SG11201404771XA - Method for working of combustor float wall panels - Google Patents
Method for working of combustor float wall panelsInfo
- Publication number
- SG11201404771XA SG11201404771XA SG11201404771XA SG11201404771XA SG11201404771XA SG 11201404771X A SG11201404771X A SG 11201404771XA SG 11201404771X A SG11201404771X A SG 11201404771XA SG 11201404771X A SG11201404771X A SG 11201404771XA SG 11201404771X A SG11201404771X A SG 11201404771XA
- Authority
- SG
- Singapore
- Prior art keywords
- working
- wall panels
- float wall
- combustor float
- combustor
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
-
- 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
-
- 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
- B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
- B23P2700/13—Parts of turbine combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00018—Manufacturing combustion chamber liners or subparts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00019—Repairing or maintaining combustion chamber liners or subparts
-
- 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
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine 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
- Y10T29/49348—Burner, torch or metallurgical lance making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/461,283 US8910378B2 (en) | 2012-05-01 | 2012-05-01 | Method for working of combustor float wall panels |
PCT/US2013/036284 WO2013165672A1 (en) | 2012-05-01 | 2013-04-12 | Method for working of combustor float wall panels |
Publications (1)
Publication Number | Publication Date |
---|---|
SG11201404771XA true SG11201404771XA (en) | 2014-11-27 |
Family
ID=49511437
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG11201404771XA SG11201404771XA (en) | 2012-05-01 | 2013-04-12 | Method for working of combustor float wall panels |
Country Status (4)
Country | Link |
---|---|
US (1) | US8910378B2 (en) |
EP (1) | EP2844423B1 (en) |
SG (1) | SG11201404771XA (en) |
WO (1) | WO2013165672A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015112473A1 (en) * | 2014-01-24 | 2015-07-30 | United Technologies Corporation | Additive repair for combustor liner panels |
US10935240B2 (en) | 2015-04-23 | 2021-03-02 | Raytheon Technologies Corporation | Additive manufactured combustor heat shield |
US10443846B2 (en) * | 2016-04-21 | 2019-10-15 | United Technologies Corporation | Combustor thermal shield fabrication method |
US10480788B2 (en) * | 2016-08-16 | 2019-11-19 | United Technologies Corporation | Systems and methods for combustor panel |
US20190072276A1 (en) * | 2017-09-06 | 2019-03-07 | United Technologies Corporation | Float wall combustor panels having heat transfer augmentation |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB624939A (en) * | 1946-07-12 | 1949-06-20 | Bbc Brown Boveri & Cie | Gas turbine combustion chamber |
GB719380A (en) | 1950-11-17 | 1954-12-01 | Power Jets Res & Dev Ltd | Improvements in combustion chambers |
US4302941A (en) * | 1980-04-02 | 1981-12-01 | United Technologies Corporation | Combuster liner construction for gas turbine engine |
JPS60247478A (en) * | 1984-05-24 | 1985-12-07 | Hidetake Washimi | Method for repairing stud bolt of boiler tube |
JPH0660740B2 (en) * | 1985-04-05 | 1994-08-10 | 工業技術院長 | Gas turbine combustor |
GB2204672B (en) * | 1987-05-06 | 1991-03-06 | Rolls Royce Plc | Combustor |
US5461866A (en) * | 1994-12-15 | 1995-10-31 | United Technologies Corporation | Gas turbine engine combustion liner float wall cooling arrangement |
US5542246A (en) * | 1994-12-15 | 1996-08-06 | United Technologies Corporation | Bulkhead cooling fairing |
US6807059B1 (en) * | 1998-12-28 | 2004-10-19 | James L. Dale | Stud welded pin fin heat sink |
GB9926257D0 (en) * | 1999-11-06 | 2000-01-12 | Rolls Royce Plc | Wall elements for gas turbine engine combustors |
US6345441B1 (en) * | 2000-07-18 | 2002-02-12 | General Electric Company | Method of repairing combustion chamber liners |
US6581285B2 (en) | 2001-06-11 | 2003-06-24 | General Electric Co. | Methods for replacing nuggeted combustor liner panels |
US6532656B1 (en) * | 2001-10-10 | 2003-03-18 | General Electric Company | Gas turbine engine compressor blade restoration method |
US6986201B2 (en) * | 2002-12-04 | 2006-01-17 | General Electric Company | Methods for replacing combustor liners |
US6904676B2 (en) * | 2002-12-04 | 2005-06-14 | General Electric Company | Methods for replacing a portion of a combustor liner |
US6901758B2 (en) * | 2003-08-08 | 2005-06-07 | General Electric Company | Method for repairing an air cooled combustor liner segment edge portion and repaired segment |
US6994920B2 (en) * | 2003-10-31 | 2006-02-07 | General Electric Company | Fusion welding method and welded article |
US6984102B2 (en) * | 2003-11-19 | 2006-01-10 | General Electric Company | Hot gas path component with mesh and turbulated cooling |
US7546684B2 (en) | 2004-07-27 | 2009-06-16 | General Electric Company | Method for repair and replacement of combustor liner panel |
GB2434199B (en) | 2006-01-14 | 2011-01-05 | Alstom Technology Ltd | Combustor liner with heat shield |
US20090142548A1 (en) * | 2007-10-18 | 2009-06-04 | David Bruce Patterson | Air cooled gas turbine components and methods of manufacturing and repairing the same |
US8510926B2 (en) | 2008-05-05 | 2013-08-20 | United Technologies Corporation | Method for repairing a gas turbine engine component |
JP5821550B2 (en) * | 2011-11-10 | 2015-11-24 | 株式会社Ihi | Combustor liner |
-
2012
- 2012-05-01 US US13/461,283 patent/US8910378B2/en active Active
-
2013
- 2013-04-12 SG SG11201404771XA patent/SG11201404771XA/en unknown
- 2013-04-12 WO PCT/US2013/036284 patent/WO2013165672A1/en active Application Filing
- 2013-04-12 EP EP13785223.2A patent/EP2844423B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
WO2013165672A1 (en) | 2013-11-07 |
US8910378B2 (en) | 2014-12-16 |
EP2844423A4 (en) | 2015-05-06 |
EP2844423A1 (en) | 2015-03-11 |
US20130291382A1 (en) | 2013-11-07 |
EP2844423B1 (en) | 2020-11-18 |
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