DE60336701D1 - Verfahren zum Ersetzen von Turbinenmantelträgerteilen - Google Patents
Verfahren zum Ersetzen von TurbinenmantelträgerteilenInfo
- Publication number
- DE60336701D1 DE60336701D1 DE60336701T DE60336701T DE60336701D1 DE 60336701 D1 DE60336701 D1 DE 60336701D1 DE 60336701 T DE60336701 T DE 60336701T DE 60336701 T DE60336701 T DE 60336701T DE 60336701 D1 DE60336701 D1 DE 60336701D1
- Authority
- DE
- Germany
- Prior art keywords
- turbine casing
- carrier parts
- casing carrier
- replacing turbine
- replacing
- 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.)
- Expired - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
- B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/80—Repairing, retrofitting or upgrading methods
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49718—Repairing
- Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
- Y10T29/49742—Metallurgically attaching preform
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/330,420 US6892931B2 (en) | 2002-12-27 | 2002-12-27 | Methods for replacing portions of turbine shroud supports |
Publications (1)
Publication Number | Publication Date |
---|---|
DE60336701D1 true DE60336701D1 (de) | 2011-05-26 |
Family
ID=32469042
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60336701T Expired - Lifetime DE60336701D1 (de) | 2002-12-27 | 2003-12-19 | Verfahren zum Ersetzen von Turbinenmantelträgerteilen |
Country Status (7)
Country | Link |
---|---|
US (1) | US6892931B2 (de) |
EP (1) | EP1433565B1 (de) |
JP (1) | JP4588318B2 (de) |
BR (1) | BR0306280B1 (de) |
CA (1) | CA2453026C (de) |
DE (1) | DE60336701D1 (de) |
SG (1) | SG121855A1 (de) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7546684B2 (en) * | 2004-07-27 | 2009-06-16 | General Electric Company | Method for repair and replacement of combustor liner panel |
US7377036B2 (en) * | 2004-10-05 | 2008-05-27 | General Electric Company | Methods for tuning fuel injection assemblies for a gas turbine fuel nozzle |
US20060280610A1 (en) * | 2005-06-13 | 2006-12-14 | Heyward John P | Turbine blade and method of fabricating same |
DE102005055984A1 (de) * | 2005-11-24 | 2007-05-31 | Mtu Aero Engines Gmbh | Verfahren zur Reparatur eines Mantelringsegments einer Gasturbine |
US20080216300A1 (en) * | 2007-03-06 | 2008-09-11 | United Technologies Corporation | Splitter fairing repair |
US9765622B2 (en) * | 2007-09-12 | 2017-09-19 | United Technologies Corporation | Methods for performing gas turbine engine casing repairs and repaired cases |
US8887390B2 (en) | 2008-08-15 | 2014-11-18 | Dresser-Rand Company | Method for correcting downstream deflection in gas turbine nozzles |
US8245399B2 (en) * | 2009-01-20 | 2012-08-21 | United Technologies Corporation | Replacement of part of engine case with dissimilar material |
US8281487B2 (en) * | 2009-01-20 | 2012-10-09 | United Technologies Corporation | Control of case wall growth during repair and method |
US8123474B2 (en) * | 2009-05-12 | 2012-02-28 | Dresser-Rand Company | Repair of industrial gas turbine nozzle diaphragm packing |
US8763403B2 (en) | 2010-11-19 | 2014-07-01 | United Technologies Corporation | Method for use with annular gas turbine engine component |
US20120224960A1 (en) * | 2010-12-30 | 2012-09-06 | Raymond Ruiwen Xu | Gas turbine engine case |
US9145792B2 (en) | 2012-01-31 | 2015-09-29 | General Electric Company | Fixture assembly for repairing a shroud tile of a gas turbine |
US9206702B2 (en) * | 2012-01-31 | 2015-12-08 | General Electric Company | Method for repairing a shroud tile of a gas turbine |
US9291071B2 (en) | 2012-12-03 | 2016-03-22 | United Technologies Corporation | Turbine nozzle baffle |
US9796055B2 (en) * | 2013-02-17 | 2017-10-24 | United Technologies Corporation | Turbine case retention hook with insert |
CA2901191C (en) | 2013-02-25 | 2021-01-19 | General Electric Company | Integral segmented cmc shroud hanger and retainer system |
WO2015047495A2 (en) * | 2013-07-11 | 2015-04-02 | United Technologies Corporation | Flange partial section replacement repair |
GB201616197D0 (en) * | 2016-09-23 | 2016-11-09 | Rolls Royce Plc | Gas turbine engine |
US20190040762A1 (en) | 2017-08-02 | 2019-02-07 | Cummins Inc. | Method and system for nozzle ring repair |
Family Cites Families (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE755567A (fr) | 1969-12-01 | 1971-02-15 | Gen Electric | Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe |
US3907455A (en) | 1974-02-07 | 1975-09-23 | United Technologies Corp | Intermediate compressor case for gas turbine engines |
GB1485032A (en) | 1974-08-23 | 1977-09-08 | Rolls Royce | Gas turbine engine casing |
US4303371A (en) * | 1978-06-05 | 1981-12-01 | General Electric Company | Shroud support with impingement baffle |
US4371311A (en) | 1980-04-28 | 1983-02-01 | United Technologies Corporation | Compression section for an axial flow rotary machine |
US4693667A (en) | 1980-04-29 | 1987-09-15 | Teledyne Industries, Inc. | Turbine inlet nozzle with cooling means |
FR2725474B1 (fr) | 1984-03-14 | 1996-12-13 | Snecma | Aube de distributeur de turbine refroidie |
US4820116A (en) | 1987-09-18 | 1989-04-11 | United Technologies Corporation | Turbine cooling for gas turbine engine |
JP2862536B2 (ja) | 1987-09-25 | 1999-03-03 | 株式会社東芝 | ガスタービンの翼 |
US4844322A (en) * | 1987-10-15 | 1989-07-04 | General Electric Company | Method for replacing a section of tubing |
US5188507A (en) | 1991-11-27 | 1993-02-23 | General Electric Company | Low-pressure turbine shroud |
US5201846A (en) | 1991-11-29 | 1993-04-13 | General Electric Company | Low-pressure turbine heat shield |
US5593276A (en) | 1995-06-06 | 1997-01-14 | General Electric Company | Turbine shroud hanger |
US5593277A (en) | 1995-06-06 | 1997-01-14 | General Electric Company | Smart turbine shroud |
GB2310255B (en) | 1996-02-13 | 1999-06-16 | Rolls Royce Plc | A turbomachine |
US5749701A (en) | 1996-10-28 | 1998-05-12 | General Electric Company | Interstage seal assembly for a turbine |
US5794338A (en) * | 1997-04-04 | 1998-08-18 | General Electric Company | Method for repairing a turbine engine member damaged tip |
JP3316415B2 (ja) | 1997-05-01 | 2002-08-19 | 三菱重工業株式会社 | ガスタービン冷却静翼 |
US5993150A (en) | 1998-01-16 | 1999-11-30 | General Electric Company | Dual cooled shroud |
US6120242A (en) | 1998-11-13 | 2000-09-19 | General Electric Company | Blade containing turbine shroud |
US6435820B1 (en) | 1999-08-25 | 2002-08-20 | General Electric Company | Shroud assembly having C-clip retainer |
US6241471B1 (en) | 1999-08-26 | 2001-06-05 | General Electric Co. | Turbine bucket tip shroud reinforcement |
US6254345B1 (en) | 1999-09-07 | 2001-07-03 | General Electric Company | Internally cooled blade tip shroud |
FR2803871B1 (fr) * | 2000-01-13 | 2002-06-07 | Snecma Moteurs | Agencement de reglage de diametre d'un stator de turbine a gaz |
US6345441B1 (en) * | 2000-07-18 | 2002-02-12 | General Electric Company | Method of repairing combustion chamber liners |
US6367686B1 (en) * | 2000-08-31 | 2002-04-09 | United Technologies Corporation | Self cleaning braze material |
US6416278B1 (en) * | 2000-11-16 | 2002-07-09 | General Electric Company | Turbine nozzle segment and method of repairing same |
US6508000B2 (en) * | 2001-02-08 | 2003-01-21 | Siemens Westinghouse Power Corporation | Transient liquid phase bonding repair for advanced turbine blades and vanes |
US6431820B1 (en) | 2001-02-28 | 2002-08-13 | General Electric Company | Methods and apparatus for cooling gas turbine engine blade tips |
JP3915423B2 (ja) * | 2001-03-29 | 2007-05-16 | 株式会社日立製作所 | ガスタービン燃焼器ライナー構造とその補修方法 |
US6558119B2 (en) * | 2001-05-29 | 2003-05-06 | General Electric Company | Turbine airfoil with separately formed tip and method for manufacture and repair thereof |
US6568079B2 (en) * | 2001-06-11 | 2003-05-27 | General Electric Company | Methods for replacing combustor liner panels |
-
2002
- 2002-12-27 US US10/330,420 patent/US6892931B2/en not_active Expired - Lifetime
-
2003
- 2003-12-11 CA CA002453026A patent/CA2453026C/en not_active Expired - Fee Related
- 2003-12-19 DE DE60336701T patent/DE60336701D1/de not_active Expired - Lifetime
- 2003-12-19 EP EP03258059A patent/EP1433565B1/de not_active Expired - Lifetime
- 2003-12-23 BR BRPI0306280-5A patent/BR0306280B1/pt not_active IP Right Cessation
- 2003-12-25 JP JP2003428680A patent/JP4588318B2/ja not_active Expired - Fee Related
- 2003-12-26 SG SG200307734A patent/SG121855A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
CA2453026A1 (en) | 2004-06-27 |
BR0306280A (pt) | 2004-12-28 |
BR0306280B1 (pt) | 2012-06-26 |
SG121855A1 (en) | 2006-05-26 |
JP2004211697A (ja) | 2004-07-29 |
US20040124229A1 (en) | 2004-07-01 |
EP1433565B1 (de) | 2011-04-13 |
EP1433565A1 (de) | 2004-06-30 |
JP4588318B2 (ja) | 2010-12-01 |
CA2453026C (en) | 2009-06-09 |
US6892931B2 (en) | 2005-05-17 |
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