JP2014181701A - ガスタービン燃焼器の燃焼モジュールのための流れスリーブ組立体 - Google Patents
ガスタービン燃焼器の燃焼モジュールのための流れスリーブ組立体 Download PDFInfo
- Publication number
- JP2014181701A JP2014181701A JP2014048294A JP2014048294A JP2014181701A JP 2014181701 A JP2014181701 A JP 2014181701A JP 2014048294 A JP2014048294 A JP 2014048294A JP 2014048294 A JP2014048294 A JP 2014048294A JP 2014181701 A JP2014181701 A JP 2014181701A
- Authority
- JP
- Japan
- Prior art keywords
- sleeve
- flow sleeve
- annular
- flow
- assembly
- 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.)
- Pending
Links
- 238000002485 combustion reaction Methods 0.000 title claims description 84
- 239000000446 fuel Substances 0.000 claims description 92
- 238000002347 injection Methods 0.000 claims description 20
- 239000007924 injection Substances 0.000 claims description 20
- 238000001816 cooling Methods 0.000 claims description 17
- 238000011144 upstream manufacturing Methods 0.000 claims description 11
- 230000004323 axial length Effects 0.000 claims description 5
- 239000007787 solid Substances 0.000 claims 1
- 239000012530 fluid Substances 0.000 description 28
- 239000007789 gas Substances 0.000 description 23
- 230000007704 transition Effects 0.000 description 9
- 239000000567 combustion gas Substances 0.000 description 6
- 238000004891 communication Methods 0.000 description 5
- 239000003570 air Substances 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 238000003466 welding Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000012080 ambient air Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- VEMKTZHHVJILDY-UHFFFAOYSA-N resmethrin Chemical compound CC1(C)C(C=C(C)C)C1C(=O)OCC1=COC(CC=2C=CC=CC=2)=C1 VEMKTZHHVJILDY-UHFFFAOYSA-N 0.000 description 1
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
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
- F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
-
- 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
- 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
- F23R3/42—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
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 |
|---|---|---|---|
| US13/845,378 | 2013-03-18 | ||
| US13/845,378 US9322556B2 (en) | 2013-03-18 | 2013-03-18 | Flow sleeve assembly for a combustion module of a gas turbine combustor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2014181701A true JP2014181701A (ja) | 2014-09-29 |
| JP2014181701A5 JP2014181701A5 (enExample) | 2017-03-30 |
Family
ID=51419079
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2014048294A Pending JP2014181701A (ja) | 2013-03-18 | 2014-03-12 | ガスタービン燃焼器の燃焼モジュールのための流れスリーブ組立体 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9322556B2 (enExample) |
| JP (1) | JP2014181701A (enExample) |
| CN (1) | CN104061596A (enExample) |
| CH (1) | CH707853A2 (enExample) |
| DE (1) | DE102014103081A1 (enExample) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2017166479A (ja) * | 2016-03-15 | 2017-09-21 | ゼネラル・エレクトリック・カンパニイ | ガスタービンの流れスリーブの取り付け |
Families Citing this family (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9803555B2 (en) * | 2014-04-23 | 2017-10-31 | General Electric Company | Fuel delivery system with moveably attached fuel tube |
| CN104613499B (zh) * | 2014-12-30 | 2018-10-16 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 一种燃气轮机过渡段结构及燃气轮机 |
| US10066837B2 (en) | 2015-02-20 | 2018-09-04 | General Electric Company | Combustor aft mount assembly |
| EP3088691B1 (en) * | 2015-04-27 | 2019-06-19 | Ansaldo Energia Switzerland AG | Gas turbine disassembly method |
