DE60301074T2 - Verfahren zur Entfernung der Beschichtung eines Durchganglochs in einem Bauteil und auf diese Weise bearbeitetes Bauteil - Google Patents

Verfahren zur Entfernung der Beschichtung eines Durchganglochs in einem Bauteil und auf diese Weise bearbeitetes Bauteil Download PDF

Info

Publication number
DE60301074T2
DE60301074T2 DE2003601074 DE60301074T DE60301074T2 DE 60301074 T2 DE60301074 T2 DE 60301074T2 DE 2003601074 DE2003601074 DE 2003601074 DE 60301074 T DE60301074 T DE 60301074T DE 60301074 T2 DE60301074 T2 DE 60301074T2
Authority
DE
Germany
Prior art keywords
hole
component
coating
jet
holes
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.)
Expired - Lifetime
Application number
DE2003601074
Other languages
German (de)
English (en)
Other versions
DE60301074D1 (de
Inventor
Gilbert Cincinnati Farmer
Jeffrey Arnold Cincinnati Fehrenbach
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.)
General Electric Co
Original Assignee
General Electric Co
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=27733408&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE60301074(T2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60301074D1 publication Critical patent/DE60301074D1/de
Publication of DE60301074T2 publication Critical patent/DE60301074T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186—Film cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/06—Cooling passages of turbine components, e.g. unblocking or preventing blocking of cooling passages of turbine components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/10—Manufacture by removing material
    • F05D2230/13—Manufacture by removing material using lasers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/607—Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49318—Repairing or disassembling
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12361—All metal or with adjacent metals having aperture or cut
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
  • Coating By Spraying Or Casting (AREA)
DE2003601074 2002-03-01 2003-02-26 Verfahren zur Entfernung der Beschichtung eines Durchganglochs in einem Bauteil und auf diese Weise bearbeitetes Bauteil Expired - Lifetime DE60301074T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/086,266 US6663919B2 (en) 2002-03-01 2002-03-01 Process of removing a coating deposit from a through-hole in a component and component processed thereby
US86266 2002-03-01

Publications (2)

Publication Number Publication Date
DE60301074D1 DE60301074D1 (de) 2005-09-01
DE60301074T2 true DE60301074T2 (de) 2006-06-01

Family

ID=27733408

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2003601074 Expired - Lifetime DE60301074T2 (de) 2002-03-01 2003-02-26 Verfahren zur Entfernung der Beschichtung eines Durchganglochs in einem Bauteil und auf diese Weise bearbeitetes Bauteil

Country Status (7)

Country Link
US (2) US6663919B2 (OSRAM)
EP (1) EP1340587B1 (OSRAM)
JP (1) JP2003285269A (OSRAM)
BR (1) BR0300479A (OSRAM)
CA (1) CA2419361A1 (OSRAM)
DE (1) DE60301074T2 (OSRAM)
SG (1) SG106131A1 (OSRAM)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014220362A1 (de) * 2014-10-08 2016-04-14 Siemens Aktiengesellschaft Verschließen von Löchern mittels eines thermischen Spritzverfahrens durch ein Pulvergemisch

Families Citing this family (69)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7003880B2 (en) * 2001-10-05 2006-02-28 Denso Corporation Injector nozzle and method of manufacturing injector nozzle
US6926928B2 (en) * 2002-07-19 2005-08-09 General Electric Company Protection of a gas turbine component by a vapor-deposited oxide coating
US20040106360A1 (en) * 2002-11-26 2004-06-03 Gilbert Farmer Method and apparatus for cleaning combustor liners
US20040163254A1 (en) * 2002-12-27 2004-08-26 Masanori Miyagawa Method for manufacturing injection hole member
US6847004B2 (en) * 2003-01-10 2005-01-25 General Electric Company Process of removing a ceramic coating deposit in a surface hole of a component
US7744020B2 (en) * 2003-07-21 2010-06-29 Continental Automotive Systems Us, Inc. Fuel injector including an orifice disc, and a method of forming the orifice disc including punching and shaving
US20050123785A1 (en) * 2003-12-04 2005-06-09 Purusottam Sahoo High temperature clearance coating
US7805822B2 (en) * 2003-12-15 2010-10-05 Turbocombustor Technology, Inc. Process for removing thermal barrier coatings
DE102004001394A1 (de) * 2004-01-09 2005-08-04 Mtu Aero Engines Gmbh Verfahren zur Herstellung bzw. Bearbeitung von Bauteilen
US20060016191A1 (en) * 2004-07-23 2006-01-26 Honeywell International Inc. Combined effusion and thick TBC cooling method
US7216485B2 (en) * 2004-09-03 2007-05-15 General Electric Company Adjusting airflow in turbine component by depositing overlay metallic coating
US7186091B2 (en) * 2004-11-09 2007-03-06 General Electric Company Methods and apparatus for cooling gas turbine engine components
EP1686240A1 (de) * 2005-01-27 2006-08-02 Siemens Aktiengesellschaft Bauteil mit Abflachung in einem Loch
US20060275553A1 (en) * 2005-06-03 2006-12-07 Siemens Westinghouse Power Corporation Electrically conductive thermal barrier coatings capable for use in electrode discharge machining
GB0610578D0 (en) 2006-05-27 2006-07-05 Rolls Royce Plc Method of removing deposits
US7622160B2 (en) 2006-07-28 2009-11-24 General Electric Company Method for concurrent thermal spray and cooling hole cleaning
US7544112B1 (en) * 2006-12-13 2009-06-09 Huffman Corporation Method and apparatus for removing coatings from a substrate using multiple sequential steps
DE102008004559B4 (de) 2007-01-23 2017-03-16 General Electric Technology Gmbh Verfahren zum Bearbeiten eines thermisch belasteten Bauteils
US20090142548A1 (en) * 2007-10-18 2009-06-04 David Bruce Patterson Air cooled gas turbine components and methods of manufacturing and repairing the same
US8727831B2 (en) * 2008-06-17 2014-05-20 General Electric Company Method and system for machining a profile pattern in ceramic coating
EP2175003A1 (en) 2008-10-13 2010-04-14 Services Pétroliers Schlumberger Particle-loaded wash for well cleanup
DE102009007164A1 (de) * 2009-02-03 2010-08-12 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zum Ausbilden einer Kühlluftöffnung in einer Wand einer Gasturbinenbrennkammer sowie nach dem Verfahren hergestellte Brennkammerwand
US8776370B2 (en) * 2009-03-05 2014-07-15 United Technologies Corporation Method of maintaining gas turbine engine components
US20100263384A1 (en) * 2009-04-17 2010-10-21 Ronald James Chila Combustor cap with shaped effusion cooling holes
ES2553224T3 (es) * 2009-07-24 2015-12-07 Mogas Industries, Inc. Miembro tubular con camisa de manguito térmico
US20110076405A1 (en) * 2009-09-25 2011-03-31 United Technologies Corporation Hole drilling with close proximity backwall
IT1399945B1 (it) 2010-04-29 2013-05-09 Turbocoating S P A Metodo e apparato per rimuovere ricoprimenti ceramici, con sabbiatura di anidride carbonica allo stato solido.
US8905713B2 (en) * 2010-05-28 2014-12-09 General Electric Company Articles which include chevron film cooling holes, and related processes
JP5517163B2 (ja) 2010-10-07 2014-06-11 株式会社日立製作所 タービン翼の冷却孔加工方法
US8673397B2 (en) * 2010-11-10 2014-03-18 General Electric Company Methods of fabricating and coating a component
US9089933B2 (en) 2010-12-20 2015-07-28 Pratt & Whitney Canada Corp. Method for making and repairing effusion cooling holes in cumbustor liner
FR2970666B1 (fr) * 2011-01-24 2013-01-18 Snecma Procede de perforation d'au moins une paroi d'une chambre de combustion
US20120328445A1 (en) * 2011-06-27 2012-12-27 United Technologies Corporation Grit blast free thermal barrier coating rework
US20130020291A1 (en) * 2011-07-19 2013-01-24 Pratt & Whitney Canada Corp. Laser drilling methods of shallow-angled holes
US8631557B2 (en) * 2011-07-19 2014-01-21 Pratt & Whitney Canada Corp. Laser drilling methods of shallow-angled holes
US9434025B2 (en) 2011-07-19 2016-09-06 Pratt & Whitney Canada Corp. Laser drilling methods of shallow-angled holes
US20130086784A1 (en) * 2011-10-06 2013-04-11 General Electric Company Repair methods for cooled components
EP2604377B1 (de) * 2011-12-15 2015-07-15 Siemens Aktiengesellschaft Verfahren zur Laserbearbeitung eines Schichtsystems mit keramischer Schicht
US20130203320A1 (en) * 2012-02-06 2013-08-08 Hamid R. Ghalambor Methods and Systems for Sensor-Based Deburring
WO2013144022A1 (en) 2012-03-28 2013-10-03 Alstom Technology Ltd Method for removing a ceramic
US10100650B2 (en) 2012-06-30 2018-10-16 General Electric Company Process for selectively producing thermal barrier coatings on turbine hardware
US9260788B2 (en) * 2012-10-30 2016-02-16 General Electric Company Reinforced articles and methods of making the same
US11143030B2 (en) * 2012-12-21 2021-10-12 Raytheon Technologies Corporation Coating process for gas turbine engine component with cooling holes
US9523287B2 (en) 2013-01-18 2016-12-20 General Electric Company Cooling hole cleaning method and apparatus
JP5456192B1 (ja) * 2013-02-26 2014-03-26 三菱重工業株式会社 タービン翼の加工方法、加工工具及びタービン翼
DE102013211047B4 (de) * 2013-06-13 2015-04-30 MTU Aero Engines AG Verfahren zum Verschließen von Kühlluftbohrungen
EP3058200A4 (en) * 2013-10-18 2016-11-16 United Technologies Corp TURBINE EXHAUST BOX WITH COOLING HOLES COATED
EP2883977A1 (en) * 2013-12-11 2015-06-17 Siemens Aktiengesellschaft Method for coating a component with holes
US20150165569A1 (en) * 2013-12-18 2015-06-18 Petya M. Georgieva Repair of turbine engine components using waterjet ablation process
GB201418042D0 (en) * 2014-10-13 2014-11-26 Rolls Royce Plc A liner element for a combustor, and a related method
US20160243655A1 (en) * 2015-02-20 2016-08-25 General Electric Company Component repair using confined laser drilling
US10443395B2 (en) 2016-03-18 2019-10-15 General Electric Company Component for a turbine engine with a film hole
US10619499B2 (en) * 2017-01-23 2020-04-14 General Electric Company Component and method for forming a component
US10895157B2 (en) * 2017-04-24 2021-01-19 Honeywell International Inc. Gas turbine engine components with air-cooling features, and related methods of manufacturing the same
US11440139B2 (en) 2018-05-03 2022-09-13 Raytheon Technologies Corporation Liquid enhanced laser stripping
US10815783B2 (en) 2018-05-24 2020-10-27 General Electric Company In situ engine component repair
US11407067B2 (en) * 2018-06-29 2022-08-09 Pratt & Whitney Canada Corp. Method for repairing a part
US20200024951A1 (en) * 2018-07-17 2020-01-23 General Electric Company Component for a turbine engine with a cooling hole
US11585224B2 (en) 2020-08-07 2023-02-21 General Electric Company Gas turbine engines and methods associated therewith
CN112855281B (zh) * 2021-01-29 2022-06-10 南京航空航天大学 基于2.5d编织陶瓷基复合材料的台阶气膜冷却孔及其设计方法
US11603769B2 (en) 2021-08-13 2023-03-14 Raytheon Technologies Corporation Forming lined cooling aperture(s) in a turbine engine component
US11913119B2 (en) 2021-08-13 2024-02-27 Rtx Corporation Forming cooling aperture(s) in a turbine engine component
US11732590B2 (en) 2021-08-13 2023-08-22 Raytheon Technologies Corporation Transition section for accommodating mismatch between other sections of a cooling aperture in a turbine engine component
US11813706B2 (en) 2021-08-13 2023-11-14 Rtx Corporation Methods for forming cooling apertures in a turbine engine component
US12123839B2 (en) 2021-08-13 2024-10-22 Rtx Corporation Forming and/or inspecting cooling aperture(s) in a turbine engine component
US11673200B2 (en) 2021-08-13 2023-06-13 Raytheon Technologies Corporation Forming cooling aperture(s) using electrical discharge machining
US11542831B1 (en) 2021-08-13 2023-01-03 Raytheon Technologies Corporation Energy beam positioning during formation of a cooling aperture
US11898465B2 (en) 2021-08-13 2024-02-13 Rtx Corporation Forming lined cooling aperture(s) in a turbine engine component
US12006837B2 (en) * 2022-01-28 2024-06-11 Rtx Corporation Ceramic matrix composite article and method of making the same

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06346281A (ja) * 1993-06-08 1994-12-20 Makoo Kk ワーク表面処理方法
JP3611607B2 (ja) * 1994-10-12 2005-01-19 石川島播磨重工業株式会社 エンジン部品のクーリングホール再加工方法
US5702288A (en) * 1995-08-30 1997-12-30 United Technologies Corporation Method of removing excess overlay coating from within cooling holes of aluminide coated gas turbine engine components
JP3657331B2 (ja) * 1995-12-08 2005-06-08 石川島播磨重工業株式会社 エンジン部品のクーリングホール再加工方法及び該方法に使用されるクーリングホール再加工装置
GB9723762D0 (en) * 1997-11-12 1998-01-07 Rolls Royce Plc A method of coating a component
US6210488B1 (en) * 1998-12-30 2001-04-03 General Electric Company Method of removing a thermal barrier coating
SG127668A1 (en) * 1999-11-24 2006-12-29 Gen Electric Method for thermal barrier coating
US6329015B1 (en) * 2000-05-23 2001-12-11 General Electric Company Method for forming shaped holes
US6368060B1 (en) * 2000-05-23 2002-04-09 General Electric Company Shaped cooling hole for an airfoil
US6380512B1 (en) * 2001-10-09 2002-04-30 Chromalloy Gas Turbine Corporation Method for removing coating material from a cooling hole of a gas turbine engine component

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014220362A1 (de) * 2014-10-08 2016-04-14 Siemens Aktiengesellschaft Verschließen von Löchern mittels eines thermischen Spritzverfahrens durch ein Pulvergemisch

Also Published As

Publication number Publication date
SG106131A1 (en) 2004-09-30
EP1340587B1 (en) 2005-07-27
US20040115447A1 (en) 2004-06-17
US20030165621A1 (en) 2003-09-04
US6908657B2 (en) 2005-06-21
EP1340587A3 (en) 2003-12-17
JP2003285269A (ja) 2003-10-07
BR0300479A (pt) 2004-08-17
CA2419361A1 (en) 2003-09-01
US6663919B2 (en) 2003-12-16
DE60301074D1 (de) 2005-09-01
EP1340587A2 (en) 2003-09-03

Similar Documents

Publication Publication Date Title
DE60217590T3 (de) Verfahren zum Reparieren eines gelöcherten Gasturbinenbauteils
DE69707056T2 (de) Verfahren zur Reparatur einer Wärmesperrschicht
EP1340587B1 (en) Process of removing a coating deposit from a through-hole in a component and component processed thereby
DE69730245T2 (de) Verfahren zur behandlung von metallteilen
DE69807892T2 (de) Verfahren zur herstellung eines durchbrochenen artikels zur wiederbeschichtung
DE60310168T2 (de) Verfahren zum Schutz von Teilflächen eines Werkstücks
DE69734625T2 (de) Fluidum gekühlter Gegenstand und seine Herstellungsweise
DE69524353T2 (de) Hochtemperatur-Schutzschicht
DE69815024T2 (de) Verfahren zum Beschichten eines Bauelementes
EP1115906B1 (de) Verfahren zur innenbearbeitung eines hohlen bauteils
DE102011057170A1 (de) Verfahren zur Erzeugung eines filmgekühlten Gegenstands
EP2732072B1 (de) Verfahren zum reparieren einer schadstelle in einem gussteil und verfahren zum erzeugen eines geeigneten reparaturmaterials
DE69401543T2 (de) Zerkleinerungs- oder Raffinationsscheibe für Papierfaserbrei sowie Verfahren zu seiner Herstellung
EP3230492B1 (de) Verfahren zum kaltgasspritzen mit maske
WO2000025005A1 (de) Erzeugnis mit wärmedämmschicht sowie verfahren zur herstellung einer wärmedämmschicht
DE102011085801A1 (de) Bauelement und Turbomaschine mit einem Bauelement
DE69522098T2 (de) Thermische sprühdüse zur herstellung von thermischen rauhen sprühbeschichtungen; verfahren zur herstellung von thermischen rauhen sprühbeschichtungen
DE102005050873A1 (de) Verfahren zur Herstellung einer segmentierten Beschichtung und nach dem Verfahren hergestelltes Bauteil
DE602004003757T2 (de) Verfahren zur Aufbereitung und Verfahren zur Herstellung einer Turbinenschaufel
DE10310130A1 (de) Herstellungsverfahren für eine Zylinderblock-Einheit
DE3224305A1 (de) Verfahren zur herstellung einer spannungsunempfindlichen keramischen thermischen sperrschicht auf einem metallsubstrat
WO2011088817A1 (de) Strukturierte oberflächenbeschichtung mittels kinetischem kaltgasspritzen
EP2603355B1 (de) Verfahren zum entfernen einer schicht von einer oberfläche eines körpers
EP1617972B1 (de) Verfahren zum verrunden von kanten an bauteilen
WO2013053581A1 (de) Verfahren zum aufbringen einer verschleissschutzschicht auf eine strömungsmaschinenkomponente

Legal Events

Date Code Title Description
8363 Opposition against the patent