JP2006170204A5 - - Google Patents

Download PDF

Info

Publication number
JP2006170204A5
JP2006170204A5 JP2005358418A JP2005358418A JP2006170204A5 JP 2006170204 A5 JP2006170204 A5 JP 2006170204A5 JP 2005358418 A JP2005358418 A JP 2005358418A JP 2005358418 A JP2005358418 A JP 2005358418A JP 2006170204 A5 JP2006170204 A5 JP 2006170204A5
Authority
JP
Japan
Prior art keywords
inner band
segment
vane
band
replacement inner
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
JP2005358418A
Other languages
English (en)
Japanese (ja)
Other versions
JP2006170204A (ja
Filing date
Publication date
Priority claimed from US11/015,611 external-priority patent/US7185433B2/en
Application filed filed Critical
Publication of JP2006170204A publication Critical patent/JP2006170204A/ja
Publication of JP2006170204A5 publication Critical patent/JP2006170204A5/ja
Pending legal-status Critical Current

Links

JP2005358418A 2004-12-17 2005-12-13 タービンノズルセグメント及びその修理方法 Pending JP2006170204A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/015,611 US7185433B2 (en) 2004-12-17 2004-12-17 Turbine nozzle segment and method of repairing same

Publications (2)

Publication Number Publication Date
JP2006170204A JP2006170204A (ja) 2006-06-29
JP2006170204A5 true JP2006170204A5 (enExample) 2009-01-29

Family

ID=36084183

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2005358418A Pending JP2006170204A (ja) 2004-12-17 2005-12-13 タービンノズルセグメント及びその修理方法

Country Status (6)

Country Link
US (1) US7185433B2 (enExample)
EP (1) EP1674665B2 (enExample)
JP (1) JP2006170204A (enExample)
BR (1) BRPI0505694B1 (enExample)
CA (1) CA2529337C (enExample)
SG (1) SG123728A1 (enExample)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7434329B2 (en) * 2004-05-27 2008-10-14 Bear Cub Enterprises, Llc Mounting clips for siding boards
ATE486195T1 (de) * 2005-12-22 2010-11-15 Techspace Aero Schaufelleitring einer strömungsmaschine, strömungsmaschine mit einem solchen leitring und leitschaufel
US20080267775A1 (en) * 2007-04-30 2008-10-30 General Electric Company Nozzle segments and method of repairing the same
US8220150B2 (en) * 2007-05-22 2012-07-17 United Technologies Corporation Split vane cluster repair method
US9765622B2 (en) * 2007-09-12 2017-09-19 United Technologies Corporation Methods for performing gas turbine engine casing repairs and repaired cases
US20090113706A1 (en) * 2007-11-06 2009-05-07 General Electric Company Craze crack repair of combustor liners
US8257038B2 (en) * 2008-02-01 2012-09-04 Siemens Energy, Inc. Metal injection joining
US20090274562A1 (en) * 2008-05-02 2009-11-05 United Technologies Corporation Coated turbine-stage nozzle segments
US8206101B2 (en) * 2008-06-16 2012-06-26 General Electric Company Windward cooled turbine nozzle
US20100050407A1 (en) * 2008-08-28 2010-03-04 Buck David A Method of Repairing Tong Jaw
US8210807B2 (en) 2008-08-28 2012-07-03 United Technologies Corporation Gas turbine airfoil assemblies and methods of repair
US8133015B2 (en) * 2008-09-30 2012-03-13 General Electric Company Turbine nozzle for a gas turbine engine
US8047771B2 (en) * 2008-11-17 2011-11-01 Honeywell International Inc. Turbine nozzles and methods of manufacturing the same
US8251651B2 (en) * 2009-01-28 2012-08-28 United Technologies Corporation Segmented ceramic matrix composite turbine airfoil component
US8544173B2 (en) 2010-08-30 2013-10-01 General Electric Company Turbine nozzle biform repair
US9447689B2 (en) * 2011-06-17 2016-09-20 General Electric Company Method of repairing a turbine nozzle segment in a turbine engine
US9745849B2 (en) 2015-06-26 2017-08-29 General Electric Company Methods for treating field operated components
EP3805525A1 (en) * 2019-10-09 2021-04-14 Rolls-Royce plc Turbine vane assembly incorporating ceramic matric composite materials

Family Cites Families (18)

* 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
CA989153A (en) 1972-08-22 1976-05-18 John M. Aartman Guide vane repair
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
US5332360A (en) * 1993-09-08 1994-07-26 General Electric Company Stator vane having reinforced braze joint
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
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
US20030106215A1 (en) * 2001-12-11 2003-06-12 General Electric Company Turbine nozzle segment and method of repairing same
US6793457B2 (en) * 2002-11-15 2004-09-21 General Electric Company Fabricated repair of cast nozzle
US6905308B2 (en) * 2002-11-20 2005-06-14 General Electric Company Turbine nozzle segment and method of repairing same

Similar Documents

Publication Publication Date Title
JP2006170204A5 (enExample)
US8105133B2 (en) Airfoil mask, airfoil and mask system
JP2004169701A5 (enExample)
JP2002168133A5 (enExample)
JP4733306B2 (ja) ろう付け無し隅肉を用いるタービンノズル
JP6452736B2 (ja) 一体的な壁厚制御のためのフィルム孔突出部を用いるタービンブレードインベストメント鋳造
CN104246134B (zh) 包括由铰接接头连接的构件的翼片
US6595749B2 (en) Turbine airfoil and method for manufacture and repair thereof
CA2448465A1 (en) Fabricated repair of cast nozzle
EP1227218A3 (en) Turbine nozzle segment and method of repairing same
JP6240388B2 (ja) 中空cmcバケット用の薄肉強化格子構造体
US9546552B2 (en) Gas turbine
US8915718B2 (en) Airfoil including damper member
US7726938B2 (en) Turbine blade and diaphragm construction
CA2449339A1 (en) Turbine nozzle segment and method of repairing same
JP6002028B2 (ja) スロット付きタービン翼形部
JP2007198293A (ja) 軸流圧縮機の静翼環
EP1207270A3 (en) Repairing method for a turbine nozzle segment
EP1340885A3 (en) Leaf seal support for a gas turbine engine nozzle vane
JP2002355822A5 (enExample)
JP3839389B2 (ja) ベーンの修理方法
JP2008044011A (ja) 鋳造中子および粗鋳造物、シェル、中子の組み合わせ
JP2003106104A5 (enExample)
WO2009025895A3 (en) Modular chevron exhaust nozzle
US10273810B2 (en) Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities