EP2326740A1 - Dispositif et procédé de masquage d'une zone d'un élément - Google Patents

Dispositif et procédé de masquage d'une zone d'un élément

Info

Publication number
EP2326740A1
EP2326740A1 EP09776090A EP09776090A EP2326740A1 EP 2326740 A1 EP2326740 A1 EP 2326740A1 EP 09776090 A EP09776090 A EP 09776090A EP 09776090 A EP09776090 A EP 09776090A EP 2326740 A1 EP2326740 A1 EP 2326740A1
Authority
EP
European Patent Office
Prior art keywords
component
thermal spraying
masking
room temperature
zone
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.)
Withdrawn
Application number
EP09776090A
Other languages
German (de)
English (en)
Inventor
Andreas Jakimov
Manuel Hertter
Stefan Schneiderbanger
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 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 MTU Aero Engines GmbH filed Critical MTU Aero Engines GmbH
Publication of EP2326740A1 publication Critical patent/EP2326740A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/01—Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Definitions

  • the present invention relates to a device for masking a component zone of a component which is coated with a thermal spray coating.
  • the present invention relates to the masking and partial coating of components manufactured and used in the aerospace industry, such as gas turbines or aircraft engines.
  • the invention further relates to a method which uses the above-mentioned device for masking and partially coating component surfaces by thermal spraying, in particular components that are manufactured and used in the aerospace industry, such as gas turbines or aircraft engines.
  • Thermal spraying is a coating process in which a spray additive is continuously melted and spun onto a surface to be coated. Due to the accumulation of flattened and lamellar droplets, superimposed layers which form the so-called sprayed layer, which may be harder, more brittle and more porous than the starting material, are formed on the surface to be coated.
  • thermal spraying different spray methods are summarized, which differ in the type of spray additive, the production or the energy carrier such as arc spraying, laser spraying, flame spraying, high-velocity flame spraying or plasma spraying in a vacuum or under a controlled
  • the characteristic properties, such as the porosity, the structure of the structure, the density, the phase composition, the hardness, the modulus of elasticity and the residual stress of the layers formed by this process depend on many parameters, including thermal energy , the powder material used, the kinetic energy, the type of process gases, the substrate material to be coated and the pretreatment thereof.
  • thermal spraying is, on the one hand, that each material can both be sprayed and sprayed, that, with few exceptions, the materials to be coated remain thermally unchanged and, above all, that almost every component size and component geometry can be coated , Furthermore, good reproducibility, high quality standards and excellent automation of the coating process can be achieved with this method. Finally, several elements can be included or combined in the sprayed layers, so that the thermal spraying is characterized by a very flexible use.
  • thermal spraying processes are of great importance both in the manufacture of new parts and in the design, as well as in the repair of high-quality worn parts.
  • the fields of application and applications of thermal spraying are therefore diverse and range from decorative layers for household and kitchen appliances on emergency running and wear protective layers in automotive technology to Abst-, high-temperature protection and expedikorrektur füren in aerospace engineering.
  • the overlay mask consists of a multilayer cover film consisting of a metallic and a resin film, which is attached to large area uncoated parts.
  • Such support masks are not suitable for more complicated surfaces to be protected without additional conformance and mounting options and can not be reused as a rule.
  • No. 5,203,944 discloses, for example, the use of a plurality of masks for constructing a three-dimensional structure which consist of a plastic film which on the one hand comprises a removable carrier material and on the other hand an adhesive surface.
  • a disadvantage is that material deterioration of the adhesive tapes and adhesives occurs at higher temperatures.
  • masking consisting of adhesive tapes or reinforced adhesive tapes can be destroyed frequently and quickly in the course of the spraying process. They must therefore be removed frequently and replaced.
  • the adhesive residues left behind by the adhesive tapes or the like must be removed on the protected component surfaces by means of complicated cleaning processes, mechanical or chemical. This required surface treatment is associated with a high technical and time and therefore increased costs.
  • the chemicals used in the cleaning process are generally polluting and the risk of damaging the surfaces in a mechanical process is very high.
  • Another covering method known from the prior art provides for a masking of a lacquer or of a binder-containing mixture to be applied to the areas to be protected, as described, for example, in US Pat. No. 4,464,430.
  • the strongly adhering coating material must be removed from the masking or the masking itself. This is usually done by means of solvents that cause costly disposal measures and must be disposed of together with the resulting waste as hazardous waste.
  • Common masks are thus subject in thermal spraying either a high adhesion of the coating material and are therefore only temporarily dimensionally stable or they have a surface on which no coating material can adhere.
  • a cleaning of the masks used after the thermal spraying is usually possible, but associated with an intensive time and cost.
  • the unfavorable bouncing of the spray particles on the masking surface causes undesirable degradation of the film quality at the areas adjacent to the masking.
  • the object of the present invention is therefore to provide an apparatus and a method for masking of components to be thermally sprayed, in particular components for the aerospace industry, such as for gas turbines or aircraft engines, which avoids the disadvantages of the prior art , Furthermore, a solution is to be provided which enables a safe, fast, clean, reproducible and cost-effective partial coating of the components.
  • the device according to the invention for masking components to be thermally sprayed consists at least in part of a material which is elastically deformable at room temperature and is produced in a slight undersize in a form suitable for the partial regions of the component to be protected. Due to the at least partially possible elastic deformation of the device at room temperature, a simple, material-protecting, and tight fitting attachment of the device to the corresponding pre-sprayed to be protected components is guaranteed. Due to the at least partial elasticity and the slight undersize of the device, no fastening devices are needed, neither on the component nor on the device itself, to keep the device in the intended location.
  • the device according to the invention for masking components to be sprayed during the injection process has at least one inelastic surface on which the spray particles impinging on the device surface adhere and which are thereby prevented from entering the adjacent sprayed layers.
  • an undesirable deterioration of the quality of the adjacent to the device spray surfaces is prevented.
  • the device is finally easy, fast and residue-free by elastic deformation of the protected component surfaces can be separated. The risk of damaging the component surface is thereby ensured by the simple attachment of the device to the component and by the absence of a surface treatment of the protected component zones after the thermal spraying process.
  • the device is degraded undamaged by at least one thermal spraying process of the component to be protected and is used again in a new thermal spraying process.
  • a device consisting partly of one of the materials listed below and of a non-elastic part, for example one or more metal surfaces, which are held together and form the device for masking.
  • the device material consists of at least one of the following materials: silicone resin, thermally crosslinkable elastomers, thermosets, thermoplastics, natural rubber with additives, silicone elastomers, polyamide (PA), polycarbonate (PC), polymethylmethacrylate (PMMA) ), Polyoxymethylene (POM), polytetrafluoromethylene (PTFE), silicone polymers, vinyl-silicone polymers, polyesters, epoxy resin, quartz silica, dimethylvinyl, xylenes, polyethers, polyethylene, polyvinyl chloride (PVC), polystyrene (PS ), Polypropylene (PP), polysulfides. Ethylene-propylene rubber.
  • silicone elastomers can be easily created on a positive mold with appropriate undersize and simply use in the inventive way by a different choice of the impact surface material.
  • a plastic may be used which is elastic at low temperatures and at higher temperature to the 8O 0 C 5 as it is present during thermal spraying hardens.
  • the masking can be easily attached and removed, but is so inelastic by the curing during the injection process that it does not come to bounce off the impinging spray particles.
  • a reversible plastic which has the abovementioned properties but which reacts at low temperature, ie after cooling becomes elastic. This simplifies the removal and reuse of the mask and also facilitates the cleaning of the device.
  • the device is at least partially reinforced with metallic, glass or plastic fibers.
  • metallic fiber laid parallel to one another increases the stability of the device in that direction, but retains the elasticity perpendicular to that direction.
  • a cylindrical device for masking a part of a cylinder with embedded and non-elastic fibers along its longitudinal axis would, for example, be attached to this cylinder by radial elastic deformation.
  • At least a part of the surface of the device for masking is provided with an additional protective layer which promotes adherence of the spray particles during the thermal spraying process and which can be sprayed from the surface of the device by a suitable mechanical and / or detach chemical cleaning process.
  • This additional layer consists, for example, of a solvent-sensitive lacquer, of a water-receptive layer, of a dried, previously sprayed-on emulsion which can be dissolved either with water or with a solvent.
  • a method for masking components to be thermally sprayed provides a device, which is at least partially elastic at room temperature and undersized with respect to a component to be protected, in order to improve the quality of the sprayed layers adjacent to the masking and to ensure a reproducible production process.
  • elastic deformation of the corresponding device is attached to the corresponding component and is held tightly lying in this position during the injection process due to their elastic properties and their small undersize. This is especially for geometrically difficult components, such as turbine blades, the convex and have concave profile curvatures and torsions over the blade length, particularly advantageous.
  • the device is cleaned after completion of the thermal spraying process and subsequent cooling and degradation of the sprayed component in a cleaning process of the spray coating thereon.
  • a cleaning method is to elastically deform the device so that the sprayed layer peels off its surface.
  • Another cleaning method includes, for example, holding the device to be cleaned in a water or solvent bath whose temperature is varied.
  • Another cleaning method is to use ultra-sonic to aid in the cleaning procedure.
  • Fig. 1 is a schematic representation of a component to be partially coated on the lower part of a device according to the invention for masking a component zone is mounted;
  • Fig. 2 is a schematic detail view of the device of Fig. 1 prior to its attachment to the component.
  • FIG. 1 shows a schematic representation of a component 2 to be partially coated by means of thermal spraying, to the lower part of which a device 1 according to the invention for covering the lower component zone is attached.
  • the component 2 is the blade of a rotor of a gas turbine, wherein only the blade 2 was shown.
  • FIG. 1 shows the length of the blade D and the length of the device L e applied therefrom for masking a component zone.
  • the upper rear portion of the blade is coated with a thermally sprayed wear resistant layer of chromium carbide nickel aluminum.
  • the device 1 for masking the lower part of the blade 2 is made entirely of polyamide and its height corresponds to half the blade height.
  • FIG. 2 shows a schematic representation of a device 1 according to the invention for masking a component zone before it is attached to the blade 2.
  • FIG. 2 also shows the length LN of the elastic device not yet attached.
  • the shape of the device 1 corresponds to the shape of the airfoil 2, wherein the device 1 is hollow over its entire height.
  • the shape of the recess also corresponds to that of the airfoil 2, wherein the device 1 is provided with a lower dimension, so that LN ⁇ L e applies and thus the recess also has smaller dimensions than the airfoil 2.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Details Or Accessories Of Spraying Plant Or Apparatus (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Abstract

La présente invention concerne un dispositif (1) et un procédé de masquage d'une zone d'un élément (2) ne devant pas être atteinte par un jet lors du revêtement de l'élément par projection à chaud, le dispositif (1) étant au moins partiellement élastiquement déformable à température ambiante de manière à pouvoir être appliqué sur l'élément (2), le dispositif (1) présentant au moins une surface inélastique pendant la projection à chaud, de sorte qu'au moment de l'impact, les particules pulvérisées restent accrochées à la surface du dispositif, et ce dispositif (1) pouvant être retiré de la zone recouverte, sans résidu, après la projection à chaud. L'invention se rapporte également à un procédé de masquage d'une zone d'un élément (2) lors du revêtement de l'élément par projection à chaud ainsi que l'utilisation du dispositif (1) selon l'invention et la mise en oeuvre du procédé selon l'invention en particulier pour la fabrication, la réparation ou l'enduction en particulier d'éléments (2) de turbines à gaz ou de groupes motopropulseurs. L'invention offre ainsi une solution simple et réutilisable, qui évite les inconvénients de l'état de la technique.
EP09776090A 2008-09-20 2009-08-11 Dispositif et procédé de masquage d'une zone d'un élément Withdrawn EP2326740A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008048127A DE102008048127A1 (de) 2008-09-20 2008-09-20 Vorrichtung und Verfahren zum Maskieren einer Bauteilzone
PCT/DE2009/001143 WO2010031370A1 (fr) 2008-09-20 2009-08-11 Dispositif et procédé de masquage d'une zone d'un élément

Publications (1)

Publication Number Publication Date
EP2326740A1 true EP2326740A1 (fr) 2011-06-01

Family

ID=41632060

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09776090A Withdrawn EP2326740A1 (fr) 2008-09-20 2009-08-11 Dispositif et procédé de masquage d'une zone d'un élément

Country Status (4)

Country Link
US (1) US20110177250A1 (fr)
EP (1) EP2326740A1 (fr)
DE (1) DE102008048127A1 (fr)
WO (1) WO2010031370A1 (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012105521A1 (de) 2012-06-25 2014-01-02 Nemak Dillingen Gmbh Verwendung einer Kohlenstoffbeschichtung sowie Maskierungsmittel und Beschichtungsanlage zum thermischen Spritzen
DE102013200198A1 (de) * 2013-01-09 2014-07-10 Bayerische Motoren Werke Aktiengesellschaft Metallisches Mehrfarbendekor
WO2014123841A1 (fr) * 2013-02-10 2014-08-14 United Technologies Corporation Film amovible pour surfaces de profil aérodynamique
DE102013223856A1 (de) * 2013-11-21 2015-05-21 Siemens Aktiengesellschaft Vorrichtung zum Schutz von Bauteilen beim Beschichten und Verfahren zur Beschichtung
DE102014204117A1 (de) * 2014-03-06 2015-10-15 MTU Aero Engines AG Verfahren und Vorrichtung zum partiellen Abdecken eines Bauteilbereichs eines Bauteils
CN108603274A (zh) * 2015-11-12 2018-09-28 欧瑞康美科股份公司，沃伦 用于遮盖应以热喷覆层而被覆层的构件的方法
DE102016207863A1 (de) * 2016-05-09 2017-11-09 MTU Aero Engines AG Verfahren zum Bearbeiten wenigstens eines Bauteilbereichs eines Bauteils und Maskierungselement zum partiellen Abdecken eines zu bearbeitenden Bauteils
DE102016211397A1 (de) * 2016-06-24 2017-12-28 MTU Aero Engines AG Maskierungseinrichtung und Verfahren zum Herstellen einer Maskierungseinrichtung zum partiellen Abdecken eines Bauteils
CA3053782C (fr) * 2017-02-17 2021-08-10 Mti Masking Innovations Inc. Film pour masquer des composants d'aeronef et methode de deploiement
CN107379862A (zh) * 2017-07-25 2017-11-24 苏州特铭精密科技有限公司 一种手柄装饰盖加工方法、手柄装饰盖及汽车手柄
DE102018209615A1 (de) 2018-06-15 2019-12-19 MTU Aero Engines AG Abdeckvorrichtung zum Abdecken von wenigstens einem Bereich eines Bauteils während einem Hochtemperaturbeschichtungsverfahren
WO2020097042A1 (fr) * 2018-11-07 2020-05-14 Orizon Aerostructures, Llc Systèmes, dispositifs et procédés à utiliser avec des pièces aérospatiales
DE102019004282A1 (de) * 2019-06-17 2020-09-10 Daimler Ag Maske zum Maskieren einer Zylinderbohrung
CN110918303B (zh) * 2019-12-31 2024-06-18 广西玉柴机器股份有限公司 机油滤清器的屏蔽工具及屏蔽方法
CN112553557A (zh) * 2020-11-10 2021-03-26 中国航发北京航空材料研究院 一种带叶片的槽形零件热喷涂防护方法
CN112538601A (zh) * 2020-11-20 2021-03-23 西安交通大学 一种基于可重复使用的热喷涂用金属/聚合物复合结构遮挡工装的制造方法
RU2750047C1 (ru) * 2020-11-26 2021-06-21 Общество С Ограниченной Ответственностью «Гласс Декор» Способ нанесения лакокрасочного покрытия на стеклянное изделие
DE202021105511U1 (de) 2021-10-12 2023-01-17 Weidplas Gmbh Vorrichtung zum Maskieren eines Bauteils und Vorrichtung zum Beschichten eines Bauteils
EP4176975A1 (fr) * 2021-11-09 2023-05-10 ZF CV Systems Europe BV Procédé de peinture d'un composant d'un frein de véhicule, en particulier un frein de véhicule utilitaire, ainsi que bouchons d'étanchéité et utilisation correspondante

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4464430A (en) 1981-02-26 1984-08-07 Alloy Surfaces Company, Inc. Metal diffusion
JPH03158451A (ja) 1989-11-15 1991-07-08 Ngk Insulators Ltd 溶射用マスキングテープ
US5203944A (en) 1991-10-10 1993-04-20 Prinz Fritz B Method for fabrication of three-dimensional articles by thermal spray deposition using masks as support structures
JP3021193B2 (ja) 1992-06-26 2000-03-15 株式会社フジクラ 溶射用マスキング治具およびマスキング方法
US5573814A (en) 1995-10-30 1996-11-12 Ford Motor Company Masking cylinder bore extremities from internal thermal spraying
US5691018A (en) 1995-12-15 1997-11-25 Caterpillar Inc. Silicone mask for thermal spray coating system
US5902647A (en) * 1996-12-03 1999-05-11 General Electric Company Method for protecting passage holes in a metal-based substrate from becoming obstructed, and related compositions
EP1080394A1 (fr) * 1998-04-21 2001-03-07 President And Fellows of Harvard College Masque elastomere et son utilisation dans la fabrication de dispositifs, dont des afficheurs electroluminescents pixelises
US6060117A (en) 1998-08-31 2000-05-09 Ford Global Technologies, Inc. Making and using thermal spray masks carrying thermoset epoxy coating
US6395090B1 (en) * 1999-08-16 2002-05-28 Ford Global Technologies, Inc. Masking for engine blocks for thermally sprayed coatings
US6645299B2 (en) 2001-09-18 2003-11-11 General Electric Company Method and assembly for masking
EP1387040B1 (fr) * 2002-08-02 2006-12-06 ALSTOM Technology Ltd Procédé pour la protection d'une aire partielle d'une pièce de travail
WO2008138384A1 (fr) * 2007-05-16 2008-11-20 Siemens Aktiengesellschaft Composition de matériaux à employer comme matière de masquage pour protéger les zones à ne pas revêtir d'un élément de turbine, et procédé pour revêtir des éléments de turbine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2010031370A1 *

Also Published As

Publication number Publication date
US20110177250A1 (en) 2011-07-21
DE102008048127A1 (de) 2010-03-25
WO2010031370A1 (fr) 2010-03-25

Similar Documents

Publication Publication Date Title
EP2326740A1 (fr) Dispositif et procédé de masquage d'une zone d'un élément
DE19547903C1 (de) Verfahren zur Herstellung oder Instandsetzung von Schaufeln für Turbomaschinen mittels Laserstrahlauftragsschweißen unter Verwendung eines Metallpulvers als Zusatzwerkstoff, sowie Stützform zur Herstellung oder Instandsetzung derartiger Schaufeln und Verfahren zur Herstellung der Stützform
DE102008042237B4 (de) Metallische Beschichtung
EP1762303B1 (fr) Procédé pour préparer des aubes de turbine en vue de leur revêtement par pulvérisation et support pour fixer de telles aubes
DE102006057641A1 (de) Reparatur und/oder Konturänderung einer Formoberfläche eines Formwerkzeugs
DE19909675A1 (de) Schichtstruktur und Verfahren zu ihrer Herstellung
DE102008011427B4 (de) Verfahren zur Herstellung und Anwendung einer Schutzschicht
EP2038083B1 (fr) Procédé de réparation et/ou de remplacement d'éléments individuels d'une pièce d'une turbine à gaz
DE102009051717A1 (de) Verfahren zum thermischen Beschichten einer Oberfläche eines Bauteils
DE102018129495A1 (de) Verfahren zur Reparatur eines Metall-Faser-Kunststoff-Verbund-Bauteils
DE102006029070B3 (de) Verfahren zum Beschichten eines Bauteils, in dessen Oberfläche Löcher vorgesehen sind
DE202006009145U1 (de) Verbindung von Bauteilen
DE102008053394A1 (de) Vorrichtung zum partiellen Abdecken einer Bauteilzone
EP1048389B1 (fr) Protection pour la surface d'une pièce
DE102016207863A1 (de) Verfahren zum Bearbeiten wenigstens eines Bauteilbereichs eines Bauteils und Maskierungselement zum partiellen Abdecken eines zu bearbeitenden Bauteils
DE102006046518A1 (de) Verfahren zum Beschichten eines Substrates
EP1593445A1 (fr) Procédé de fabrication d'un élément coulé creux avec un revêtement intérieur
DE102009008887A1 (de) Verfahren zum Herstellen einer Schaufelpanzerung auf einer Schaufel für eine Turbomaschine
DE102012105521A1 (de) Verwendung einer Kohlenstoffbeschichtung sowie Maskierungsmittel und Beschichtungsanlage zum thermischen Spritzen
DE102006057640A1 (de) Verfahren zum Herstellen eines Formwerkzeugs mit einer Verschleißschutzschicht
DE102016211397A1 (de) Maskierungseinrichtung und Verfahren zum Herstellen einer Maskierungseinrichtung zum partiellen Abdecken eines Bauteils
WO2008067959A1 (fr) Procédé de fabrication d'un outil de moulage
EP1598444B1 (fr) Procédé d'ajustement par projection de carboglace de la conductivité électrique d'un revêtement d'un composant d'une machine, cette conductivité électrique étant variable avec la pression
DE102013202483A1 (de) Verfahren und Maschine zur Herstellung einer Oberflächenbeschichtung
EP2860231A1 (fr) Procédé de fabrication d'une couche de brasage mince

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: 20110318

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 HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

AX Request for extension of the european patent

Extension state: AL BA RS

RIN1 Information on inventor provided before grant (corrected)

Inventor name: SCHNEIDERBANGER, STEFAN

Inventor name: HERTTER, MANUEL

Inventor name: JAKIMOV, ANDREAS

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

Effective date: 20120918

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

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20140301