JP4958709B2 - 燃焼器音響作用の低減を促進する装置 - Google Patents
燃焼器音響作用の低減を促進する装置 Download PDFInfo
- Publication number
- JP4958709B2 JP4958709B2 JP2007254133A JP2007254133A JP4958709B2 JP 4958709 B2 JP4958709 B2 JP 4958709B2 JP 2007254133 A JP2007254133 A JP 2007254133A JP 2007254133 A JP2007254133 A JP 2007254133A JP 4958709 B2 JP4958709 B2 JP 4958709B2
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- swirler
- main
- elbo
- pilot
- 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
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- 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
- F23R3/34—Feeding into different combustion zones
- F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
-
- 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
-
- 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
- F23R2900/03343—Pilot burners operating in premixed mode
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air Supply (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/537,100 US7631500B2 (en) | 2006-09-29 | 2006-09-29 | Methods and apparatus to facilitate decreasing combustor acoustics |
| US11/537,100 | 2006-09-29 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2008089296A JP2008089296A (ja) | 2008-04-17 |
| JP2008089296A5 JP2008089296A5 (https=) | 2010-11-11 |
| JP4958709B2 true JP4958709B2 (ja) | 2012-06-20 |
Family
ID=38654661
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2007254133A Expired - Fee Related JP4958709B2 (ja) | 2006-09-29 | 2007-09-28 | 燃焼器音響作用の低減を促進する装置 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7631500B2 (https=) |
| EP (1) | EP1909030B1 (https=) |
| JP (1) | JP4958709B2 (https=) |
| CA (1) | CA2603567C (https=) |
Families Citing this family (57)
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| DE102005062079A1 (de) * | 2005-12-22 | 2007-07-12 | Rolls-Royce Deutschland Ltd & Co Kg | Magervormischbrenner mit einer Zerstäuberlippe |
| US8099960B2 (en) * | 2006-11-17 | 2012-01-24 | General Electric Company | Triple counter rotating swirler and method of use |
| US8195292B2 (en) * | 2007-02-16 | 2012-06-05 | Pacestter, Inc. | Cardiac resynchronization therapy optimization using parameter estimation from realtime electrode motion tracking |
| US7905093B2 (en) * | 2007-03-22 | 2011-03-15 | General Electric Company | Apparatus to facilitate decreasing combustor acoustics |
| EP2042807A1 (de) * | 2007-09-25 | 2009-04-01 | Siemens Aktiengesellschaft | Vormischstufe für einen Gasturbinenbrenner |
| US9188341B2 (en) * | 2008-04-11 | 2015-11-17 | General Electric Company | Fuel nozzle |
| US8019409B2 (en) * | 2008-06-09 | 2011-09-13 | Pacesetter, Inc. | Cardiac resynchronization therapy optimization using electromechanical delay from realtime electrode motion tracking |
| US8155739B2 (en) * | 2008-06-20 | 2012-04-10 | Pacesetter, Inc. | Cardiac resynchronization therapy optimization using mechanical dyssynchrony and shortening parameters from realtime electrode motion tracking |
| EP2154428A1 (de) * | 2008-08-11 | 2010-02-17 | Siemens Aktiengesellschaft | Brennstoffeinsatz |
| US8113001B2 (en) * | 2008-09-30 | 2012-02-14 | General Electric Company | Tubular fuel injector for secondary fuel nozzle |
| KR101024321B1 (ko) | 2008-10-31 | 2011-03-23 | 한국전력공사 | 석탄가스용 가스터빈 연소기 |
| KR101049359B1 (ko) * | 2008-10-31 | 2011-07-13 | 한국전력공사 | 삼중 스월형 가스터빈 연소기 |
| US8527049B2 (en) * | 2008-12-11 | 2013-09-03 | Pacesetter, Inc. | Cardiac resynchronization therapy optimization using vector measurements obtained from realtime electrode position tracking |
| US8256226B2 (en) * | 2009-04-23 | 2012-09-04 | General Electric Company | Radial lean direct injection burner |
| US20110054560A1 (en) * | 2009-09-03 | 2011-03-03 | Pacesetter, Inc. | Pacing, sensing and other parameter maps based on localization system data |
| US8285377B2 (en) * | 2009-09-03 | 2012-10-09 | Pacesetter, Inc. | Pacing, sensing and other parameter maps based on localization system data |
| US20110066202A1 (en) * | 2009-09-17 | 2011-03-17 | Pacesetter, Inc. | Electrode and lead stability indexes and stability maps based on localization system data |
| US8401645B2 (en) * | 2009-09-17 | 2013-03-19 | Pacesetter, Inc. | Electrode and lead stability indexes and stability maps based on localization system data |
| US20110066203A1 (en) * | 2009-09-17 | 2011-03-17 | Pacesetter, Inc. | Electrode and lead stability indexes and stability maps based on localization system data |
| US8412327B2 (en) * | 2009-11-18 | 2013-04-02 | Pacesetter, Inc. | Cardiac resynchronization therapy optimization using vector measurements obtained from realtime electrode position tracking |
| US20110144510A1 (en) * | 2009-12-16 | 2011-06-16 | Pacesetter, Inc. | Methods to identify damaged or scarred tissue based on position information and physiological information |
| US8903510B2 (en) * | 2010-01-28 | 2014-12-02 | Pacesetter, Inc. | Electrode configurations for leads or catheters to enhance localization using a localization system |
| US8590311B2 (en) * | 2010-04-28 | 2013-11-26 | General Electric Company | Pocketed air and fuel mixing tube |
| BE1019331A5 (nl) | 2010-05-10 | 2012-06-05 | Flooring Ind Ltd Sarl | Vloerpaneel en werkwijzen voor het vervaardigen van vloerpanelen. |
| BE1019747A3 (nl) | 2010-07-15 | 2012-12-04 | Flooring Ind Ltd Sarl | Bekleding, alsmede panelen en hulpstukken daarbij aangewend. |
| US20120137690A1 (en) * | 2010-12-03 | 2012-06-07 | General Electric Company | Wide frequency response tunable resonator |
| US9920932B2 (en) | 2011-01-26 | 2018-03-20 | United Technologies Corporation | Mixer assembly for a gas turbine engine |
| US8312724B2 (en) | 2011-01-26 | 2012-11-20 | United Technologies Corporation | Mixer assembly for a gas turbine engine having a pilot mixer with a corner flame stabilizing recirculation zone |
| US8973368B2 (en) | 2011-01-26 | 2015-03-10 | United Technologies Corporation | Mixer assembly for a gas turbine engine |
| US20120266602A1 (en) * | 2011-04-22 | 2012-10-25 | General Electric Company | Aerodynamic Fuel Nozzle |
| US9284231B2 (en) | 2011-12-16 | 2016-03-15 | General Electric Company | Hydrocarbon film protected refractory carbide components and use |
| US9719685B2 (en) * | 2011-12-20 | 2017-08-01 | General Electric Company | System and method for flame stabilization |
| JP6154988B2 (ja) * | 2012-01-05 | 2017-06-28 | 三菱日立パワーシステムズ株式会社 | 燃焼器 |
| US20130192237A1 (en) * | 2012-01-31 | 2013-08-01 | Solar Turbines Inc. | Fuel injector system with fluidic oscillator |
| CN103256633B (zh) * | 2012-02-16 | 2015-03-25 | 中国科学院工程热物理研究所 | 一种采用燃油分级空气三级旋流进气的低污染燃烧室 |
| US9115896B2 (en) | 2012-07-31 | 2015-08-25 | General Electric Company | Fuel-air mixer for use with a combustor assembly |
| GB201310261D0 (en) * | 2013-06-10 | 2013-07-24 | Rolls Royce Plc | A fuel injector and a combustion chamber |
| US9513010B2 (en) | 2013-08-07 | 2016-12-06 | Honeywell International Inc. | Gas turbine engine combustor with fluidic control of swirlers |
| US10794596B2 (en) * | 2013-08-30 | 2020-10-06 | Raytheon Technologies Corporation | Dual fuel nozzle with liquid filming atomization for a gas turbine engine |
| US10006330B2 (en) * | 2014-10-28 | 2018-06-26 | General Electric Company | System and method for emissions control in gas turbine systems |
| ITUA20163988A1 (it) * | 2016-05-31 | 2017-12-01 | Nuovo Pignone Tecnologie Srl | Ugello carburante per una turbina a gas con swirler radiale e swirler assiale e turbina a gas / fuel nozzle for a gas turbine with radial swirler and axial swirler and gas turbine |
| US10502425B2 (en) * | 2016-06-03 | 2019-12-10 | General Electric Company | Contoured shroud swirling pre-mix fuel injector assembly |
| US11149952B2 (en) * | 2016-12-07 | 2021-10-19 | Raytheon Technologies Corporation | Main mixer in an axial staged combustor for a gas turbine engine |
| CN107543203B (zh) * | 2017-08-21 | 2019-12-10 | 哈尔滨工程大学 | 一种用于气态燃料低污染燃烧室的双级复合旋流喷嘴 |
| US10816210B2 (en) | 2017-09-28 | 2020-10-27 | General Electric Company | Premixed fuel nozzle |
| US20190093562A1 (en) * | 2017-09-28 | 2019-03-28 | Solar Turbines Incorporated | Scroll for fuel injector assemblies in gas turbine engines |
| WO2019134748A1 (en) * | 2018-01-04 | 2019-07-11 | Wärtsilä Moss As | Dual fuel burner with swirl arrangement |
| US10935245B2 (en) * | 2018-11-20 | 2021-03-02 | General Electric Company | Annular concentric fuel nozzle assembly with annular depression and radial inlet ports |
| US11162682B2 (en) * | 2019-10-11 | 2021-11-02 | Solar Turbines Incorporated | Fuel injector |
| FR3115075B1 (fr) * | 2020-10-14 | 2022-10-21 | Safran Aircraft Engines | Circuit d’alimentation en carburant pour une chambre de combustion de turbomachine |
| US11761632B2 (en) * | 2021-08-05 | 2023-09-19 | General Electric Company | Combustor swirler with vanes incorporating open area |
| EP4614070A3 (en) | 2021-12-21 | 2025-10-01 | General Electric Company | Gas turbine engine |
| US11725819B2 (en) | 2021-12-21 | 2023-08-15 | General Electric Company | Gas turbine fuel nozzle having a fuel passage within a swirler |
| CN115899763B (zh) * | 2022-11-30 | 2024-10-29 | 南京航空航天大学 | 一种加力或冲压燃烧室尾缘剪切强化火焰稳定器 |
| US12135130B2 (en) | 2023-01-20 | 2024-11-05 | Collins Engine Nozzles, Inc. | Fuel nozzles |
| US20240263785A1 (en) * | 2023-02-02 | 2024-08-08 | Pratt & Whitney Canada Corp. | Combined air swirler and fuel distributor |
| US12181153B2 (en) * | 2023-02-23 | 2024-12-31 | Rtx Corporation | Fuel injector assembly for gas turbine engine |
Family Cites Families (30)
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|---|---|---|---|---|
| JPS63161318A (ja) * | 1986-12-23 | 1988-07-05 | Mitsubishi Heavy Ind Ltd | ガスタ−ビン用燃焼器の燃焼方法 |
| US5099644A (en) | 1990-04-04 | 1992-03-31 | General Electric Company | Lean staged combustion assembly |
| WO1992007221A1 (en) * | 1990-10-23 | 1992-04-30 | Rolls-Royce Plc | Gasturbine combustion chamber and method of operation thereof |
| WO1992019913A1 (de) * | 1991-04-25 | 1992-11-12 | Siemens Aktiengesellschaft | Brenneranordnung, insbesondere für gasturbinen, zur schadstoffarmen verbrennung von kohlegas und anderen brennstoffen |
| US5406799A (en) | 1992-06-12 | 1995-04-18 | United Technologies Corporation | Combustion chamber |
| US5394688A (en) * | 1993-10-27 | 1995-03-07 | Westinghouse Electric Corporation | Gas turbine combustor swirl vane arrangement |
| US5351477A (en) * | 1993-12-21 | 1994-10-04 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US5511375A (en) * | 1994-09-12 | 1996-04-30 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| JPH08166132A (ja) * | 1994-12-12 | 1996-06-25 | Tokyo Gas Co Ltd | ガス燃焼装置 |
| US6058710A (en) | 1995-03-08 | 2000-05-09 | Bmw Rolls-Royce Gmbh | Axially staged annular combustion chamber of a gas turbine |
| US5778676A (en) | 1996-01-02 | 1998-07-14 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US5680766A (en) | 1996-01-02 | 1997-10-28 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US5675971A (en) | 1996-01-02 | 1997-10-14 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US5865024A (en) * | 1997-01-14 | 1999-02-02 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US5850732A (en) | 1997-05-13 | 1998-12-22 | Capstone Turbine Corporation | Low emissions combustion system for a gas turbine engine |
| GB2333832A (en) | 1998-01-31 | 1999-08-04 | Europ Gas Turbines Ltd | Multi-fuel gas turbine engine combustor |
| DE69916911T2 (de) | 1998-02-10 | 2005-04-21 | Gen Electric | Brenner mit gleichmässiger Brennstoff/Luft Vormischung zur emissionsarmen Verbrennung |
| EP1096201A1 (de) * | 1999-10-29 | 2001-05-02 | Siemens Aktiengesellschaft | Brenner |
| US6453658B1 (en) | 2000-02-24 | 2002-09-24 | Capstone Turbine Corporation | Multi-stage multi-plane combustion system for a gas turbine engine |
| US6381964B1 (en) * | 2000-09-29 | 2002-05-07 | General Electric Company | Multiple annular combustion chamber swirler having atomizing pilot |
| US6655145B2 (en) * | 2001-12-20 | 2003-12-02 | Solar Turbings Inc | Fuel nozzle for a gas turbine engine |
| US6968692B2 (en) | 2002-04-26 | 2005-11-29 | Rolls-Royce Corporation | Fuel premixing module for gas turbine engine combustor |
| US7140560B2 (en) * | 2003-09-26 | 2006-11-28 | Parker-Hannifin Corporation | Nozzle assembly with fuel tube deflector |
| EP1568942A1 (de) * | 2004-02-24 | 2005-08-31 | Siemens Aktiengesellschaft | Vormischbrenner sowie Verfahren zur Verbrennung eines niederkalorischen Brenngases |
| US7370466B2 (en) * | 2004-11-09 | 2008-05-13 | Siemens Power Generation, Inc. | Extended flashback annulus in a gas turbine combustor |
| JP2006144759A (ja) * | 2004-11-25 | 2006-06-08 | Toyota Central Res & Dev Lab Inc | ガスタービン用予混合燃焼器およびその燃料供給制御方法 |
| JP4476176B2 (ja) * | 2005-06-06 | 2010-06-09 | 三菱重工業株式会社 | ガスタービンの予混合燃焼バーナー |
| US7565803B2 (en) * | 2005-07-25 | 2009-07-28 | General Electric Company | Swirler arrangement for mixer assembly of a gas turbine engine combustor having shaped passages |
| US7490471B2 (en) * | 2005-12-08 | 2009-02-17 | General Electric Company | Swirler assembly |
| US20090056336A1 (en) * | 2007-08-28 | 2009-03-05 | General Electric Company | Gas turbine premixer with radially staged flow passages and method for mixing air and gas in a gas turbine |
-
2006
- 2006-09-29 US US11/537,100 patent/US7631500B2/en active Active
-
2007
- 2007-09-20 CA CA 2603567 patent/CA2603567C/en not_active Expired - Fee Related
- 2007-09-25 EP EP07117177.1A patent/EP1909030B1/en active Active
- 2007-09-28 JP JP2007254133A patent/JP4958709B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP1909030B1 (en) | 2017-01-25 |
| US20080078181A1 (en) | 2008-04-03 |
| CA2603567C (en) | 2015-03-31 |
| CA2603567A1 (en) | 2008-03-29 |
| US7631500B2 (en) | 2009-12-15 |
| EP1909030A3 (en) | 2013-01-02 |
| JP2008089296A (ja) | 2008-04-17 |
| EP1909030A2 (en) | 2008-04-09 |
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