JP2006312782A5 - - Google Patents

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Publication number
JP2006312782A5
JP2006312782A5 JP2006121521A JP2006121521A JP2006312782A5 JP 2006312782 A5 JP2006312782 A5 JP 2006312782A5 JP 2006121521 A JP2006121521 A JP 2006121521A JP 2006121521 A JP2006121521 A JP 2006121521A JP 2006312782 A5 JP2006312782 A5 JP 2006312782A5
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JP
Japan
Prior art keywords
preform
metal powder
binder
alloy
squealer tip
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
JP2006121521A
Other languages
English (en)
Japanese (ja)
Other versions
JP2006312782A (ja
JP5247990B2 (ja
Filing date
Publication date
Priority claimed from US10/908,293 external-priority patent/US7282681B2/en
Application filed filed Critical
Publication of JP2006312782A publication Critical patent/JP2006312782A/ja
Publication of JP2006312782A5 publication Critical patent/JP2006312782A5/ja
Application granted granted Critical
Publication of JP5247990B2 publication Critical patent/JP5247990B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2006121521A 2005-05-05 2006-04-26 金属構成部品を製造する方法 Expired - Fee Related JP5247990B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/908,293 US7282681B2 (en) 2005-05-05 2005-05-05 Microwave fabrication of airfoil tips
US10/908,293 2005-05-05

Publications (3)

Publication Number Publication Date
JP2006312782A JP2006312782A (ja) 2006-11-16
JP2006312782A5 true JP2006312782A5 (enExample) 2009-05-28
JP5247990B2 JP5247990B2 (ja) 2013-07-24

Family

ID=36677158

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006121521A Expired - Fee Related JP5247990B2 (ja) 2005-05-05 2006-04-26 金属構成部品を製造する方法

Country Status (6)

Country Link
US (2) US7282681B2 (enExample)
EP (1) EP1721699A1 (enExample)
JP (1) JP5247990B2 (enExample)
BR (1) BRPI0601722A (enExample)
CA (1) CA2545200A1 (enExample)
SG (1) SG126900A1 (enExample)

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US20070274854A1 (en) * 2006-05-23 2007-11-29 General Electric Company Method of making metallic composite foam components
US20070295785A1 (en) * 2006-05-31 2007-12-27 General Electric Company Microwave brazing using mim preforms
US7845549B2 (en) * 2006-05-31 2010-12-07 General Electric Company MIM braze preforms
GB0705696D0 (en) * 2007-03-24 2007-05-02 Rolls Royce Plc A method of repairing a damaged abradable coating
US20080237403A1 (en) * 2007-03-26 2008-10-02 General Electric Company Metal injection molding process for bimetallic applications and airfoil
US8146250B2 (en) * 2008-05-30 2012-04-03 General Electric Company Method of replacing a composite airfoil
US8087565B2 (en) * 2008-09-08 2012-01-03 General Electric Company Process of filling openings in a component
US20120000072A9 (en) * 2008-09-26 2012-01-05 Morrison Jay A Method of Making a Combustion Turbine Component Having a Plurality of Surface Cooling Features and Associated Components
FR2949366B1 (fr) * 2009-08-31 2011-11-18 Snecma Realisation par procede mim d'un morceau de piece pour la reparation d'une aube de distributeur de turbine
JP2013521650A (ja) 2010-03-05 2013-06-10 アプライド マテリアルズ インコーポレイテッド ラジカル成分ｃｖｄによる共形層
EP2366476B1 (en) * 2010-03-10 2014-07-02 General Electric Company Method for Fabricating Turbine Airfoils and Tip Structures Therefor
US20130104397A1 (en) 2011-10-28 2013-05-02 General Electric Company Methods for repairing turbine blade tips
US9283621B2 (en) * 2012-06-21 2016-03-15 Deere & Company Method for forming a composite article
US9737933B2 (en) * 2012-09-28 2017-08-22 General Electric Company Process of fabricating a shield and process of preparing a component
US9700941B2 (en) * 2012-10-03 2017-07-11 Siemens Energy, Inc. Method for repairing a component for use in a turbine engine
US9863249B2 (en) 2012-12-04 2018-01-09 Siemens Energy, Inc. Pre-sintered preform repair of turbine blades
EP2772329A1 (en) * 2013-02-28 2014-09-03 Alstom Technology Ltd Method for manufacturing a hybrid component
US9682449B2 (en) * 2014-05-09 2017-06-20 United Technologies Corporation Repair material preform
US10072506B2 (en) 2014-06-30 2018-09-11 Rolls-Royce Corporation Coated gas turbine engine components
US9777574B2 (en) 2014-08-18 2017-10-03 Siemens Energy, Inc. Method for repairing a gas turbine engine blade tip
US20160069184A1 (en) * 2014-09-09 2016-03-10 Rolls-Royce Corporation Method of blade tip repair
US10099290B2 (en) * 2014-12-18 2018-10-16 General Electric Company Hybrid additive manufacturing methods using hybrid additively manufactured features for hybrid components
FR3037974B1 (fr) * 2015-06-29 2017-07-21 Snecma Procede de fabrication d'une aube comportant une baignoire integrant un muret
US10029299B2 (en) 2015-07-09 2018-07-24 General Electric Company Three-dimensional manufacturing methods and systems for turbine components
US10767501B2 (en) * 2016-04-21 2020-09-08 General Electric Company Article, component, and method of making a component
US10900363B2 (en) * 2018-08-01 2021-01-26 Honeywell International Inc. Laser tip cladding to net-shape with shrouds
EP3927943B1 (en) * 2019-03-29 2024-10-16 Siemens Energy, Inc. Tip repair of a turbine component using a composite tip boron base pre-sintered preform
EP3907022A1 (de) 2020-05-08 2021-11-10 Siemens Aktiengesellschaft Verfahren zur herstellung einer materiallage
WO2025121382A1 (ja) * 2023-12-08 2025-06-12 トヨタ自動車株式会社 金属を含む固体、金属を含む固体の製造方法、金属の溶解方法、及び金属鋳物の製造方法

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US4214355A (en) * 1977-12-21 1980-07-29 General Electric Company Method for repairing a turbomachinery blade tip
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US5794338A (en) * 1997-04-04 1998-08-18 General Electric Company Method for repairing a turbine engine member damaged tip
US5822852A (en) * 1997-07-14 1998-10-20 General Electric Company Method for replacing blade tips of directionally solidified and single crystal turbine blades
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US6183689B1 (en) * 1997-11-25 2001-02-06 Penn State Research Foundation Process for sintering powder metal components
US6468040B1 (en) * 2000-07-24 2002-10-22 General Electric Company Environmentally resistant squealer tips and method for making
US6558119B2 (en) * 2001-05-29 2003-05-06 General Electric Company Turbine airfoil with separately formed tip and method for manufacture and repair thereof
US20030012677A1 (en) * 2001-07-11 2003-01-16 Senini Robert J. Bi-metallic metal injection molded hand tool and manufacturing method
US20030062660A1 (en) * 2001-10-03 2003-04-03 Beard Bradley D. Process of metal injection molding multiple dissimilar materials to form composite parts
US6908288B2 (en) * 2001-10-31 2005-06-21 General Electric Company Repair of advanced gas turbine blades
JP2003268465A (ja) * 2002-03-12 2003-09-25 Daido Metal Co Ltd 銅系焼結軸受材料の製造方法
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US7278829B2 (en) * 2005-02-09 2007-10-09 General Electric Company Gas turbine blade having a monocrystalline airfoil with a repair squealer tip, and repair method

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