CN104515146B - 内部冷却的过渡管后架 - Google Patents
内部冷却的过渡管后架 Download PDFInfo
- Publication number
- CN104515146B CN104515146B CN201410497839.0A CN201410497839A CN104515146B CN 104515146 B CN104515146 B CN 104515146B CN 201410497839 A CN201410497839 A CN 201410497839A CN 104515146 B CN104515146 B CN 104515146B
- Authority
- CN
- China
- Prior art keywords
- cooling duct
- outlet
- frame
- coupling tube
- conduit
- 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 - Fee Related
Links
- 230000007704 transition Effects 0.000 title claims abstract description 29
- 238000001816 cooling Methods 0.000 claims abstract description 106
- 239000012530 fluid Substances 0.000 claims abstract description 74
- 238000004891 communication Methods 0.000 claims abstract description 25
- 230000008878 coupling Effects 0.000 claims description 59
- 238000010168 coupling process Methods 0.000 claims description 59
- 238000005859 coupling reaction Methods 0.000 claims description 59
- 238000002485 combustion reaction Methods 0.000 claims description 44
- 239000000446 fuel Substances 0.000 claims description 27
- 239000000567 combustion gas Substances 0.000 claims description 25
- 239000007789 gas Substances 0.000 claims description 24
- 238000011144 upstream manufacturing Methods 0.000 claims description 16
- 125000004122 cyclic group Chemical group 0.000 claims description 5
- 230000006835 compression Effects 0.000 description 28
- 238000007906 compression Methods 0.000 description 28
- 238000004519 manufacturing process Methods 0.000 description 6
- 238000007599 discharging Methods 0.000 description 5
- 230000004888 barrier function Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 3
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 description 2
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000012447 hatching Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000000523 sample Substances 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 241000270295 Serpentes Species 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000009760 electrical discharge machining Methods 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000007639 printing Methods 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 238000013396 workstream Methods 0.000 description 1
Classifications
-
- 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
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
-
- 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
- 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
- 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
-
- 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
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
-
- 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
- F23R2900/03043—Convection cooled combustion chamber walls with means for guiding the cooling air flow
-
- 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
- F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies
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 |
|---|---|---|---|
| US14/036101 | 2013-09-25 | ||
| US14/036,101 US9574498B2 (en) | 2013-09-25 | 2013-09-25 | Internally cooled transition duct aft frame with serpentine cooling passage and conduit |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104515146A CN104515146A (zh) | 2015-04-15 |
| CN104515146B true CN104515146B (zh) | 2019-04-09 |
Family
ID=52623741
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410497839.0A Expired - Fee Related CN104515146B (zh) | 2013-09-25 | 2014-09-25 | 内部冷却的过渡管后架 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9574498B2 (enExample) |
| JP (1) | JP6431730B2 (enExample) |
| CN (1) | CN104515146B (enExample) |
| CH (1) | CH708646A2 (enExample) |
| DE (1) | DE102014113326A1 (enExample) |
Families Citing this family (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6289887B1 (en) | 1998-08-07 | 2001-09-18 | Portafire, Inc. | Artificial campfire device |
| EP3325887A1 (en) * | 2015-07-24 | 2018-05-30 | Siemens Aktiengesellschaft | Gas turbine transition duct with late lean injection having reduced combustion residence time |
| US9989260B2 (en) * | 2015-12-22 | 2018-06-05 | General Electric Company | Staged fuel and air injection in combustion systems of gas turbines |
| US11493066B2 (en) * | 2016-01-20 | 2022-11-08 | Soliton Holdings | Generalized jet-effect and enhanced devices |
| JP6584687B2 (ja) | 2016-03-01 | 2019-10-02 | シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ | ガスタービンエンジン内の圧縮機組立体の下流側のミッドフレームトルクディスク用の圧縮機ブリード冷却システム |
| US10830142B2 (en) * | 2016-10-10 | 2020-11-10 | General Electric Company | Combustor aft frame cooling |
| US10577957B2 (en) * | 2017-10-13 | 2020-03-03 | General Electric Company | Aft frame assembly for gas turbine transition piece |
| US11215072B2 (en) | 2017-10-13 | 2022-01-04 | General Electric Company | Aft frame assembly for gas turbine transition piece |
