JP2004169701A5 - - Google Patents

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Publication number
JP2004169701A5
JP2004169701A5 JP2003388698A JP2003388698A JP2004169701A5 JP 2004169701 A5 JP2004169701 A5 JP 2004169701A5 JP 2003388698 A JP2003388698 A JP 2003388698A JP 2003388698 A JP2003388698 A JP 2003388698A JP 2004169701 A5 JP2004169701 A5 JP 2004169701A5
Authority
JP
Japan
Prior art keywords
band
inner band
nozzle segment
joining
vane
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
JP2003388698A
Other languages
English (en)
Japanese (ja)
Other versions
JP4020856B2 (ja
JP2004169701A (ja
Filing date
Publication date
Priority claimed from US10/300,098 external-priority patent/US6905308B2/en
Application filed filed Critical
Publication of JP2004169701A publication Critical patent/JP2004169701A/ja
Publication of JP2004169701A5 publication Critical patent/JP2004169701A5/ja
Application granted granted Critical
Publication of JP4020856B2 publication Critical patent/JP4020856B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

JP2003388698A 2002-11-20 2003-11-19 タービンノズルセグメント及びその修理方法 Expired - Fee Related JP4020856B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/300,098 US6905308B2 (en) 2002-11-20 2002-11-20 Turbine nozzle segment and method of repairing same

Publications (3)

Publication Number Publication Date
JP2004169701A JP2004169701A (ja) 2004-06-17
JP2004169701A5 true JP2004169701A5 (enExample) 2007-01-11
JP4020856B2 JP4020856B2 (ja) 2007-12-12

Family

ID=32229860

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003388698A Expired - Fee Related JP4020856B2 (ja) 2002-11-20 2003-11-19 タービンノズルセグメント及びその修理方法

Country Status (7)

Country Link
US (1) US6905308B2 (enExample)
EP (1) EP1422381B1 (enExample)
JP (1) JP4020856B2 (enExample)
BR (1) BR0305810B1 (enExample)
CA (1) CA2449339C (enExample)
DE (1) DE60319492T2 (enExample)
SG (1) SG123573A1 (enExample)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7172389B2 (en) * 2004-11-16 2007-02-06 General Electric Company Method for making a repaired turbine engine stationary vane assembly and repaired assembly
US7185433B2 (en) * 2004-12-17 2007-03-06 General Electric Company Turbine nozzle segment and method of repairing same
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
DE102006034055A1 (de) 2006-07-20 2008-01-24 Mtu Aero Engines Gmbh Verfahren zur Reparatur eines Leitschaufelsegments für ein Strahltriebwerk
US7806650B2 (en) * 2006-08-29 2010-10-05 General Electric Company Method and apparatus for fabricating a nozzle segment for use with turbine engines
US7761990B2 (en) * 2006-09-26 2010-07-27 Pas Technologies, Inc. Method of repairing a stationary airfoil array directing three-dimensional flow
US8220150B2 (en) * 2007-05-22 2012-07-17 United Technologies Corporation Split vane cluster repair method
US7798773B2 (en) * 2007-08-06 2010-09-21 United Technologies Corporation Airfoil replacement repair
US8020295B2 (en) * 2007-10-18 2011-09-20 United Technologies Corp. Methods for dimensionally restoring a fastener for a gas turbine engine
US20090113706A1 (en) * 2007-11-06 2009-05-07 General Electric Company Craze crack repair of combustor liners
US20090274562A1 (en) * 2008-05-02 2009-11-05 United Technologies Corporation Coated turbine-stage nozzle segments
JP5321186B2 (ja) 2009-03-26 2013-10-23 株式会社Ｉｈｉ Ｃｍｃタービン静翼
JP5311126B2 (ja) * 2009-03-26 2013-10-09 株式会社Ｉｈｉ Ｃｍｃタービン静翼
CN101829888A (zh) * 2010-04-15 2010-09-15 上海电气电站设备有限公司 带子午面喷嘴组围带型孔加工方法
US8544173B2 (en) 2010-08-30 2013-10-01 General Electric Company Turbine nozzle biform repair
US8763403B2 (en) 2010-11-19 2014-07-01 United Technologies Corporation Method for use with annular gas turbine engine component
US9447689B2 (en) * 2011-06-17 2016-09-20 General Electric Company Method of repairing a turbine nozzle segment in a turbine engine
US9097124B2 (en) 2012-01-24 2015-08-04 United Technologies Corporation Gas turbine engine stator vane assembly with inner shroud
EP2901022B1 (en) * 2012-09-28 2019-04-24 United Technologies Corporation Turbine engine vane arrangement having a plurality of interconnected vane arrangement segments
CN103612082B (zh) * 2013-11-22 2015-11-18 哈尔滨电机厂有限责任公司 大型水轮机座环加工找正的工艺方法
US9745849B2 (en) 2015-06-26 2017-08-29 General Electric Company Methods for treating field operated components
US10436047B2 (en) * 2015-08-18 2019-10-08 General Electric Company Method for repair of a diaphragm of a rotary machine
US12097555B2 (en) * 2022-05-03 2024-09-24 GM Global Technology Operations LLC Repair ultra-large casting

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3802046A (en) 1972-01-27 1974-04-09 Chromalloy American Corp Method of making or reconditioning a turbine-nozzle or the like assembly
US4305697A (en) 1980-03-19 1981-12-15 General Electric Company Method and replacement member for repairing a gas turbine engine vane assembly
US4326833A (en) 1980-03-19 1982-04-27 General Electric Company Method and replacement member for repairing a gas turbine engine blade member
US5272809A (en) 1990-09-04 1993-12-28 United Technologies Corporation Technique for direct bonding cast and wrought materials
US5269057A (en) 1991-12-24 1993-12-14 Freedom Forge Corporation Method of making replacement airfoil components
US5248240A (en) 1993-02-08 1993-09-28 General Electric Company Turbine stator vane assembly
US5690469A (en) 1996-06-06 1997-11-25 United Technologies Corporation Method and apparatus for replacing a vane assembly in a turbine engine
US5813832A (en) 1996-12-05 1998-09-29 General Electric Company Turbine engine vane segment
US5758416A (en) 1996-12-05 1998-06-02 General Electric Company Method for repairing a turbine engine vane segment
US5797725A (en) 1997-05-23 1998-08-25 Allison Advanced Development Company Gas turbine engine vane and method of manufacture
US6183192B1 (en) 1999-03-22 2001-02-06 General Electric Company Durable turbine nozzle
US6173491B1 (en) 1999-08-12 2001-01-16 Chromalloy Gas Turbine Corporation Method for replacing a turbine vane airfoil
US6154959A (en) 1999-08-16 2000-12-05 Chromalloy Gas Turbine Corporation Laser cladding a turbine engine vane platform
US6416278B1 (en) 2000-11-16 2002-07-09 General Electric Company Turbine nozzle segment and method of repairing same
US6494677B1 (en) * 2001-01-29 2002-12-17 General Electric Company Turbine nozzle segment and method of repairing same

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