JP2004245216A5 - - Google Patents

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Publication number
JP2004245216A5
JP2004245216A5 JP2004003556A JP2004003556A JP2004245216A5 JP 2004245216 A5 JP2004245216 A5 JP 2004245216A5 JP 2004003556 A JP2004003556 A JP 2004003556A JP 2004003556 A JP2004003556 A JP 2004003556A JP 2004245216 A5 JP2004245216 A5 JP 2004245216A5
Authority
JP
Japan
Prior art keywords
hole
ceramic
laser beam
ceramic coating
milliseconds
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2004003556A
Other languages
English (en)
Japanese (ja)
Other versions
JP4344885B2 (ja
JP2004245216A (ja
Filing date
Publication date
Priority claimed from US10/248,343 external-priority patent/US6847004B2/en
Application filed filed Critical
Publication of JP2004245216A publication Critical patent/JP2004245216A/ja
Publication of JP2004245216A5 publication Critical patent/JP2004245216A5/ja
Application granted granted Critical
Publication of JP4344885B2 publication Critical patent/JP4344885B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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JP2004003556A 2003-01-10 2004-01-09 部品の表面孔内のセラミック皮膜堆積物を除去する方法 Expired - Lifetime JP4344885B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/248,343 US6847004B2 (en) 2003-01-10 2003-01-10 Process of removing a ceramic coating deposit in a surface hole of a component

Publications (3)

Publication Number Publication Date
JP2004245216A JP2004245216A (ja) 2004-09-02
JP2004245216A5 true JP2004245216A5 (enExample) 2007-02-22
JP4344885B2 JP4344885B2 (ja) 2009-10-14

Family

ID=32505744

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004003556A Expired - Lifetime JP4344885B2 (ja) 2003-01-10 2004-01-09 部品の表面孔内のセラミック皮膜堆積物を除去する方法

Country Status (6)

Country Link
US (1) US6847004B2 (enExample)
EP (1) EP1437194B1 (enExample)
JP (1) JP4344885B2 (enExample)
BR (1) BRPI0400249B1 (enExample)
CA (1) CA2454922C (enExample)
SG (1) SG116525A1 (enExample)