| US10684016B2 (en) | 2017-10-13 | 2020-06-16 | 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 |
| US11092339B2 (en) * | 2018-01-12 | 2021-08-17 | Raytheon Technologies Corporation | Apparatus and method for mitigating particulate accumulation on a component of a gas turbine |
| US11614233B2 (en) | 2020-08-31 | 2023-03-28 | General Electric Company | Impingement panel support structure and method of manufacture |
| US11371702B2 (en) | 2020-08-31 | 2022-06-28 | General Electric Company | Impingement panel for a turbomachine |
| US11994293B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus support structure and method of manufacture |
| US11994292B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus for turbomachine |
| US11460191B2 (en) | 2020-08-31 | 2022-10-04 | General Electric Company | Cooling insert for a turbomachine |
| US11255545B1 (en) | 2020-10-26 | 2022-02-22 | General Electric Company | Integrated combustion nozzle having a unified head end |
| US11767766B1 (en) | 2022-07-29 | 2023-09-26 | General Electric Company | Turbomachine airfoil having impingement cooling passages |
| CA3222070A1 (en) * | 2022-12-14 | 2024-06-14 | Cenovus Energy Inc. | Modified allam cycle system and method for hydrocarbon recovery steam generation |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6568187B1 (en) * | 2001-12-10 | 2003-05-27 | Power Systems Mfg, Llc | Effusion cooled transition duct |
| CN101629520A (zh) * | 2008-07-07 | 2010-01-20 | 通用电气公司 | 燃烧器过渡件后端冷却和相关方法 |
| CN101644191A (zh) * | 2008-08-06 | 2010-02-10 | 通用电气公司 | 过渡管路后端构架的冷却及相关方法 |
| CN102679402A (zh) * | 2011-03-16 | 2012-09-19 | 通用电气公司 | 后架以及用于冷却后架的方法 |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4195474A (en) * | 1977-10-17 | 1980-04-01 | General Electric Company | Liquid-cooled transition member to turbine inlet |
| JPS62150453U (enExample) * | 1986-03-14 | 1987-09-24 | ||
| US5414999A (en) | 1993-11-05 | 1995-05-16 | General Electric Company | Integral aft frame mount for a gas turbine combustor transition piece |
| US5906093A (en) * | 1997-02-21 | 1999-05-25 | Siemens Westinghouse Power Corporation | Gas turbine combustor transition |
| JP3310900B2 (ja) * | 1997-04-15 | 2002-08-05 | 三菱重工業株式会社 | 燃焼器尾筒の冷却構造 |
| 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 |
| 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 |
| US6619915B1 (en) | 2002-08-06 | 2003-09-16 | Power Systems Mfg, Llc | Thermally free aft frame for a transition duct |
| US6662567B1 (en) | 2002-08-14 | 2003-12-16 | Power Systems Mfg, Llc | Transition duct mounting system |
| US7178340B2 (en) | 2003-09-24 | 2007-02-20 | Power Systems Mfg., Llc | Transition duct honeycomb seal |
| US7178341B2 (en) * | 2004-06-17 | 2007-02-20 | Siemens Power Generation, Inc. | Multi-zone tubing assembly for a transition piece of a gas turbine |
| US8015818B2 (en) * | 2005-02-22 | 2011-09-13 | Siemens Energy, Inc. | Cooled transition duct for a gas turbine engine |
| US7789626B1 (en) * | 2007-05-31 | 2010-09-07 | Florida Turbine Technologies, Inc. | Turbine blade with showerhead film cooling holes |
| US8418474B2 (en) | 2008-01-29 | 2013-04-16 | Alstom Technology Ltd. | Altering a natural frequency of a gas turbine transition duct |
| US8707705B2 (en) * | 2009-09-03 | 2014-04-29 | General Electric Company | Impingement cooled transition piece aft frame |
| JP2012145098A (ja) * | 2010-12-21 | 2012-08-02 | Toshiba Corp | トランジションピースおよびガスタービン |
| US20120186260A1 (en) | 2011-01-25 | 2012-07-26 | General Electric Company | Transition piece impingement sleeve for a gas turbine |
-
2013
- 2013-09-25 US US14/036,101 patent/US9574498B2/en not_active Expired - Fee Related
-
2014
- 2014-09-16 JP JP2014187179A patent/JP6431730B2/ja not_active Expired - Fee Related
- 2014-09-16 DE DE102014113326.9A patent/DE102014113326A1/de not_active Ceased
- 2014-09-19 CH CH01421/14A patent/CH708646A2/de not_active Application Discontinuation
- 2014-09-25 CN CN201410497839.0A patent/CN104515146B/zh not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6568187B1 (en) * | 2001-12-10 | 2003-05-27 | Power Systems Mfg, Llc | Effusion cooled transition duct |
| CN101629520A (zh) * | 2008-07-07 | 2010-01-20 | 通用电气公司 | 燃烧器过渡件后端冷却和相关方法 |
| CN101644191A (zh) * | 2008-08-06 | 2010-02-10 | 通用电气公司 | 过渡管路后端构架的冷却及相关方法 |
| CN102679402A (zh) * | 2011-03-16 | 2012-09-19 | 通用电气公司 | 后架以及用于冷却后架的方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| US9574498B2 (en) | 2017-02-21 |
| DE102014113326A1 (de) | 2015-03-26 |
| US20150082795A1 (en) | 2015-03-26 |
| JP2015063994A (ja) | 2015-04-09 |
| CH708646A2 (de) | 2015-03-31 |
| CN104515146A (zh) | 2015-04-15 |
| JP6431730B2 (ja) | 2018-11-28 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240102 Address after: Swiss Baden Patentee after: GENERAL ELECTRIC CO. LTD. Address before: New York State, USA Patentee before: General Electric Co. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190409 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |