JP2001158929A5 - - Google Patents

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Publication number
JP2001158929A5
JP2001158929A5 JP2000303215A JP2000303215A JP2001158929A5 JP 2001158929 A5 JP2001158929 A5 JP 2001158929A5 JP 2000303215 A JP2000303215 A JP 2000303215A JP 2000303215 A JP2000303215 A JP 2000303215A JP 2001158929 A5 JP2001158929 A5 JP 2001158929A5
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JP
Japan
Prior art keywords
weight
less
component
composition
airfoil
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
JP2000303215A
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English (en)
Japanese (ja)
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JP2001158929A (ja
Filing date
Publication date
Priority claimed from US09/411,103 external-priority patent/US6302649B1/en
Application filed filed Critical
Publication of JP2001158929A publication Critical patent/JP2001158929A/ja
Publication of JP2001158929A5 publication Critical patent/JP2001158929A5/ja
Pending legal-status Critical Current

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JP2000303215A 1999-10-04 2000-10-03 超合金溶接組成物および修復されたタービンエンジン部品 Pending JP2001158929A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/411,103 US6302649B1 (en) 1999-10-04 1999-10-04 Superalloy weld composition and repaired turbine engine component
US09/411103 1999-10-04

Publications (2)

Publication Number Publication Date
JP2001158929A JP2001158929A (ja) 2001-06-12
JP2001158929A5 true JP2001158929A5 (enExample) 2007-11-15

Family

ID=23627571

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2000303215A Pending JP2001158929A (ja) 1999-10-04 2000-10-03 超合金溶接組成物および修復されたタービンエンジン部品

Country Status (6)

Country Link
US (1) US6302649B1 (enExample)
EP (1) EP1090710B1 (enExample)
JP (1) JP2001158929A (enExample)
KR (1) KR100757549B1 (enExample)
CZ (1) CZ300494B6 (enExample)
DE (1) DE60028150T2 (enExample)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
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US6464128B1 (en) * 1999-05-28 2002-10-15 General Electric Company Braze repair of a gas turbine engine stationary shroud
US6354799B1 (en) * 1999-10-04 2002-03-12 General Electric Company Superalloy weld composition and repaired turbine engine component
JP2003065068A (ja) * 2001-08-29 2003-03-05 Mitsubishi Heavy Ind Ltd ガスタービン翼頂部の加工孔閉塞方法
US6696176B2 (en) 2002-03-06 2004-02-24 Siemens Westinghouse Power Corporation Superalloy material with improved weldability
US7416697B2 (en) 2002-06-14 2008-08-26 General Electric Company Method for preparing a metallic article having an other additive constituent, without any melting
US7727462B2 (en) * 2002-12-23 2010-06-01 General Electric Company Method for meltless manufacturing of rod, and its use as a welding rod
US6964557B2 (en) * 2003-02-03 2005-11-15 General Electric Company Methods and apparatus for coupling a component to a turbine engine blade
US6933459B2 (en) * 2003-02-03 2005-08-23 General Electric Company Methods and apparatus for fabricating a turbine engine blade
US7009137B2 (en) * 2003-03-27 2006-03-07 Honeywell International, Inc. Laser powder fusion repair of Z-notches with nickel based superalloy powder
US20050139581A1 (en) * 2003-12-24 2005-06-30 Yiping Hu High-strength superalloy joining method for repairing turbine blades
US7531021B2 (en) 2004-11-12 2009-05-12 General Electric Company Article having a dispersion of ultrafine titanium boride particles in a titanium-base matrix
US20060219330A1 (en) * 2005-03-29 2006-10-05 Honeywell International, Inc. Nickel-based superalloy and methods for repairing gas turbine components
JP4546318B2 (ja) * 2005-04-15 2010-09-15 株式会社日立製作所 Ｎｉ基合金部材とその製造法及びタービンエンジン部品並びに溶接材料とその製造法
US20070039176A1 (en) * 2005-08-01 2007-02-22 Kelly Thomas J Method for restoring portion of turbine component
JP5201708B2 (ja) * 2006-04-14 2013-06-05 三菱マテリアル株式会社 Ｎｉ基耐熱合金溶接用ワイヤー
US8618440B2 (en) * 2007-01-04 2013-12-31 Siemens Energy, Inc. Sprayed weld strip for improved weldability
US20080164301A1 (en) * 2007-01-10 2008-07-10 General Electric Company High temperature laser welding
JP4417977B2 (ja) 2007-04-25 2010-02-17 株式会社日立製作所 ガスタービン翼およびその製造方法
JP5248197B2 (ja) * 2008-05-21 2013-07-31 株式会社東芝 Ｎｉ基鋳造合金およびそれを材料とする蒸気タービン用鋳造部品
US8726501B2 (en) * 2009-08-31 2014-05-20 General Electric Company Method of welding single crystal turbine blade tips with an oxidation-resistant filler material
US20110062220A1 (en) * 2009-09-15 2011-03-17 General Electric Company Superalloy composition and method of forming a turbine engine component
US8652650B2 (en) * 2009-10-22 2014-02-18 Honeywell International Inc. Platinum-modified nickel-based superalloys, methods of repairing turbine engine components, and turbine engine components
JP5618643B2 (ja) * 2010-06-14 2014-11-05 株式会社東芝 ガスタービン動翼の補修方法およびガスタービン動翼
US8956700B2 (en) 2011-10-19 2015-02-17 General Electric Company Method for adhering a coating to a substrate structure
WO2014134041A1 (en) 2013-02-28 2014-09-04 United Technologies Corporation System and method low heat weld
US20160263712A1 (en) * 2014-01-24 2016-09-15 United Technologies Corporation Additive repair for combutster liner panels
US9815147B2 (en) * 2014-04-04 2017-11-14 Special Metals Corporation High strength Ni—Cr—Mo—W—Nb—Ti welding product and method of welding and weld deposit using the same
US20160144461A1 (en) * 2014-11-21 2016-05-26 Huntington Alloys Corporation Ni-Cr-Mo-Ta-Nb Welding Filler Metals, Welding Filler Metal Consumables, Weld Deposits, Methods of Making Weld Deposits, and Weldments Thereof
US9987708B2 (en) 2015-03-02 2018-06-05 United Technologies Corporation Automated weld repair of combustor liners
DE102017129218A1 (de) * 2017-12-08 2019-06-13 Vdm Metals International Gmbh Schweisszusatzwerkstoff
EP3990749B1 (en) * 2019-07-30 2025-09-10 Siemens Energy, Inc. Blade for a gas turbine, formed from a nickel- based superalloy and corresponding repair method
JP7669609B2 (ja) * 2020-06-24 2025-04-30 日光金属株式会社 ニッケル基耐熱鋳造合金、それを用いた真空浸炭炉用部材及び焼却炉火格子

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US3650734A (en) 1969-06-16 1972-03-21 Cyclops Corp Wrought welding alloys
US3668023A (en) 1969-06-20 1972-06-06 Peshotan Sohrab Kotval Tantalum-containing precipitation-strengthened nickel-base alloy
JPS5118210A (ja) * 1974-08-05 1976-02-13 Nippon Steel Corp Yosetsukozoyotainetsugokin
JPS5335620A (en) * 1976-09-16 1978-04-03 Mitsubishi Metal Corp Heat-resisting ni base cast alloy
US4117179A (en) * 1976-11-04 1978-09-26 General Electric Company Oxidation corrosion resistant superalloys and coatings
JPS5582737A (en) 1978-12-15 1980-06-21 Hitachi Ltd Gas turbine nozzle material
DE3401711A1 (de) * 1984-01-19 1985-07-25 VEB Edelstahlwerk 8. Mai 1945 Freital, DDR 8210 Freital Verfahren zur herstellung hochwarmfester nickellegierungen im elektronenstrahlofen
JPS60238442A (ja) * 1984-05-14 1985-11-27 Mitsubishi Heavy Ind Ltd 耐熱耐食合金
US4750954A (en) * 1986-09-12 1988-06-14 Inco Alloys International, Inc. High temperature nickel base alloy with improved stability
US5078963A (en) 1990-02-14 1992-01-07 Mallen Ted A Method of preventing fires in engine and exhaust systems using high nickel mallen alloy
JPH07300643A (ja) * 1994-04-27 1995-11-14 Toshiba Corp 耐熱鋳造Ｃｏ基合金
JP3580441B2 (ja) 1994-07-19 2004-10-20 日立金属株式会社 Ｎｉ基超耐熱合金
CZ293486B6 (cs) * 1994-08-24 2004-05-12 Ericksonágaryál Vysoce legovaná slitina na bázi niklu s vysokou odolností proti korozi za horkaŹ monokrystalický výrobek a monokrystalický odlitek
JP3485980B2 (ja) * 1994-10-03 2004-01-13 Ｊｆｅスチール株式会社 ボイラ−用溶接クラッド鋼管の製造方法

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