ATE554346T1 - BRENNER FÜR EINE GASTURBINE UND VERFAHREN ZUR LOKALEN KÜHLUNG VON HEIßEN GASSTRÖMEN, DIE EINEN BRENNER DURCHLAUFEN - Google Patents
BRENNER FÜR EINE GASTURBINE UND VERFAHREN ZUR LOKALEN KÜHLUNG VON HEIßEN GASSTRÖMEN, DIE EINEN BRENNER DURCHLAUFENInfo
- Publication number
- ATE554346T1 ATE554346T1 AT09155235T AT09155235T ATE554346T1 AT E554346 T1 ATE554346 T1 AT E554346T1 AT 09155235 T AT09155235 T AT 09155235T AT 09155235 T AT09155235 T AT 09155235T AT E554346 T1 ATE554346 T1 AT E554346T1
- Authority
- AT
- Austria
- Prior art keywords
- burner
- gas turbine
- local cooling
- streams passing
- vortex generators
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 2
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000001816 cooling Methods 0.000 abstract 3
- 239000007789 gas Substances 0.000 abstract 2
- 239000000446 fuel Substances 0.000 abstract 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/003—Gas-turbine plants with heaters between turbine stages
-
- 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
- F23R3/06—Arrangement of apertures along the flame tube
-
- 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
- F23R3/02—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
-
- 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
- F05D2240/127—Vortex generators, turbulators, or the like, for mixing
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/21—Three-dimensional pyramidal
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2209/00—Safety arrangements
- F23D2209/20—Flame lift-off / stability
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP09155235A EP2230455B1 (de) | 2009-03-16 | 2009-03-16 | Brenner für eine Gasturbine und Verfahren zur lokalen Kühlung von heißen Gasströmen, die einen Brenner durchlaufen |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE554346T1 true ATE554346T1 (de) | 2012-05-15 |
Family
ID=40899483
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT09155235T ATE554346T1 (de) | 2009-03-16 | 2009-03-16 | BRENNER FÜR EINE GASTURBINE UND VERFAHREN ZUR LOKALEN KÜHLUNG VON HEIßEN GASSTRÖMEN, DIE EINEN BRENNER DURCHLAUFEN |
Country Status (5)
Country | Link |
---|---|
US (1) | US8850788B2 (de) |
EP (1) | EP2230455B1 (de) |
JP (1) | JP5558870B2 (de) |
CN (1) | CN101839483B (de) |
AT (1) | ATE554346T1 (de) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102645118B (zh) * | 2012-05-07 | 2013-12-25 | 华北电力大学 | 一种利用冲孔射流提高涡发生器强化换热效果的方法 |
WO2013188645A2 (en) * | 2012-06-13 | 2013-12-19 | General Electric Company | Gas turbine engine wall |
JP6012407B2 (ja) * | 2012-10-31 | 2016-10-25 | 三菱日立パワーシステムズ株式会社 | ガスタービン燃焼器及びガスタービン |
US10094571B2 (en) | 2014-12-11 | 2018-10-09 | General Electric Company | Injector apparatus with reheat combustor and turbomachine |
US10094570B2 (en) | 2014-12-11 | 2018-10-09 | General Electric Company | Injector apparatus and reheat combustor |
US10094569B2 (en) | 2014-12-11 | 2018-10-09 | General Electric Company | Injecting apparatus with reheat combustor and turbomachine |
US10107498B2 (en) | 2014-12-11 | 2018-10-23 | General Electric Company | Injection systems for fuel and gas |
EP3081862B1 (de) * | 2015-04-13 | 2020-08-19 | Ansaldo Energia Switzerland AG | Anordnung zur erzeugung eines wirbels für einen vorvermischenden brenner einer gasturbine und gasturbine mit solch einer wirbelerzeugenden anordnung |
CN104791828B (zh) * | 2015-05-06 | 2017-05-03 | 中国人民解放军国防科学技术大学 | 一种超音速燃烧室火焰稳定装置 |
CN105841191B (zh) * | 2016-03-30 | 2018-07-06 | 中国科学院工程热物理研究所 | 一种v型火焰稳定器尾缘结构 |
CN114857617B (zh) * | 2022-05-20 | 2023-07-14 | 南昌航空大学 | 一种带锯齿型凹槽涡流发生器的支板火焰稳定器 |
CN116025924B (zh) * | 2023-01-13 | 2024-09-20 | 南京航空航天大学 | 一种加力燃烧室外凹腔火焰稳定器后壁面强制冷却装置 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1492049A (en) * | 1974-12-07 | 1977-11-16 | Rolls Royce | Combustion equipment for gas turbine engines |
JPS5628415Y2 (de) * | 1976-10-25 | 1981-07-07 | ||
CH687269A5 (de) * | 1993-04-08 | 1996-10-31 | Abb Management Ag | Gasturbogruppe. |
DE59401177D1 (de) * | 1993-04-08 | 1997-01-16 | Abb Management Ag | Misch- und Flammenstabilisierungseinrichtung in einer Brennkammer mit Vormischverbrennung |
EP0619133B1 (de) * | 1993-04-08 | 1996-11-13 | ABB Management AG | Mischkammer |
CA2141066A1 (en) | 1994-02-18 | 1995-08-19 | Urs Benz | Process for the cooling of an auto-ignition combustion chamber |
DE4417538A1 (de) | 1994-05-19 | 1995-11-23 | Abb Management Ag | Brennkammer mit Selbstzündung |
DE4446611A1 (de) | 1994-12-24 | 1996-06-27 | Abb Management Ag | Brennkammer |
DE4446541A1 (de) | 1994-12-24 | 1996-06-27 | Abb Management Ag | Brennkammer |
DE19520291A1 (de) * | 1995-06-02 | 1996-12-05 | Abb Management Ag | Brennkammer |
DE10330023A1 (de) * | 2002-07-20 | 2004-02-05 | Alstom (Switzerland) Ltd. | Wirbelgenerator mit kontrollierter Nachlaufströmung |
DE102004049491A1 (de) * | 2004-10-11 | 2006-04-20 | Alstom Technology Ltd | Vormischbrenner |
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 |
US7186091B2 (en) | 2004-11-09 | 2007-03-06 | General Electric Company | Methods and apparatus for cooling gas turbine engine components |
GB0601413D0 (en) * | 2006-01-25 | 2006-03-08 | Rolls Royce Plc | Wall elements for gas turbine engine combustors |
FR2899315B1 (fr) * | 2006-03-30 | 2012-09-28 | Snecma | Configuration d'ouvertures de dilution dans une paroi de chambre de combustion de turbomachine |
US7669422B2 (en) | 2006-07-26 | 2010-03-02 | General Electric Company | Combustor liner and method of fabricating same |
US8171634B2 (en) * | 2007-07-09 | 2012-05-08 | Pratt & Whitney Canada Corp. | Method of producing effusion holes |
-
2009
- 2009-03-16 AT AT09155235T patent/ATE554346T1/de active
- 2009-03-16 EP EP09155235A patent/EP2230455B1/de not_active Not-in-force
-
2010
- 2010-03-10 US US12/720,890 patent/US8850788B2/en not_active Expired - Fee Related
- 2010-03-15 JP JP2010056982A patent/JP5558870B2/ja not_active Expired - Fee Related
- 2010-03-15 CN CN201010150085.3A patent/CN101839483B/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US20100229570A1 (en) | 2010-09-16 |
CN101839483B (zh) | 2014-06-11 |
US8850788B2 (en) | 2014-10-07 |
EP2230455A1 (de) | 2010-09-22 |
JP5558870B2 (ja) | 2014-07-23 |
EP2230455B1 (de) | 2012-04-18 |
JP2010216481A (ja) | 2010-09-30 |
CN101839483A (zh) | 2010-09-22 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ATE554346T1 (de) | BRENNER FÜR EINE GASTURBINE UND VERFAHREN ZUR LOKALEN KÜHLUNG VON HEIßEN GASSTRÖMEN, DIE EINEN BRENNER DURCHLAUFEN | |
ATE474189T1 (de) | Brennkammer für eine gasturbine | |
ATE540265T1 (de) | Drallvorrichtung, brennkammer und gasturbine mit verbessertem drall | |
JP2013148338A (ja) | インピンジメントスリーブ孔及びタービュレータを備えた燃焼器組立体 | |
FR2899936B1 (fr) | Procede de rechauffage selectif d'air a l'entree d'un compresseur associe a une turbine a gaz et systeme de production d'electricite. | |
EP2236938A3 (de) | Gasturbinenbrennkammer | |
IN2015DN03238A (de) | ||
ATE523660T1 (de) | Fluidgesteuerter ventil für ein gasturbinentriebwerk und für eine brennkammer | |
EP2236760A3 (de) | Thermisch entkoppeltes Übergangsstück einer Ringbrennkammer | |
ATE373206T1 (de) | Betriebsverfahren für eine feuerungsanlage | |
GB201114745D0 (en) | Wall elements for gas turbine engines | |
WO2014027005A3 (de) | Brenner mit in einer basis ausgebildetem brennstoffplenum | |
WO2014029512A3 (en) | Sequential combustion with dilution gas mixer | |
DE602005001742D1 (de) | Aerodynamisches aufschäumendes Brennstoff/Luft Einspritzungssystem für eine Gasturbinenbrennkammer | |
CH702103A8 (de) | Gasturbinensystem mit externer Zwischenüberhitzung. | |
BR112019004762A2 (pt) | sistema e método para a produção de energia mediante o uso de oxidação parcial | |
SA113340804B1 (ar) | طريقة لمزج هواء مخفف في نظام احتراق تسلسلي لتربينة غازية | |
JP2015511698A (ja) | 酸素含有ガスの流れに燃料を混合する混合装置 | |
ATE538300T1 (de) | System zum mischen von gasströmen in einem gasturbinentriebwerk, zugehöriges gasturbinentriebwerk und flugzeugtriebwerk | |
UA107163C2 (xx) | Повітронагрівник з верхнім обігрівом | |
SG133465A1 (en) | Combustor nozzle | |
EP2618059A3 (de) | Brennkammerdüse/-vormischer mit gekrümmten Abschnitten | |
EA201990367A1 (ru) | Способ крекинга потока углеводородов с использованием дымового газа из газовой турбины | |
SA113340952B1 (ar) | ناقل للاحتراق متكيف ليوجه غازات الاحتراق في ممر تدفق غاز ساخن | |
EP2515041A3 (de) | Brennstoffdüse und Verfahren für den Betrieb einer Brennkammer |