades, e.g. coating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/26Fabricated blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40Maintaining or repairing aircraft
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/005Repairing methods or devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/147Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2603/00Vanes, blades, propellers, rotors with blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B43/00Operations specially adapted for layered products and not otherwise provided for, e.g. repairing; Apparatus therefor
    • B32B43/006Delaminating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • B64C2027/4733Rotor blades substantially made from particular materials
    • B64C2027/4736Rotor blades substantially made from particular materials from composite materials
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2301/00Additional features of adhesives in the form of films or foils
    • C09J2301/50Additional features of adhesives in the form of films or foils characterized by process specific features
    • C09J2301/502Additional features of adhesives in the form of films or foils characterized by process specific features process for debonding adherents
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324Blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/10Manufacture by removing material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/50Intrinsic material properties or characteristics
    • F05D2300/502Thermal properties
    • F05D2300/5024Heat conductivity
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

Definitions

  • the cooling unit 38 comprises a reservoir 42 of pressurized cooling fluid and a pressure reducing valve 44 capable of receiving the fluid coming from the reservoir 42 and of delivering it under a determined pressure.
  • This pressure reducer is connected to a conduit 46, supplied with pressurized cooling fluid, which extends close to the reinforcement 14.
  • the end of the conduit 46 comprises a nozzle 48 which is configured to spray the cooling fluid onto the surface of the valve. reinforcement 14.
  • Liquid nitrogen is sprayed at a temperature of -200 ° C.
  • the adhesive film 16 is cooled by thermal conduction through the reinforcement 14.
  • the nitrogen application time therefore depends on the thickness and the nature of the metal reinforcement 14, as well as on the desired temperature in the adhesive film 16 to cause it to break.
  • the second part that is to say the reinforcement 14 is subjected to a compressive stress in a direction D substantially perpendicular to a surface of the adhesive film 16. .
  • This compressive stress is a mechanical stress corresponding to a shock exerted on the surface of the metal reinforcement 14.
  • This compression wave has the advantage of being transformed into a tensile wave at the interface between the reinforcement 14 and the adhesive film 16 of the makes the difference in mechanical impedance between the reinforcement 14 and the adhesive film 16.
  • the change in mechanical rigidity at the interface between two materials induces the reflection of part of the incident wave compression into a tensile wave.
  • These components comprise a generator 50, converting a source of electrical energy supplying the generator into a sinusoidal electrical signal. This signal feeds a converter 52, which converts the sinusoidal electrical signal into sinusoidal vibrating waves. These vibratory waves are transmitted to an amplifier 54, which amplifies them. The amplifier 54 amplifies the vibratory waves intended for a sonotrode 56 which is able to mechanically transmit the vibratory waves. At one end of the sonotrode 56 is at least one transmission finger 58, also called an "indenter”, which receives the vibratory waves from the sonotrode 56, which is arranged in contact with the reinforcement 14 of the second part, and which is suitable for them. mechanically transmit to the reinforcement 14.
  • the transmission finger or fingers 58 of the sonotrode 58 exert the mechanical stress by hammering by ultrasound, as we have seen, substantially in the direction D substantially perpendicular to a surface of the adhesive film 16 ..
  • the assembly 32 of the tooling 30 enables the two stages of cooling and stressing to be carried out simultaneously. These two operations are carried out in a coverage zone C of the leading edge 20 of the blade 12 by the tooling 30, and more particularly by the fingers 58 of the sonotrode 56 immediately after passage of the nozzle 48.
  • the zone C is of a length I less than the length L of the leading edge 14 of the vane 12.
  • the tool 40 is therefore moved along the entire length L of the leading edge 14 of the vane 12, as illustrated FIGS. 3 and 4.
  • the coverage area C first undergoes cooling by the nozzle 48 and then immediately after the mechanical stress by the transmission fingers 58.
  • the immediate proximity of the fingers 58 to the nozzle 48 prevents the leading edge 20 from heating up and the cooling from losing its effectiveness.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Forests & Forestry (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Organic Chemistry (AREA)
  • Architecture (AREA)
  • Transportation (AREA)
  • Manufacturing & Machinery (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Automatic Assembly (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
  • Laminated Bodies (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)
EP20709268.5A 2019-02-04 2020-02-04 Verfahren zur trennung eines ersten mechanischen teils von einem zweiten mechanischen teil Pending EP3921113A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1901069A FR3092267B1 (fr) 2019-02-04 2019-02-04 Procédé de désolidarisation d'une première pièce mécanique d'une deuxième pièce mécanique
PCT/FR2020/050178 WO2020161426A1 (fr) 2019-02-04 2020-02-04 Procede de desolidarisation d'une premiere piece mecanique d'une deuxieme piece mecanique

Publications (1)

Publication Number Publication Date
EP3921113A1 true EP3921113A1 (de) 2021-12-15

Family

ID=67441235

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20709268.5A Pending EP3921113A1 (de) 2019-02-04 2020-02-04 Verfahren zur trennung eines ersten mechanischen teils von einem zweiten mechanischen teil

Country Status (8)

Country Link
US (1) US11731221B2 (de)
EP (1) EP3921113A1 (de)
JP (1) JP2022524292A (de)
CN (1) CN113474117B (de)
BR (1) BR112021015211A2 (de)
CA (1) CA3128288A1 (de)
FR (1) FR3092267B1 (de)
WO (1) WO2020161426A1 (de)

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9700819D0 (en) * 1997-01-16 1997-03-05 Gkn Westland Helicopters Ltd Method of and apparatus for removing a metallic component from attachmet to a helicopter blade
FR2787366B1 (fr) 1998-12-17 2001-02-16 Eurocopter France Procede et dispositif d'enlevement d'une plaque retenue par adhesif a une piece support
FR2791293B1 (fr) * 1999-03-23 2001-05-18 Sonats Soc Des Nouvelles Appli Dispositifs de traitement de surface par impacts
DE60105830T2 (de) * 2001-12-21 2006-03-09 Siemens Ag Verfahren zum Entfernen einer Metallschicht eines Schichtsystems
DE102008036713A1 (de) * 2008-08-07 2010-02-11 Technische Universität Carolo-Wilhelmina Zu Braunschweig Verfahren zum Trennen zweier über zumindest eine Klebschicht miteinander verklebter Objekte
US9409383B2 (en) * 2008-12-22 2016-08-09 Apple Inc. Layer-specific energy distribution delamination
FR2970197B1 (fr) 2011-01-11 2013-12-20 Snecma Procede de desolidarisation/solidarisation par induction d'une piece mecanique magnetique collee a une piece mecanique.
FR2989607B1 (fr) * 2012-04-19 2014-05-09 Snecma Procede de realisation d'un renfort metallique avec insert pour la protection d'un bord d'attaque en materiau composite
FR2992243B1 (fr) * 2012-06-20 2015-02-13 Snecma Procede de decollement par choc laser
FR2993896B1 (fr) * 2012-07-26 2014-08-22 Snecma Procede de collage et de decollement entre deux pieces utilisant un adhesif charge
KR102112905B1 (ko) * 2014-06-27 2020-05-19 에리히 탈너 제1 기판을 제거하기 위한 샘플 홀더, 장치 및 방법
FR3025735B1 (fr) * 2014-09-17 2016-12-09 Europe Tech Procede de traitement d'une piece composite
FR3043685B1 (fr) * 2015-11-13 2021-03-12 Snecma Procede de collage d'un film de protection sur une piece de forme complexe
US10138732B2 (en) * 2016-06-27 2018-11-27 United Technologies Corporation Blade shield removal and replacement
FR3056605B1 (fr) 2016-09-29 2020-12-18 Safran Aircraft Engines Dispositif de traitement chimique d'une piece de turbomachine munie d'un element de surface metallique
US20190061073A1 (en) * 2017-08-25 2019-02-28 United Technologies Corporation Separating adhesively bonded lap joints

Also Published As

Publication number Publication date
CN113474117B (zh) 2024-02-20
CA3128288A1 (en) 2020-08-13
CN113474117A (zh) 2021-10-01
US11731221B2 (en) 2023-08-22
FR3092267A1 (fr) 2020-08-07
JP2022524292A (ja) 2022-05-02
US20220143766A1 (en) 2022-05-12
WO2020161426A1 (fr) 2020-08-13
BR112021015211A2 (pt) 2021-09-28
FR3092267B1 (fr) 2021-04-09

Similar Documents

Publication Publication Date Title
EP3194724B1 (de) Verfahren zur behandlung eines verbundstoffteils
EP0445035B1 (de) Verfahren zum Reibschweissen
CA2537427C (fr) Procede de reparation de disque aubage monobloc, eprouvette de debut et de fin campagne
EP0574580B1 (de) Koaxiale duese zur laser-oberflaechenbehandlung mit zufuhr von pulverfoermigem material
EP2254729B1 (de) Verfahren zur herstellung einer hohlschaufel
EP2740905B1 (de) Splitter einer axialen turbomaschine, zugehoriger verdichter und axiale turbomaschine
EP1927426A1 (de) Verfahren zum Laserbohren eines Werkstücks aus einem Verbundwerkstoff mit einer keramischen Matrix
EP1101827A1 (de) Verfahren zum ultrasonischen Kugelstahlen von grossformatigen ringförmigen Oberflächen von dünnwandiger Werkstücke
EP2709793B1 (de) Laserdüse mit einem beweglichen element
EP1752234A1 (de) Metallteil behandelt durch Komprimierung seiner unteren Schichten sowie Verfahren zum Herstellen eines solchen Metallteils
FR2804180A1 (fr) Rampe commune d'alimentation pour moteur diesel
EP1961513A1 (de) Auftragsschweißverfahren eines Werkstücks in Aluminiumlegierung
EP3921113A1 (de) Verfahren zur trennung eines ersten mechanischen teils von einem zweiten mechanischen teil
FR2882534A1 (fr) Procede de decoupe simultanee de materiaux heterogenes et son dispositif de mise en oeuvre
FR2713349A1 (fr) Procédé et dispositif pour déposer un revêtement supérieur sur une préforme primaire de fibre optique.
CA2640219A1 (fr) Procede de retouche de pieces metalliques
CA2672390A1 (fr) Procede de montage d'une piece metallique dans une piece en materiau composite
FR2992243A1 (fr) Procede de decollement par choc laser
FR2964584A1 (fr) Dispositif et procede de frettage d'une piece anti-usure dans un trou localise dans un element de turboreacteur
FR2963749A1 (fr) Tete de soudage pour laser yag a double soufflage
RU2802946C2 (ru) Способ отделения первой механической детали от второй механической детали
FR2700583A1 (fr) Procédé de fabrication d'une paroi refroidie par fluide formée de petits tubes assemblés.
WO2023061957A1 (fr) Sonde à ultrasons pour inspection d'un composant à une température supérieure à 150°c et procédé d'inspection associé
FR2996477A1 (fr) Procede de fabrication d'une piece couverte d'un revetement abradable
FR2952158A1 (fr) Procede de realisation d'une liaision de profile creux et profile creux

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

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

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

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

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: 20210820

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

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)