ATE265287T1 - Verfahren zum ersetzen von turbinenleitschaufeln - Google Patents
Verfahren zum ersetzen von turbinenleitschaufelnInfo
- Publication number
- ATE265287T1 ATE265287T1 AT00952482T AT00952482T ATE265287T1 AT E265287 T1 ATE265287 T1 AT E265287T1 AT 00952482 T AT00952482 T AT 00952482T AT 00952482 T AT00952482 T AT 00952482T AT E265287 T1 ATE265287 T1 AT E265287T1
- Authority
- AT
- Austria
- Prior art keywords
- platforms
- airfoils
- airfoil
- improved
- vane
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 4
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000005266 casting Methods 0.000 abstract 2
- 229910045601 alloy Inorganic materials 0.000 abstract 1
- 239000000956 alloy Substances 0.000 abstract 1
- 230000004075 alteration Effects 0.000 abstract 1
- 238000005219 brazing Methods 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
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
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/005—Repairing methods or devices
-
- 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
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- Y10T29/49318—Repairing or disassembling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Laser Beam Processing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/373,277 US6173491B1 (en) | 1999-08-12 | 1999-08-12 | Method for replacing a turbine vane airfoil |
| PCT/US2000/021273 WO2001012382A1 (en) | 1999-08-12 | 2000-08-04 | Method for replacing a turbine vane airfoil |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE265287T1 true ATE265287T1 (de) | 2004-05-15 |
Family
ID=23471729
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT00952482T ATE265287T1 (de) | 1999-08-12 | 2000-08-04 | Verfahren zum ersetzen von turbinenleitschaufeln |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US6173491B1 (de) |
| EP (1) | EP1212167B1 (de) |
| JP (1) | JP4689120B2 (de) |
| AT (1) | ATE265287T1 (de) |
| AU (1) | AU6517200A (de) |
| CA (1) | CA2383404C (de) |
| DE (1) | DE60010288T2 (de) |
| MX (1) | MXPA02001456A (de) |
| WO (1) | WO2001012382A1 (de) |
Families Citing this family (55)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19831736C2 (de) * | 1998-07-15 | 2000-05-31 | Mtu Muenchen Gmbh | Verfahren zur Reparatur und Herstellung eines integral beschaufelten Rotors für eine Strömungsmaschine |
| US6785961B1 (en) | 1999-11-12 | 2004-09-07 | General Electric Corporation | Turbine nozzle segment and method of repairing same |
| US6341936B1 (en) * | 2000-04-21 | 2002-01-29 | General Electric Company | FOD inspection of laser shock peened gas turbine engine airfoils |
| 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 |
| US6506014B1 (en) * | 2001-07-26 | 2003-01-14 | Advanced Pneumatics Inc. | Foreign material exclusion device |
| US6380512B1 (en) * | 2001-10-09 | 2002-04-30 | Chromalloy Gas Turbine Corporation | Method for removing coating material from a cooling hole of a gas turbine engine component |
| US20030106215A1 (en) * | 2001-12-11 | 2003-06-12 | General Electric Company | Turbine nozzle segment and method of repairing same |
| US7651319B2 (en) * | 2002-02-22 | 2010-01-26 | Drs Power Technology Inc. | Compressor stator vane |
| US6984108B2 (en) * | 2002-02-22 | 2006-01-10 | Drs Power Technology Inc. | Compressor stator vane |
| 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 |
| DE10256414A1 (de) * | 2002-12-02 | 2004-06-09 | Siemens Ag | Verfahren zur Herstellung eines Bauteils |
| US7009137B2 (en) * | 2003-03-27 | 2006-03-07 | Honeywell International, Inc. | Laser powder fusion repair of Z-notches with nickel based superalloy powder |
| US7051435B1 (en) | 2003-06-13 | 2006-05-30 | General Electric Company | Process for repairing turbine components |
| US6927361B2 (en) * | 2003-09-04 | 2005-08-09 | Thomas Joseph Kelly | Surface oxide weld penetration enhancement method and article |
| US20050135923A1 (en) * | 2003-12-22 | 2005-06-23 | Todd Coons | Cooled vane cluster |
| US20050178750A1 (en) * | 2004-02-13 | 2005-08-18 | Kenny Cheng | Repair of article by laser cladding |
| US7381029B2 (en) * | 2004-09-30 | 2008-06-03 | General Electric Company | Multi-piece wind turbine rotor blades and wind turbines incorporating same |
| US7303112B2 (en) * | 2004-10-29 | 2007-12-04 | United Technologies Corporation | Repair of braze joint and article repaired |
| US7185433B2 (en) | 2004-12-17 | 2007-03-06 | General Electric Company | Turbine nozzle segment and method of repairing same |
| US7533698B2 (en) | 2005-08-26 | 2009-05-19 | Advanced Pneumatics Inc. | Trackable, identifiable foreign material exclusion device |
| SG134184A1 (en) * | 2006-01-16 | 2007-08-29 | United Technologies Corp | Chordwidth restoration of a trailing edge of a turbine airfoil by laser clad |
| SG134185A1 (en) * | 2006-01-16 | 2007-08-29 | United Technologies Corp | Turbine platform repair using laser clad |
| DE102006016703A1 (de) * | 2006-04-08 | 2007-10-11 | Mtu Aero Engines Gmbh | Verfahren zur Reparatur eines Leitschaufelsegments |
| US20100236067A1 (en) * | 2006-08-01 | 2010-09-23 | Honeywell International, Inc. | Hybrid welding repair of gas turbine superalloy components |
| US7806650B2 (en) * | 2006-08-29 | 2010-10-05 | General Electric Company | Method and apparatus for fabricating a nozzle segment for use with turbine engines |
| 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 |
| US20090110552A1 (en) * | 2007-10-31 | 2009-04-30 | Anderson Rodger O | Compressor stator vane repair with pin |
| US20090165275A1 (en) * | 2007-12-29 | 2009-07-02 | Michael Scott Cole | Method for repairing a cooled turbine nozzle segment |
| US20090169361A1 (en) * | 2007-12-29 | 2009-07-02 | Michael Scott Cole | Cooled turbine nozzle segment |
| US20090274562A1 (en) * | 2008-05-02 | 2009-11-05 | United Technologies Corporation | Coated turbine-stage nozzle segments |
| US8210807B2 (en) * | 2008-08-28 | 2012-07-03 | United Technologies Corporation | Gas turbine airfoil assemblies and methods of repair |
| US8057178B2 (en) * | 2008-09-04 | 2011-11-15 | General Electric Company | Turbine bucket for a turbomachine and method of reducing bow wave effects at a turbine bucket |
| 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 |
| US20110200838A1 (en) * | 2010-02-18 | 2011-08-18 | Clover Industries, Inc. | Laser clad metal matrix composite compositions and methods |
| US8763403B2 (en) | 2010-11-19 | 2014-07-01 | United Technologies Corporation | Method for use with annular gas turbine engine component |
| US20130004320A1 (en) * | 2011-06-28 | 2013-01-03 | United Technologies Corporation | Method of rotated airfoils |
| US9650905B2 (en) | 2012-08-28 | 2017-05-16 | United Technologies Corporation | Singlet vane cluster assembly |
| US9664111B2 (en) | 2012-12-19 | 2017-05-30 | United Technologies Corporation | Closure of cooling holes with a filing agent |
| US9884343B2 (en) * | 2012-12-20 | 2018-02-06 | United Technologies Corporation | Closure of cooling holes with a filling agent |
| US20140270072A1 (en) * | 2013-03-13 | 2014-09-18 | Robert L. McCormick | Grain size inspection of a gas turbine component by x-ray refraction |
| US10408061B2 (en) * | 2013-03-15 | 2019-09-10 | United Technologies Corporation | Article with sections having different microstructures and method therefor |
| US8967203B2 (en) * | 2013-03-15 | 2015-03-03 | Advanced F.M.E. Products, Inc. | Foreign material exclusion device |
| US9987700B2 (en) | 2014-07-08 | 2018-06-05 | Siemens Energy, Inc. | Magnetically impelled arc butt welding method having magnet arrangement for welding components having complex curvatures |
| GB201413456D0 (en) * | 2014-07-30 | 2014-09-10 | Rolls Royce Plc | Gas turbine engine end-wall component |
| US20160146014A1 (en) * | 2014-11-20 | 2016-05-26 | General Electric Company | Modified bucket platforms of turbine buckets and methods for modifying bucket platforms of turbine buckets |
| DE102017207667A1 (de) | 2017-05-08 | 2018-11-08 | Siemens Aktiengesellschaft | Verfahren zum Instandhalten einer Strömungsmaschine |
| USD878190S1 (en) | 2017-06-19 | 2020-03-17 | Advanced F.M.E. Products, Inc. | Single post retaining member |
| USD877602S1 (en) | 2017-06-19 | 2020-03-10 | Advanced F.M.E. Products, Inc. | Dual post retaining member |
| US10436111B2 (en) | 2017-06-19 | 2019-10-08 | Advanced F.M.E. Products, Inc. | Foreign material exclusion device and retaining member therefor |
| US11339668B2 (en) * | 2018-10-29 | 2022-05-24 | Chromalloy Gas Turbine Llc | Method and apparatus for improving cooling of a turbine shroud |