| US10088167B2 (en) * | 2015-06-15 | 2018-10-02 | General Electric Company | Combustion flow sleeve lifting tool |
| US10337736B2 (en) * | 2015-07-24 | 2019-07-02 | Pratt & Whitney Canada Corp. | Gas turbine engine combustor and method of forming same |
| WO2017018982A1 (en) * | 2015-07-24 | 2017-02-02 | Siemens Aktiengesellschaft | Gas turbine transition duct with late lean injection having reduced combustion residence time |
| US10228141B2 (en) | 2016-03-04 | 2019-03-12 | General Electric Company | Fuel supply conduit assemblies |
| US10203114B2 (en) | 2016-03-04 | 2019-02-12 | General Electric Company | Sleeve assemblies and methods of fabricating same |
| US10215039B2 (en) * | 2016-07-12 | 2019-02-26 | Siemens Energy, Inc. | Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine |
| US10513987B2 (en) | 2016-12-30 | 2019-12-24 | General Electric Company | System for dissipating fuel egress in fuel supply conduit assemblies |
| US10851999B2 (en) | 2016-12-30 | 2020-12-01 | General Electric Company | Fuel injectors and methods of use in gas turbine combustor |
| US10865992B2 (en) | 2016-12-30 | 2020-12-15 | General Electric Company | Fuel injectors and methods of use in gas turbine combustor |
| US10816208B2 (en) | 2017-01-20 | 2020-10-27 | General Electric Company | Fuel injectors and methods of fabricating same |
| EP3354985B1 (en) * | 2017-01-27 | 2020-11-25 | General Electric Company | Combustion can maintenance apparatus and method |
| US10718523B2 (en) | 2017-05-12 | 2020-07-21 | General Electric Company | Fuel injectors with multiple outlet slots for use in gas turbine combustor |
| US10502426B2 (en) | 2017-05-12 | 2019-12-10 | General Electric Company | Dual fuel injectors and methods of use in gas turbine combustor |
| US20180340689A1 (en) * | 2017-05-25 | 2018-11-29 | General Electric Company | Low Profile Axially Staged Fuel Injector |
| EP3428535A1 (en) * | 2017-07-12 | 2019-01-16 | Siemens Aktiengesellschaft | A combustor triple liner assembly for gas turbine engines |
| US10690349B2 (en) | 2017-09-01 | 2020-06-23 | General Electric Company | Premixing fuel injectors and methods of use in gas turbine combustor |
| US10578022B2 (en) | 2017-09-25 | 2020-03-03 | Delavan Inc. | Transfer tube assembly of nested tubes and a connecting segment having parallel and offset bores |
| US11371709B2 (en) | 2020-06-30 | 2022-06-28 | General Electric Company | Combustor air flow path |
| US12188658B1 (en) | 2023-07-07 | 2025-01-07 | Ge Infrastructure Technology Llc | Fuel injection assembly for a combustor |
| US12467630B2 (en) | 2023-07-07 | 2025-11-11 | Ge Vernova Infrastructure Technology Llc | Fuel injection assembly having a boss with a serpentine cooling passage |
| US12281793B1 (en) | 2024-01-29 | 2025-04-22 | Ge Infrastructure Technology Llc | Fuel injection assembly for a combustor |
| US12449128B1 (en) | 2024-11-27 | 2025-10-21 | Ge Vernova Infrastructure Technology Llc | Boss for a fuel injection assembly having cooling circuit and combustor provided therewith |
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| JPS60140023A (ja) * | 1983-12-27 | 1985-07-24 | Tocera Eng Co Ltd | ハイベロシテイ−バ−ナ |
| JPH06323544A (ja) * | 1993-05-11 | 1994-11-25 | Toshiba Corp | ガスタービン燃焼器のトランジションピース |
| JP2005077089A (ja) * | 2003-08-28 | 2005-03-24 | General Electric Co <Ge> | 燃焼ダイナミックスを低減するための燃焼ライナキャップ組立体 |
| US20120186260A1 (en) * | 2011-01-25 | 2012-07-26 | General Electric Company | Transition piece impingement sleeve for a gas turbine |
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| US3872664A (en) | 1973-10-15 | 1975-03-25 | United Aircraft Corp | Swirl combustor with vortex burning and mixing |
| US4265615A (en) | 1978-12-11 | 1981-05-05 | United Technologies Corporation | Fuel injection system for low emission burners |
| US4420929A (en) | 1979-01-12 | 1983-12-20 | General Electric Company | Dual stage-dual mode low emission gas turbine combustion system |
| JP2644745B2 (ja) | 1987-03-06 | 1997-08-25 | 株式会社日立製作所 | ガスタービン用燃焼器 |
| CA2070511C (en) | 1991-07-22 | 2001-08-21 | Steven Milo Toborg | Turbine nozzle support |
| US5271714A (en) | 1992-07-09 | 1993-12-21 | General Electric Company | Turbine nozzle support arrangement |
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| GB9325708D0 (en) | 1993-12-16 | 1994-02-16 | Rolls Royce Plc | A gas turbine engine combustion chamber |
| JP2950720B2 (ja) | 1994-02-24 | 1999-09-20 | 株式会社東芝 | ガスタービン燃焼装置およびその燃焼制御方法 |
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| US6047550A (en) | 1996-05-02 | 2000-04-11 | General Electric Co. | Premixing dry low NOx emissions combustor with lean direct injection of gas fuel |
| EP0962874A1 (en) | 1998-06-04 | 1999-12-08 | Asea Brown Boveri AG | Method for designing a flow device |
| GB9813972D0 (en) | 1998-06-30 | 1998-08-26 | Rolls Royce Plc | A combustion chamber |
| US6212870B1 (en) | 1998-09-22 | 2001-04-10 | General Electric Company | Self fixturing combustor dome assembly |
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| US20030039542A1 (en) | 2001-08-21 | 2003-02-27 | Cromer Robert Harold | Transition piece side sealing element and turbine assembly containing such seal |
| JP2004125379A (ja) | 2002-07-29 | 2004-04-22 | Miura Co Ltd | 低NOx燃焼方法とその装置 |
| EP1439349A1 (de) | 2003-01-14 | 2004-07-21 | Alstom Technology Ltd | Verbrennungsverfahren sowie Brenner zur Durchführung des Verfahrens |
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| US8601820B2 (en) | 2011-06-06 | 2013-12-10 | General Electric Company | Integrated late lean injection on a combustion liner and late lean injection sleeve assembly |
| US8407892B2 (en) * | 2011-08-05 | 2013-04-02 | General Electric Company | Methods relating to integrating late lean injection into combustion turbine engines |
| US9316155B2 (en) | 2013-03-18 | 2016-04-19 | General Electric Company | System for providing fuel to a combustor |
-
2013
- 2013-03-18 US US13/845,378 patent/US9322556B2/en active Active
-
2014
- 2014-03-07 DE DE201410103081 patent/DE102014103081A1/de active Pending
- 2014-03-12 JP JP2014048294A patent/JP2014181701A/ja active Pending
- 2014-03-17 CH CH00396/14A patent/CH707853A2/de not_active Application Discontinuation
- 2014-03-18 CN CN201410100653.7A patent/CN104061596A/zh active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS60140023A (ja) * | 1983-12-27 | 1985-07-24 | Tocera Eng Co Ltd | ハイベロシテイ−バ−ナ |
| JPH06323544A (ja) * | 1993-05-11 | 1994-11-25 | Toshiba Corp | ガスタービン燃焼器のトランジションピース |
| JP2005077089A (ja) * | 2003-08-28 | 2005-03-24 | General Electric Co <Ge> | 燃焼ダイナミックスを低減するための燃焼ライナキャップ組立体 |
| US20120186260A1 (en) * | 2011-01-25 | 2012-07-26 | General Electric Company | Transition piece impingement sleeve for a gas turbine |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2017166479A (ja) * | 2016-03-15 | 2017-09-21 | ゼネラル・エレクトリック・カンパニイ | ガスタービンの流れスリーブの取り付け |
| JP7109884B2 (ja) | 2016-03-15 | 2022-08-01 | ゼネラル・エレクトリック・カンパニイ | ガスタービンの流れスリーブの取り付け |
Also Published As
| Publication number | Publication date |
|---|---|
| US20140260275A1 (en) | 2014-09-18 |
| CH707853A2 (de) | 2014-09-30 |
| US9322556B2 (en) | 2016-04-26 |
| CN104061596A (zh) | 2014-09-24 |
| DE102014103081A1 (de) | 2014-09-18 |
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