IN2014DE01107A - - Google Patents
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- Publication number
- IN2014DE01107A IN2014DE01107A IN1107DE2014A IN2014DE01107A IN 2014DE01107 A IN2014DE01107 A IN 2014DE01107A IN 1107DE2014 A IN1107DE2014 A IN 1107DE2014A IN 2014DE01107 A IN2014DE01107 A IN 2014DE01107A
- Authority
- IN
- India
- Prior art keywords
- front panel
- combustor
- fuel
- air mixture
- burner
- Prior art date
Links
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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/44—Combustion chambers comprising a single tubular flame tube within a tubular casing
-
- 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
- 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
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
-
- 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
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- 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
-
- 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
-
- 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
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
- F23C2900/07002—Premix burners with air inlet slots obtained between offset curved wall surfaces, e.g. double cone burners
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Incineration Of Waste (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP13165488.1A EP2796789B1 (de) | 2013-04-26 | 2013-04-26 | Rohrbrennkammer für eine Rohr-Ring Anordnung in einer Gasturbine |
Publications (1)
Publication Number | Publication Date |
---|---|
IN2014DE01107A true IN2014DE01107A (de) | 2015-06-05 |
Family
ID=48190758
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IN1107DE2014 IN2014DE01107A (de) | 2013-04-26 | 2014-04-23 |
Country Status (8)
Country | Link |
---|---|
US (1) | US10422535B2 (de) |
EP (1) | EP2796789B1 (de) |
JP (1) | JP2014215036A (de) |
KR (1) | KR101702854B1 (de) |
CN (1) | CN104121601B (de) |
CA (1) | CA2848898C (de) |
IN (1) | IN2014DE01107A (de) |
RU (1) | RU2581265C2 (de) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9939156B2 (en) * | 2013-06-05 | 2018-04-10 | Siemens Aktiengesellschaft | Asymmetric baseplate cooling with alternating swirl main burners |
US10480823B2 (en) * | 2013-11-14 | 2019-11-19 | Lennox Industries Inc. | Multi-burner head assembly |
EP3023696B1 (de) * | 2014-11-20 | 2019-08-28 | Ansaldo Energia Switzerland AG | Nockenlanze für eine Gasturbinenbrennkammer |
US11002190B2 (en) * | 2016-03-25 | 2021-05-11 | General Electric Company | Segmented annular combustion system |
JP6822868B2 (ja) * | 2017-02-21 | 2021-01-27 | 三菱重工業株式会社 | 燃焼器及びガスタービン |
US10584877B2 (en) * | 2017-04-28 | 2020-03-10 | DOOSAN Heavy Industries Construction Co., LTD | Device to correct flow non-uniformity within a combustion system |
KR102063169B1 (ko) | 2017-07-04 | 2020-01-07 | 두산중공업 주식회사 | 연료 노즐 조립체와 이를 포함하는 연소기 및 가스 터빈 |
JP6995696B2 (ja) * | 2018-05-28 | 2022-01-17 | 三菱重工業株式会社 | 燃料噴射装置及びガスタービン |
US11286884B2 (en) * | 2018-12-12 | 2022-03-29 | General Electric Company | Combustion section and fuel injector assembly for a heat engine |
KR102164622B1 (ko) * | 2019-06-11 | 2020-10-12 | 두산중공업 주식회사 | 공진주파수 회피형 멀티 튜브를 갖는 연소기 및 가스터빈 |
JP2022171082A (ja) * | 2021-04-30 | 2022-11-11 | 東芝エネルギーシステムズ株式会社 | ガスタービン燃焼器構造体 |
US20230003385A1 (en) * | 2021-07-02 | 2023-01-05 | General Electric Company | Premixer array |
US20230204215A1 (en) * | 2021-12-29 | 2023-06-29 | General Electric Company | Fuel nozzle and swirler |
KR102608433B1 (ko) * | 2022-02-09 | 2023-11-29 | 두산에너빌리티 주식회사 | 연소진동 저감을 위한 연소기용 노즐 및 이를 포함하는 가스 터빈 |
Family Cites Families (35)
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SU352573A1 (ru) * | 1970-10-05 | 1983-06-23 | Pinchuk V V | Кольцева камера сгорани газотурбинного двигател |
US3811274A (en) | 1972-08-30 | 1974-05-21 | United Aircraft Corp | Crossover tube construction |
CH674561A5 (de) | 1987-12-21 | 1990-06-15 | Bbc Brown Boveri & Cie | |
CH687269A5 (de) * | 1993-04-08 | 1996-10-31 | Abb Management Ag | Gasturbogruppe. |
CN2200120Y (zh) | 1994-07-16 | 1995-06-07 | 汤义勇 | 自动增压式合成燃料燃烧装置 |
DE4435266A1 (de) | 1994-10-01 | 1996-04-04 | Abb Management Ag | Brenner |
DE19547913A1 (de) * | 1995-12-21 | 1997-06-26 | Abb Research Ltd | Brenner für einen Wärmeerzeuger |
DE19615910B4 (de) * | 1996-04-22 | 2006-09-14 | Alstom | Brenneranordnung |
EP0925472B1 (de) * | 1996-09-16 | 2001-04-04 | Siemens Aktiengesellschaft | Verfahren zur unterdrückung von verbrennungsschwingungen und einrichtung zur verbrennung von brennstoff mit luft |
GB2319078B (en) | 1996-11-08 | 1999-11-03 | Europ Gas Turbines Ltd | Combustor arrangement |
SE9802707L (sv) | 1998-08-11 | 2000-02-12 | Abb Ab | Brännkammaranordning och förfarande för att reducera inverkan av akustiska trycksvängningar i en brännkammaranordning |
EP1292795B1 (de) | 2000-06-15 | 2005-05-04 | ALSTOM Technology Ltd | Verfahren zum betrieb eines brenners mit gestufter vormischgas-eindüsung |
US6438959B1 (en) * | 2000-12-28 | 2002-08-27 | General Electric Company | Combustion cap with integral air diffuser and related method |
JP3872960B2 (ja) | 2001-02-28 | 2007-01-24 | 株式会社日立製作所 | ガスタ−ビン燃焼器 |
JP3986348B2 (ja) | 2001-06-29 | 2007-10-03 | 三菱重工業株式会社 | ガスタービン燃焼器の燃料供給ノズルおよびガスタービン燃焼器並びにガスタービン |
JP4610800B2 (ja) | 2001-06-29 | 2011-01-12 | 三菱重工業株式会社 | ガスタービン燃焼器 |
DE50212743D1 (de) | 2002-01-14 | 2008-10-16 | Alstom Technology Ltd | Brenneranordnung für die ringförmige brennkammer einer gasturbine |
JP4134311B2 (ja) | 2002-03-08 | 2008-08-20 | 独立行政法人 宇宙航空研究開発機構 | ガスタービン燃焼器 |
US6968693B2 (en) * | 2003-09-22 | 2005-11-29 | General Electric Company | Method and apparatus for reducing gas turbine engine emissions |
JP2006105534A (ja) | 2004-10-07 | 2006-04-20 | Niigata Power Systems Co Ltd | ガスタービン燃焼器 |
CN101095012B (zh) | 2004-11-03 | 2010-11-10 | 阿尔斯托姆科技有限公司 | 预混合式烧嘴 |
ATE479054T1 (de) * | 2005-03-09 | 2010-09-15 | Alstom Technology Ltd | Vormischbrenner zum erzeugen eines zündfähigen brennstoff-luftgemisches |
EP1856447B1 (de) * | 2005-03-09 | 2014-09-24 | Alstom Technology Ltd | Vormischbrenner zum betreiben einer brennkammer |
US7827797B2 (en) * | 2006-09-05 | 2010-11-09 | General Electric Company | Injection assembly for a combustor |
US7886545B2 (en) * | 2007-04-27 | 2011-02-15 | General Electric Company | Methods and systems to facilitate reducing NOx emissions in combustion systems |
FR2919348A1 (fr) * | 2007-07-23 | 2009-01-30 | Centre Nat Rech Scient | Dispositif d'injection d'un combustible ou d'un pre-melange combustible/comburant comprenant des moyens permettant un controle passif des instabilites de combustion |
US8087228B2 (en) | 2008-09-11 | 2012-01-03 | General Electric Company | Segmented combustor cap |
US20100192578A1 (en) * | 2009-01-30 | 2010-08-05 | General Electric Company | System and method for suppressing combustion instability in a turbomachine |
RU2506499C2 (ru) | 2009-11-09 | 2014-02-10 | Дженерал Электрик Компани | Топливные форсунки газовой турбины с противоположными направлениями завихрения |
RU2534189C2 (ru) | 2010-02-16 | 2014-11-27 | Дженерал Электрик Компани | Камера сгорания для газовой турбины(варианты) и способ эксплуатации газовой турбины |
EP2423591B1 (de) * | 2010-08-24 | 2018-10-31 | Ansaldo Energia IP UK Limited | Verfahren zum Betrieb einer Brennkammer |
CH704829A2 (de) | 2011-04-08 | 2012-11-15 | Alstom Technology Ltd | Gasturbogruppe und zugehöriges Betriebsverfahren. |
CH705179A1 (de) * | 2011-06-20 | 2012-12-31 | Alstom Technology Ltd | Verfahren zum Betrieb einer Verbrennungsvorrichtung sowie Verbrennungsvorrichtung zur Durchführung des Verfahrens. |
US9310072B2 (en) * | 2012-07-06 | 2016-04-12 | Hamilton Sundstrand Corporation | Non-symmetric arrangement of fuel nozzles in a combustor |
RU2561956C2 (ru) * | 2012-07-09 | 2015-09-10 | Альстом Текнолоджи Лтд | Газотурбинная система сгорания |
-
2013
- 2013-04-26 EP EP13165488.1A patent/EP2796789B1/de active Active
-
2014
- 2014-04-14 CA CA2848898A patent/CA2848898C/en not_active Expired - Fee Related
- 2014-04-23 RU RU2014116563/06A patent/RU2581265C2/ru active
- 2014-04-23 IN IN1107DE2014 patent/IN2014DE01107A/en unknown
- 2014-04-24 US US14/260,617 patent/US10422535B2/en active Active
- 2014-04-25 CN CN201410169977.6A patent/CN104121601B/zh active Active
- 2014-04-25 KR KR1020140049781A patent/KR101702854B1/ko active IP Right Grant
- 2014-04-28 JP JP2014092325A patent/JP2014215036A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
CN104121601A (zh) | 2014-10-29 |
US10422535B2 (en) | 2019-09-24 |
RU2014116563A (ru) | 2015-10-27 |
CA2848898A1 (en) | 2014-10-26 |
CA2848898C (en) | 2016-10-04 |
EP2796789A1 (de) | 2014-10-29 |
JP2014215036A (ja) | 2014-11-17 |
KR101702854B1 (ko) | 2017-02-06 |
US20140318135A1 (en) | 2014-10-30 |
CN104121601B (zh) | 2017-11-10 |
EP2796789B1 (de) | 2017-03-01 |
KR20140128260A (ko) | 2014-11-05 |
RU2581265C2 (ru) | 2016-04-20 |
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