| US20250345872A1 (en) * | 2024-05-07 | 2025-11-13 | Rtx Corporation | Method of diffusion braze repair of cooling holes and cracks |
Family Cites Families (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3909157A (en) * | 1972-01-27 | 1975-09-30 | Chromalloy American Corp | Turbine nozzle-vane construction |
| US4028787A (en) * | 1975-09-15 | 1977-06-14 | Cretella Salvatore | Refurbished turbine vanes and method of refurbishment thereof |
| US4883216A (en) * | 1988-03-28 | 1989-11-28 | General Electric Company | Method for bonding an article projection |
| US5111570A (en) * | 1990-08-10 | 1992-05-12 | United Technologies Corporation | Forge joining repair technique |
| US5197190A (en) * | 1991-03-04 | 1993-03-30 | United Technologies Corporation | Fabrication of repair method for an integrally bladed rotor |
| US5269057A (en) * | 1991-12-24 | 1993-12-14 | Freedom Forge Corporation | Method of making replacement airfoil components |
| US5285572A (en) * | 1992-08-12 | 1994-02-15 | General Electric Company | Method and system for machining contoured parts |
| NL9300596A (nl) * | 1993-04-05 | 1994-11-01 | Aweta Bv | Werkwijze en inrichting voor het meten van vormparameters van voorwerpen. |
| JPH0710401U (ja) * | 1993-07-22 | 1995-02-14 | 三菱重工業株式会社 | ガスタービン静翼 |
| US5554837A (en) * | 1993-09-03 | 1996-09-10 | Chromalloy Gas Turbine Corporation | Interactive laser welding at elevated temperatures of superalloy articles |
| US5332360A (en) * | 1993-09-08 | 1994-07-26 | General Electric Company | Stator vane having reinforced braze joint |
| US5477026A (en) * | 1994-01-27 | 1995-12-19 | Chromalloy Gas Turbine Corporation | Laser/powdered metal cladding nozzle |
| JP3796758B2 (ja) * | 1994-02-28 | 2006-07-12 | 三菱電機株式会社 | アルミ金型及びその補修方法 |
| DE4411680C1 (de) * | 1994-04-05 | 1995-08-17 | Mtu Muenchen Gmbh | Verfahren zur Reparatur von Fehlstellen in Bauteiloberflächen |
| US5444911A (en) | 1994-05-05 | 1995-08-29 | Chromalloy Gas Turbine Corporation | Gas turbine engine vane assembly repair |
| US5522134A (en) * | 1994-06-30 | 1996-06-04 | United Technologies Corporation | Turbine vane flow area restoration method |
| JPH08284604A (ja) * | 1995-04-14 | 1996-10-29 | Ishikawajima Harima Heavy Ind Co Ltd | ガスタービン翼の補修方法 |
| JPH09168927A (ja) * | 1995-12-19 | 1997-06-30 | Hitachi Ltd | ガスタービン用動翼,静翼の補修方法 |
| JP2851577B2 (ja) * | 1996-02-26 | 1999-01-27 | 三菱重工業株式会社 | ガスタービン静翼シュラウドにおける冷却空気流路の加工方法 |
| US5690469A (en) * | 1996-06-06 | 1997-11-25 | United Technologies Corporation | Method and apparatus for replacing a vane assembly in a turbine engine |
| US5758416A (en) | 1996-12-05 | 1998-06-02 | General Electric Company | Method for repairing a turbine engine vane segment |
| US5732468A (en) | 1996-12-05 | 1998-03-31 | General Electric Company | Method for bonding a turbine engine vane segment |
| US5813832A (en) | 1996-12-05 | 1998-09-29 | General Electric Company | Turbine engine vane segment |
| JPH10184309A (ja) * | 1996-12-26 | 1998-07-14 | Mitsubishi Heavy Ind Ltd | 冷却溝用プラグ蓋の取付方法 |
-
1999
- 1999-08-12 US US09/373,277 patent/US6173491B1/en not_active Expired - Lifetime
-
2000
- 2000-08-04 WO PCT/US2000/021273 patent/WO2001012382A1/en not_active Ceased
- 2000-08-04 AU AU65172/00A patent/AU6517200A/en not_active Abandoned
- 2000-08-04 DE DE60010288T patent/DE60010288T2/de not_active Expired - Lifetime
- 2000-08-04 JP JP2001516710A patent/JP4689120B2/ja not_active Expired - Lifetime
- 2000-08-04 AT AT00952482T patent/ATE265287T1/de not_active IP Right Cessation
- 2000-08-04 CA CA002383404A patent/CA2383404C/en not_active Expired - Lifetime
- 2000-08-04 MX MXPA02001456A patent/MXPA02001456A/es active IP Right Grant
- 2000-08-04 EP EP00952482A patent/EP1212167B1/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| US6173491B1 (en) | 2001-01-16 |
| DE60010288T2 (de) | 2005-05-04 |
| EP1212167B1 (de) | 2004-04-28 |
| JP4689120B2 (ja) | 2011-05-25 |
| DE60010288D1 (de) | 2004-06-03 |
| JP2003507614A (ja) | 2003-02-25 |
| CA2383404A1 (en) | 2001-02-22 |
| CA2383404C (en) | 2006-11-28 |
| EP1212167A1 (de) | 2002-06-12 |
| AU6517200A (en) | 2001-03-13 |
| EP1212167A4 (de) | 2002-11-13 |
| WO2001012382A1 (en) | 2001-02-22 |
| MXPA02001456A (es) | 2003-07-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |