JP5487095B2 - マルチノズルドライ低NOx燃焼システムの燃焼ダイナミクスを軽減するための燃料システム音響特性 - Google Patents
マルチノズルドライ低NOx燃焼システムの燃焼ダイナミクスを軽減するための燃料システム音響特性 Download PDFInfo
- Publication number
- JP5487095B2 JP5487095B2 JP2010285235A JP2010285235A JP5487095B2 JP 5487095 B2 JP5487095 B2 JP 5487095B2 JP 2010285235 A JP2010285235 A JP 2010285235A JP 2010285235 A JP2010285235 A JP 2010285235A JP 5487095 B2 JP5487095 B2 JP 5487095B2
- Authority
- JP
- Japan
- Prior art keywords
- downstream
- fuel nozzle
- fuel
- upstream
- orifice
- 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.)
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Links
- 239000000446 fuel Substances 0.000 title claims description 88
- 238000002485 combustion reaction Methods 0.000 title description 16
- 238000011144 upstream manufacturing Methods 0.000 claims description 64
- 239000012530 fluid Substances 0.000 claims description 37
- 230000004323 axial length Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 description 5
- 239000006227 byproduct Substances 0.000 description 3
- 238000013459 approach Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000009940 knitting Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
Images
Classifications
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- 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
- F02C7/22—Fuel supply systems
- F02C7/228—Dividing fuel between various burners
-
- 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
- F02C7/22—Fuel supply systems
-
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/128—Nozzles
-
- 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
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/08—Purpose of the control system to produce clean exhaust gases
- F05D2270/082—Purpose of the control system to produce clean exhaust gases with as little NOx as possible
-
- 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
- F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
-
- 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
- Y10T29/49826—Assembling or joining
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/651,600 | 2010-01-04 | ||
| US12/651,600 US8322140B2 (en) | 2010-01-04 | 2010-01-04 | Fuel system acoustic feature to mitigate combustion dynamics for multi-nozzle dry low NOx combustion system and method |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2011137629A JP2011137629A (ja) | 2011-07-14 |
| JP2011137629A5 JP2011137629A5 (enExample) | 2013-02-07 |
| JP5487095B2 true JP5487095B2 (ja) | 2014-05-07 |
Family
ID=44203224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2010285235A Active JP5487095B2 (ja) | 2010-01-04 | 2010-12-22 | マルチノズルドライ低NOx燃焼システムの燃焼ダイナミクスを軽減するための燃料システム音響特性 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US8322140B2 (enExample) |
| JP (1) | JP5487095B2 (enExample) |
| CN (1) | CN102116478B (enExample) |
| FR (1) | FR2954968B1 (enExample) |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10088165B2 (en) | 2015-04-07 | 2018-10-02 | General Electric Company | System and method for tuning resonators |
| US9303564B2 (en) | 2013-02-27 | 2016-04-05 | General Electric Company | Combustor can temperature control system |
| JP6021705B2 (ja) * | 2013-03-22 | 2016-11-09 | 三菱重工業株式会社 | 燃焼器、および、ガスタービン |
| US20160195271A1 (en) * | 2013-09-23 | 2016-07-07 | Siemens Aktiengesellschaft | Burner for a gas turbine and method for reducing thermoacoustic oscillations in a gas turbine |
| US9964045B2 (en) | 2014-02-03 | 2018-05-08 | General Electric Company | Methods and systems for detecting lean blowout in gas turbine systems |
| US9644845B2 (en) | 2014-02-03 | 2017-05-09 | General Electric Company | System and method for reducing modal coupling of combustion dynamics |
| US9689574B2 (en) | 2014-02-03 | 2017-06-27 | General Electric Company | System and method for reducing modal coupling of combustion dynamics |
| US9709279B2 (en) | 2014-02-27 | 2017-07-18 | General Electric Company | System and method for control of combustion dynamics in combustion system |
| US9709278B2 (en) | 2014-03-12 | 2017-07-18 | General Electric Company | System and method for control of combustion dynamics in combustion system |
| JP6452298B2 (ja) * | 2014-03-25 | 2019-01-16 | 三菱日立パワーシステムズ株式会社 | 噴射ノズル、ガスタービン燃焼器及びガスタービン |
| US9644846B2 (en) * | 2014-04-08 | 2017-05-09 | General Electric Company | Systems and methods for control of combustion dynamics and modal coupling in gas turbine engine |
| US9845956B2 (en) | 2014-04-09 | 2017-12-19 | General Electric Company | System and method for control of combustion dynamics in combustion system |
| US9845732B2 (en) | 2014-05-28 | 2017-12-19 | General Electric Company | Systems and methods for variation of injectors for coherence reduction in combustion system |
| US9551283B2 (en) | 2014-06-26 | 2017-01-24 | General Electric Company | Systems and methods for a fuel pressure oscillation device for reduction of coherence |
| US10113747B2 (en) | 2015-04-15 | 2018-10-30 | General Electric Company | Systems and methods for control of combustion dynamics in combustion system |
| WO2017123619A1 (en) * | 2016-01-13 | 2017-07-20 | General Electric Company | Fuel nozzle assembly for reducing multiple tone combustion dynamics |
| DE102017212616A1 (de) * | 2017-07-21 | 2019-01-24 | Rolls-Royce Deutschland Ltd & Co Kg | Düsenbaugruppe für eine Brennkammer eines Triebwerks |
| US11506125B2 (en) | 2018-08-01 | 2022-11-22 | General Electric Company | Fluid manifold assembly for gas turbine engine |
Family Cites Families (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5321949A (en) * | 1991-07-12 | 1994-06-21 | General Electric Company | Staged fuel delivery system with secondary distribution valve |
| JP2759722B2 (ja) * | 1992-05-20 | 1998-05-28 | 川崎重工業株式会社 | ガスタ−ビンの燃焼制御装置 |
| DE69515931T2 (de) * | 1994-06-10 | 2000-11-02 | General Electric Co., Schenectady | Regelung einer Gasturbinenbrennkammer |
| US5943866A (en) * | 1994-10-03 | 1999-08-31 | General Electric Company | Dynamically uncoupled low NOx combustor having multiple premixers with axial staging |
| JP3578852B2 (ja) * | 1995-12-05 | 2004-10-20 | 東京瓦斯株式会社 | マルチバーナ式燃焼器の燃料供給システム及び該燃料供給システムを持つガスタービン |
| SE9802707L (sv) * | 1998-08-11 | 2000-02-12 | Abb Ab | Brännkammaranordning och förfarande för att reducera inverkan av akustiska trycksvängningar i en brännkammaranordning |
| JP2002531805A (ja) * | 1998-12-08 | 2002-09-24 | シーメンス アクチエンゲゼルシヤフト | 燃焼装置および燃焼方法 |
| DE59810760D1 (de) | 1998-12-15 | 2004-03-18 | Krasnojarskij Politekhn I Kras | Brennkammer mit akustisch gedämpftem Brennstoffversorgungssystem |
| JP3962554B2 (ja) * | 2001-04-19 | 2007-08-22 | 三菱重工業株式会社 | ガスタービン燃焼器及びガスタービン |
| US6820431B2 (en) * | 2002-10-31 | 2004-11-23 | General Electric Company | Acoustic impedance-matched fuel nozzle device and tunable fuel injection resonator assembly |
| US7464552B2 (en) | 2004-07-02 | 2008-12-16 | Siemens Energy, Inc. | Acoustically stiffened gas-turbine fuel nozzle |
| RU2300702C1 (ru) * | 2006-04-04 | 2007-06-10 | Общество с ограниченной ответственностью "Научно-производственное предприятие "ЭСТ" | Способ сжигания топлива и устройство для его осуществления |
| US7827797B2 (en) * | 2006-09-05 | 2010-11-09 | General Electric Company | Injection assembly for a combustor |
| US20090077945A1 (en) * | 2007-08-24 | 2009-03-26 | Delavan Inc | Variable amplitude double binary valve system for active fuel control |
| US20090111063A1 (en) * | 2007-10-29 | 2009-04-30 | General Electric Company | Lean premixed, radial inflow, multi-annular staged nozzle, can-annular, dual-fuel combustor |
| EP2110602A1 (de) * | 2008-04-16 | 2009-10-21 | Siemens Aktiengesellschaft | Akustiche Teilentkopplung zur Verringerung von selbstinduzierten Flammenschwingungen |
| US7578130B1 (en) * | 2008-05-20 | 2009-08-25 | General Electric Company | Methods and systems for combustion dynamics reduction |
| US8087228B2 (en) * | 2008-09-11 | 2012-01-03 | General Electric Company | Segmented combustor cap |
| US8707707B2 (en) * | 2009-01-07 | 2014-04-29 | General Electric Company | Late lean injection fuel staging configurations |
-
2010
- 2010-01-04 US US12/651,600 patent/US8322140B2/en active Active
- 2010-12-22 JP JP2010285235A patent/JP5487095B2/ja active Active
-
2011
- 2011-01-03 FR FR1150009A patent/FR2954968B1/fr not_active Expired - Fee Related
- 2011-01-04 CN CN201110005811.7A patent/CN102116478B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN102116478A (zh) | 2011-07-06 |
| US8322140B2 (en) | 2012-12-04 |
| FR2954968A1 (fr) | 2011-07-08 |
| CN102116478B (zh) | 2014-12-31 |
| JP2011137629A (ja) | 2011-07-14 |
| US20110162370A1 (en) | 2011-07-07 |
| FR2954968B1 (fr) | 2021-07-23 |
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