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US20030155328A1 (en) * 2002-02-15 2003-08-21 Huth Mark C. Laser micromachining and methods and systems of same
US20050036004A1 (en) * 2003-08-13 2005-02-17 Barbara Horn Methods and systems for conditioning slotted substrates
EP1510283B1 (en) * 2003-08-27 2007-10-17 ALSTOM Technology Ltd Automated adaptive machining of obstructed passages
US20060016191A1 (en) * 2004-07-23 2006-01-26 Honeywell International Inc. Combined effusion and thick TBC cooling method
EP1810774A1 (de) * 2006-01-24 2007-07-25 Siemens Aktiengesellschaft Verfahren zur Herstellung eines Loches
US7216485B2 (en) * 2004-09-03 2007-05-15 General Electric Company Adjusting airflow in turbine component by depositing overlay metallic coating
DE102005015153B4 (de) * 2005-03-31 2017-03-09 General Electric Technology Gmbh Verfahren zum Reparieren oder Erneuern von Kühllöchern einer beschichteten Komponente und beschichtete Komponente mit Kühllöchern einer Gasturbine
ATE474821T1 (de) * 2006-03-28 2010-08-15 Comadur Sa Verfahren zur herstellung einer satinierten oberfläche
US7992272B2 (en) * 2007-05-29 2011-08-09 Metem Corporation Method and apparatus for milling thermal barrier coated metals
US20090142548A1 (en) * 2007-10-18 2009-06-04 David Bruce Patterson Air cooled gas turbine components and methods of manufacturing and repairing the same
DE102009011913A1 (de) * 2009-03-10 2010-09-16 Rolls-Royce Deutschland Ltd & Co Kg Wärmedämmschichtsystem
US20110076405A1 (en) * 2009-09-25 2011-03-31 United Technologies Corporation Hole drilling with close proximity backwall
US8857055B2 (en) * 2010-01-29 2014-10-14 General Electric Company Process and system for forming shaped air holes
JP2012072705A (ja) * 2010-09-29 2012-04-12 Hitachi Ltd ガスタービン翼の製造方法
US10113435B2 (en) 2011-07-15 2018-10-30 United Technologies Corporation Coated gas turbine components
US9023486B2 (en) * 2011-10-13 2015-05-05 General Electric Company Thermal barrier coating systems and processes therefor
EP2599575A1 (de) * 2011-12-01 2013-06-05 Siemens Aktiengesellschaft Laserbohren von Durchgangsbohrungen ohne Schutz im Inneren
EP2604377B1 (de) * 2011-12-15 2015-07-15 Siemens Aktiengesellschaft Verfahren zur Laserbearbeitung eines Schichtsystems mit keramischer Schicht
US9598979B2 (en) 2012-02-15 2017-03-21 United Technologies Corporation Manufacturing methods for multi-lobed cooling holes
US8962066B2 (en) 2012-06-04 2015-02-24 United Technologies Corporation Coating for cooling air holes
US10100650B2 (en) * 2012-06-30 2018-10-16 General Electric Company Process for selectively producing thermal barrier coatings on turbine hardware
DE102013109116A1 (de) * 2012-08-27 2014-03-27 General Electric Company (N.D.Ges.D. Staates New York) Bauteil mit Kühlkanälen und Verfahren zur Herstellung
US11143030B2 (en) * 2012-12-21 2021-10-12 Raytheon Technologies Corporation Coating process for gas turbine engine component with cooling holes
US10815796B2 (en) 2013-01-30 2020-10-27 Raytheon Technologies Corporation Coating process for gas turbine engine component with cooling holes
WO2014151479A2 (en) * 2013-03-22 2014-09-25 Videojet Technologies Inc. Method of removing a coating of a substrate
DE102013211047B4 (de) * 2013-06-13 2015-04-30 MTU Aero Engines AG Verfahren zum Verschließen von Kühlluftbohrungen
JP5908009B2 (ja) * 2013-08-20 2016-04-26 三菱重工業株式会社 レーザ加工方法及びレーザ加工装置
US9707645B2 (en) 2014-01-09 2017-07-18 General Electric Company Systems, methods, and apparatus for locating and drilling closed holes of a turbine component
EP3094865A4 (en) * 2014-01-16 2017-09-13 United Technologies Corporation Systems and methods for thermal location of cooling holes
DE102014204806A1 (de) * 2014-03-14 2015-09-17 Siemens Aktiengesellschaft Verfahren zur Neuherstellung von Durchgangslöchern in einem Schichtsystem
GB201419327D0 (en) 2014-10-30 2014-12-17 Rolls Royce Plc A cooled component
US9718735B2 (en) * 2015-02-03 2017-08-01 General Electric Company CMC turbine components and methods of forming CMC turbine components
JP2018051764A (ja) * 2016-09-26 2018-04-05 エスアイアイ・プリンテック株式会社 噴射孔プレートの製造方法
SG10201708210PA (en) * 2017-10-05 2019-05-30 United Technologies Corp Multi-step clearance of coating
WO2019245532A1 (en) * 2018-06-19 2019-12-26 Siemens Aktiengesellschaft Manufacturing method for finishing of ceramic cores flash
US11407067B2 (en) * 2018-06-29 2022-08-09 Pratt & Whitney Canada Corp. Method for repairing a part
GB201918856D0 (en) * 2019-12-19 2020-02-05 Smith & Nephew Sensor integrated dressings and systems
GB202107236D0 (en) 2021-05-20 2021-07-07 Rolls Royce Plc Debris removal
EP4105449A1 (en) 2021-06-18 2022-12-21 Raytheon Technologies Corporation Hybrid bonded configuration for blade outer airseal (boas)
EP4105440A1 (en) 2021-06-18 2022-12-21 Raytheon Technologies Corporation Hybrid superalloy article and method of manufacture thereof
US20230147399A1 (en) * 2021-06-18 2023-05-11 Raytheon Technologies Corporation Joining individual turbine vanes with field assisted sintering technology (fast)
US11821337B1 (en) * 2022-08-05 2023-11-21 Rtx Corporation Internal aluminide coating for vanes and blades and method of manufacture
US20250345872A1 (en) * 2024-05-07 2025-11-13 Rtx Corporation Method of diffusion braze repair of cooling holes and cracks

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US4818834A (en) * 1988-03-21 1989-04-04 Raycon Corporation Process for drilling chamfered holes
US5216808A (en) * 1990-11-13 1993-06-08 General Electric Company Method for making or repairing a gas turbine engine component
US5465780A (en) * 1993-11-23 1995-11-14 Alliedsignal Inc. Laser machining of ceramic cores
US6172331B1 (en) 1997-09-17 2001-01-09 General Electric Company Method and apparatus for laser drilling
US6154959A (en) * 1999-08-16 2000-12-05 Chromalloy Gas Turbine Corporation Laser cladding a turbine engine vane platform
SG127668A1 (en) * 1999-11-24 2006-12-29 Gen Electric Method for thermal barrier coating
US6441341B1 (en) * 2000-06-16 2002-08-27 General Electric Company Method of forming cooling holes in a ceramic matrix composite turbine components
US6420677B1 (en) 2000-12-20 2002-07-16 Chromalloy Gas Turbine Corporation Laser machining cooling holes in gas turbine components
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
US6663919B2 (en) * 2002-03-01 2003-12-16 General Electric Company Process of removing a coating deposit from a through-hole in a component and component processed thereby

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