JP7242237B2 - ガスタービンのトランジションピースのための後部フレームアセンブリ - Google Patents
ガスタービンのトランジションピースのための後部フレームアセンブリ Download PDFInfo
- Publication number
- JP7242237B2 JP7242237B2 JP2018188724A JP2018188724A JP7242237B2 JP 7242237 B2 JP7242237 B2 JP 7242237B2 JP 2018188724 A JP2018188724 A JP 2018188724A JP 2018188724 A JP2018188724 A JP 2018188724A JP 7242237 B2 JP7242237 B2 JP 7242237B2
- Authority
- JP
- Japan
- Prior art keywords
- facing surface
- microchannels
- rear frame
- frame assembly
- downstream
- 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.)
- Active
Links
- 230000007704 transition Effects 0.000 title claims description 47
- 238000001816 cooling Methods 0.000 claims description 63
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- 239000007789 gas Substances 0.000 description 38
- 239000012530 fluid Substances 0.000 description 26
- 238000002485 combustion reaction Methods 0.000 description 20
- 239000000446 fuel Substances 0.000 description 19
- 238000004891 communication Methods 0.000 description 8
- 239000000567 combustion gas Substances 0.000 description 5
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Images
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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
-
- 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
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- 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
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- 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
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
- F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/186—Film cooling
-
- 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
- F02C7/12—Cooling of plants
-
- 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
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/22—Manufacture essentially without removing material by sintering
-
- 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
- F05D2230/90—Coating; Surface treatment
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/204—Heat transfer, e.g. cooling by the use of microcircuits
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 (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/783,291 | 2017-10-13 | ||
| US15/783,291 US10684016B2 (en) | 2017-10-13 | 2017-10-13 | Aft frame assembly for gas turbine transition piece |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2019105437A JP2019105437A (ja) | 2019-06-27 |
| JP2019105437A5 JP2019105437A5 (enExample) | 2022-12-22 |
| JP7242237B2 true JP7242237B2 (ja) | 2023-03-20 |
Family
ID=63722295
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2018188724A Active JP7242237B2 (ja) | 2017-10-13 | 2018-10-04 | ガスタービンのトランジションピースのための後部フレームアセンブリ |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US10684016B2 (enExample) |
| EP (1) | EP3470628B1 (enExample) |
| JP (1) | JP7242237B2 (enExample) |
| KR (1) | KR20190041933A (enExample) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10577957B2 (en) * | 2017-10-13 | 2020-03-03 | General Electric Company | Aft frame assembly for gas turbine transition piece |
| US10718224B2 (en) | 2017-10-13 | 2020-07-21 | General Electric Company | AFT frame assembly for gas turbine transition piece |
| US11859818B2 (en) | 2019-02-25 | 2024-01-02 | General Electric Company | Systems and methods for variable microchannel combustor liner cooling |
| EP3954870B1 (en) * | 2020-08-14 | 2024-02-07 | Ansaldo Energia Switzerland AG | Transition duct for a gas turbine plant and gas turbine plant comprising said transition duct |
| US11187152B1 (en) * | 2020-09-30 | 2021-11-30 | General Electric Company | Turbomachine sealing arrangement having a cooling flow director |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010038166A (ja) | 2008-08-06 | 2010-02-18 | General Electric Co <Ge> | トランジションダクト後方端部フレーム冷却及び関連方法 |
| US20120210720A1 (en) | 2011-02-18 | 2012-08-23 | Mcmahan Kevin Weston | Combustor assembly for use in a turbine engine and methods of fabricating same |
| JP2014009937A (ja) | 2012-06-29 | 2014-01-20 | General Electric Co <Ge> | ガスタービン用移行ダクト |
Family Cites Families (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6412268B1 (en) * | 2000-04-06 | 2002-07-02 | General Electric Company | Cooling air recycling for gas turbine transition duct end frame and related method |
| EP1146289B1 (en) * | 2000-04-13 | 2008-12-24 | Mitsubishi Heavy Industries, Ltd. | Cooling structure of combustor tail tube |
| 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 |
| JP2002243154A (ja) * | 2001-02-16 | 2002-08-28 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器 |
| US20090324387A1 (en) * | 2008-06-30 | 2009-12-31 | General Electric Company | Aft frame with oval-shaped cooling slots and related method |
| US8186167B2 (en) * | 2008-07-07 | 2012-05-29 | General Electric Company | Combustor transition piece aft end cooling and related method |
| US20110162378A1 (en) * | 2010-01-06 | 2011-07-07 | General Electric Company | Tunable transition piece aft frame |
| EP2353763A1 (en) | 2010-02-10 | 2011-08-10 | Siemens Aktiengesellschaft | A method of manufacturing a hot-gas component with a cooling channel by brazing a sintered sheet on a carrier ;corresponding hot-gas component |
| US8651805B2 (en) * | 2010-04-22 | 2014-02-18 | General Electric Company | Hot gas path component cooling system |
| US8499566B2 (en) | 2010-08-12 | 2013-08-06 | General Electric Company | Combustor liner cooling system |
| US9255484B2 (en) | 2011-03-16 | 2016-02-09 | General Electric Company | Aft frame and method for cooling aft frame |
| US8956104B2 (en) | 2011-10-12 | 2015-02-17 | General Electric Company | Bucket assembly for turbine system |
| US9297262B2 (en) | 2012-05-24 | 2016-03-29 | General Electric Company | Cooling structures in the tips of turbine rotor blades |
| US20140360155A1 (en) * | 2013-06-07 | 2014-12-11 | General Electric Company | Microchannel systems and methods for cooling turbine components of a gas turbine engine |
| US9574498B2 (en) * | 2013-09-25 | 2017-02-21 | General Electric Company | Internally cooled transition duct aft frame with serpentine cooling passage and conduit |
| US9909432B2 (en) * | 2013-11-26 | 2018-03-06 | General Electric Company | Gas turbine transition piece aft frame assemblies with cooling channels and methods for manufacturing the same |
| EP3026219B1 (en) * | 2014-11-27 | 2017-07-26 | Ansaldo Energia Switzerland AG | Support segment for a transition piece between combustor and turbine |
| EP3390781B1 (en) | 2015-12-15 | 2020-08-12 | Siemens Aktiengesellschaft | Cooling features for a gas turbine engine transition duct and corresponding method for forming |
| EP3287610B1 (en) * | 2016-08-22 | 2019-07-10 | Ansaldo Energia Switzerland AG | Gas turbine transition duct |
| US10830142B2 (en) * | 2016-10-10 | 2020-11-10 | General Electric Company | Combustor aft frame cooling |
-
2017
- 2017-10-13 US US15/783,291 patent/US10684016B2/en active Active
-
2018
- 2018-10-02 EP EP18198359.4A patent/EP3470628B1/en active Active
- 2018-10-04 JP JP2018188724A patent/JP7242237B2/ja active Active
- 2018-10-11 KR KR1020180121048A patent/KR20190041933A/ko not_active Ceased
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010038166A (ja) | 2008-08-06 | 2010-02-18 | General Electric Co <Ge> | トランジションダクト後方端部フレーム冷却及び関連方法 |
| US20120210720A1 (en) | 2011-02-18 | 2012-08-23 | Mcmahan Kevin Weston | Combustor assembly for use in a turbine engine and methods of fabricating same |
| JP2014009937A (ja) | 2012-06-29 | 2014-01-20 | General Electric Co <Ge> | ガスタービン用移行ダクト |
Also Published As
| Publication number | Publication date |
|---|---|
| KR20190041933A (ko) | 2019-04-23 |
| JP2019105437A (ja) | 2019-06-27 |
| EP3470628A1 (en) | 2019-04-17 |
| US10684016B2 (en) | 2020-06-16 |
| EP3470628B1 (en) | 2020-06-17 |
| US20190113230A1 (en) | 2019-04-18 |
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