SG97216A1 - Turbine nozzle segment and method of repairing same - Google Patents
Turbine nozzle segment and method of repairing sameInfo
- Publication number
- SG97216A1 SG97216A1 SG200106880A SG200106880A SG97216A1 SG 97216 A1 SG97216 A1 SG 97216A1 SG 200106880 A SG200106880 A SG 200106880A SG 200106880 A SG200106880 A SG 200106880A SG 97216 A1 SG97216 A1 SG 97216A1
- Authority
- SG
- Singapore
- Prior art keywords
- turbine nozzle
- nozzle segment
- repairing same
- repairing
- same
- Prior art date
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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
-
- 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
- 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
- F05D2230/10—Manufacture by removing material
- F05D2230/12—Manufacture by removing material by spark erosion methods
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
- F05D2230/237—Brazing
-
- 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
- Y10T29/49318—Repairing or disassembling
-
- 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
- Y10T29/49721—Repairing with disassembling
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/713,936 US6416278B1 (en) | 2000-11-16 | 2000-11-16 | Turbine nozzle segment and method of repairing same |
Publications (1)
Publication Number | Publication Date |
---|---|
SG97216A1 true SG97216A1 (en) | 2003-07-18 |
Family
ID=24868140
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200106880A SG97216A1 (en) | 2000-11-16 | 2001-11-08 | Turbine nozzle segment and method of repairing same |
Country Status (10)
Country | Link |
---|---|
US (1) | US6416278B1 (de) |
EP (1) | EP1207270B1 (de) |
JP (1) | JP4097419B2 (de) |
KR (1) | KR100672134B1 (de) |
CN (1) | CN100467200C (de) |
BR (1) | BR0105227B1 (de) |
DE (1) | DE60126723T2 (de) |
MX (1) | MXPA01011698A (de) |
PL (1) | PL202702B1 (de) |
SG (1) | SG97216A1 (de) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3846169B2 (ja) * | 2000-09-14 | 2006-11-15 | 株式会社日立製作所 | ガスタービンの補修方法 |
US6685431B2 (en) * | 2001-10-24 | 2004-02-03 | United Technologies Corporation | Method for repairing a turbine vane |
GB2388161A (en) * | 2002-05-02 | 2003-11-05 | Rolls Royce Plc | Gas turbine engine compressor casing |
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 |
US6892931B2 (en) * | 2002-12-27 | 2005-05-17 | General Electric Company | Methods for replacing portions of turbine shroud supports |
US20050135923A1 (en) * | 2003-12-22 | 2005-06-23 | Todd Coons | Cooled vane cluster |
US7296615B2 (en) * | 2004-05-06 | 2007-11-20 | General Electric Company | Method and apparatus for determining the location of core-generated features in an investment casting |
US7186070B2 (en) * | 2004-10-12 | 2007-03-06 | Honeywell International, Inc. | Method for modifying gas turbine nozzle area |
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 |
US7434383B2 (en) * | 2005-05-12 | 2008-10-14 | Honeywell International Inc. | Bypass duct boss repair technology |
US7578164B2 (en) * | 2005-09-22 | 2009-08-25 | General Electric Company | Method and apparatus for inspecting turbine nozzle segments |
US7743497B2 (en) * | 2005-10-06 | 2010-06-29 | General Electric Company | Method of providing non-uniform stator vane spacing in a compressor |
US20070274854A1 (en) * | 2006-05-23 | 2007-11-29 | General Electric Company | Method of making metallic composite foam components |
US7845549B2 (en) * | 2006-05-31 | 2010-12-07 | General Electric Company | MIM braze preforms |
US20070295785A1 (en) * | 2006-05-31 | 2007-12-27 | General Electric Company | Microwave brazing using mim preforms |
US7837437B2 (en) * | 2007-03-07 | 2010-11-23 | General Electric Company | Turbine nozzle segment and repair method |
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 |
US8182229B2 (en) * | 2008-01-14 | 2012-05-22 | General Electric Company | Methods and apparatus to repair a rotor disk for a gas turbine |
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 |
US8245399B2 (en) * | 2009-01-20 | 2012-08-21 | United Technologies Corporation | Replacement of part of engine case with dissimilar material |
US9506355B2 (en) * | 2009-12-14 | 2016-11-29 | Snecma | Turbine engine blade or vane made of composite material, turbine nozzle or compressor stator incorporating such vanes and method of fabricating same |
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 |
US8920117B2 (en) * | 2011-10-07 | 2014-12-30 | Pratt & Whitney Canada Corp. | Fabricated gas turbine duct |
US9631517B2 (en) | 2012-12-29 | 2017-04-25 | United Technologies Corporation | Multi-piece fairing for monolithic turbine exhaust case |
WO2014143301A1 (en) | 2013-03-15 | 2014-09-18 | United Technologies Corporation | Multi-airfoil split and rejion method to produce enhanced durability coating |
WO2014143263A1 (en) * | 2013-03-15 | 2014-09-18 | United Technologies Corporation | Multi-airfoil split and rejoin method |
WO2014143285A1 (en) * | 2013-03-15 | 2014-09-18 | United Technologies Corporation | Datum transfer apparatus and method for inspecting coated components |
CN105436639A (zh) * | 2014-08-13 | 2016-03-30 | 常州兰翔机械有限责任公司 | 适于电脉冲加工锁片槽的电极装置及加工方法 |
US10436047B2 (en) | 2015-08-18 | 2019-10-08 | General Electric Company | Method for repair of a diaphragm of a rotary machine |
JP6033391B1 (ja) | 2015-11-24 | 2016-11-30 | 三菱日立パワーシステムズ株式会社 | ガスタービンの運転制御方法、改装方法、及びガスタービン制御装置の設定変更方法 |
US10502220B2 (en) * | 2016-07-22 | 2019-12-10 | Solar Turbines Incorporated | Method for improving turbine compressor performance |
US20180216464A1 (en) * | 2017-01-31 | 2018-08-02 | General Electric Company | Method of repairing a blisk |
CN107953064B (zh) * | 2017-11-08 | 2019-07-05 | 师宗煤焦化工有限公司 | 一种半开式叶轮的修复方法 |
US10738659B2 (en) * | 2018-05-25 | 2020-08-11 | Solar Turbines Incorporated | Turbine nozzle port seal for machining |
CN111206964A (zh) * | 2018-11-22 | 2020-05-29 | 中发天信(北京)航空发动机科技股份有限公司 | 一种整体铸造航空发动机涡轮导向器及其制备方法 |
Citations (3)
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 |
US5269057A (en) * | 1991-12-24 | 1993-12-14 | Freedom Forge Corporation | Method of making replacement airfoil components |
US5272809A (en) * | 1990-09-04 | 1993-12-28 | United Technologies Corporation | Technique for direct bonding cast and wrought materials |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3909157A (en) * | 1972-01-27 | 1975-09-30 | Chromalloy American Corp | Turbine nozzle-vane construction |
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 |
US4883216A (en) * | 1988-03-28 | 1989-11-28 | General Electric Company | Method for bonding an article projection |
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 |
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 |
-
2000
- 2000-11-16 US US09/713,936 patent/US6416278B1/en not_active Expired - Lifetime
-
2001
- 2001-11-08 SG SG200106880A patent/SG97216A1/en unknown
- 2001-11-13 EP EP01309572A patent/EP1207270B1/de not_active Expired - Lifetime
- 2001-11-13 DE DE60126723T patent/DE60126723T2/de not_active Expired - Lifetime
- 2001-11-14 BR BRPI0105227-6A patent/BR0105227B1/pt not_active IP Right Cessation
- 2001-11-15 KR KR1020010070927A patent/KR100672134B1/ko active IP Right Grant
- 2001-11-15 MX MXPA01011698A patent/MXPA01011698A/es active IP Right Grant
- 2001-11-15 JP JP2001349511A patent/JP4097419B2/ja not_active Expired - Fee Related
- 2001-11-16 CN CNB011374853A patent/CN100467200C/zh not_active Expired - Fee Related
- 2001-11-16 PL PL350714A patent/PL202702B1/pl unknown
Patent Citations (3)
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 |
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 |
Also Published As
Publication number | Publication date |
---|---|
PL202702B1 (pl) | 2009-07-31 |
EP1207270A3 (de) | 2004-01-28 |
MXPA01011698A (es) | 2005-04-19 |
JP2002168133A (ja) | 2002-06-14 |
PL350714A1 (en) | 2002-05-20 |
EP1207270B1 (de) | 2007-02-21 |
BR0105227A (pt) | 2002-06-25 |
CN100467200C (zh) | 2009-03-11 |
US6416278B1 (en) | 2002-07-09 |
EP1207270A2 (de) | 2002-05-22 |
BR0105227B1 (pt) | 2010-06-15 |
DE60126723D1 (de) | 2007-04-05 |
CN1354066A (zh) | 2002-06-19 |
DE60126723T2 (de) | 2007-11-22 |
KR20020038512A (ko) | 2002-05-23 |
JP4097419B2 (ja) | 2008-06-11 |
KR100672134B1 (ko) | 2007-01-19 |
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