EP2748443A4 - Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines - Google Patents
Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine enginesInfo
- Publication number
- EP2748443A4 EP2748443A4 EP11871108.4A EP11871108A EP2748443A4 EP 2748443 A4 EP2748443 A4 EP 2748443A4 EP 11871108 A EP11871108 A EP 11871108A EP 2748443 A4 EP2748443 A4 EP 2748443A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- premixed
- gas turbine
- turbine engines
- air nozzles
- annular combustor
- 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.)
- Granted
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
- F23R3/346—Feeding into different combustion zones for staged 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
- 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
- F23R3/425—Combustion chambers comprising a tangential or helicoidal arrangement of the flame tubes
-
- 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
- F23R3/58—Cyclone or vortex type combustion chambers
-
- 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
- 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
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising 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
- F23R3/42—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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL11871108T PL2748443T3 (en) | 2011-08-22 | 2011-08-22 | Method of mixing combustion reactants for combustion in a gas turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US2011/048622 WO2013028169A1 (en) | 2011-08-22 | 2011-08-22 | Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2748443A1 EP2748443A1 (en) | 2014-07-02 |
EP2748443A4 true EP2748443A4 (en) | 2015-05-27 |
EP2748443B1 EP2748443B1 (en) | 2019-04-24 |
Family
ID=47746712
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11871108.4A Active EP2748443B1 (en) | 2011-08-22 | 2011-08-22 | Method of mixing combustion reactants for combustion in a gas turbine engine |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP2748443B1 (en) |
JP (1) | JP6086371B2 (en) |
KR (1) | KR101774094B1 (en) |
CN (1) | CN104053883B (en) |
PL (1) | PL2748443T3 (en) |
RU (1) | RU2619673C2 (en) |
WO (1) | WO2013028169A1 (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102010646B1 (en) | 2017-07-04 | 2019-08-13 | 두산중공업 주식회사 | Turning guide, fuel nozzle, fuel nozzle assembly and gas turbine having the same |
CN107631323B (en) * | 2017-09-05 | 2019-12-06 | 中国联合重型燃气轮机技术有限公司 | Nozzle for gas turbine |
CN108487988A (en) * | 2018-03-14 | 2018-09-04 | 罗显平 | A kind of combustion gas screwed pipe rotary engine loopful shape combustion chamber |
CN109404965A (en) * | 2018-12-04 | 2019-03-01 | 新奥能源动力科技(上海)有限公司 | A kind of combustion chamber of gas turbine and gas turbine |
US11156164B2 (en) | 2019-05-21 | 2021-10-26 | General Electric Company | System and method for high frequency accoustic dampers with caps |
US11174792B2 (en) | 2019-05-21 | 2021-11-16 | General Electric Company | System and method for high frequency acoustic dampers with baffles |
CN112923398B (en) * | 2021-03-04 | 2022-07-22 | 西北工业大学 | Afterburning chamber antivibration heat screen |
CN114646077B (en) * | 2022-03-23 | 2023-08-11 | 西北工业大学 | Air atomizing nozzle with holes in annular cavity |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4098075A (en) * | 1976-06-01 | 1978-07-04 | United Technologies Corporation | Radial inflow combustor |
US4938020A (en) * | 1987-06-22 | 1990-07-03 | Sundstrand Corporation | Low cost annular combustor |
US20040144098A1 (en) * | 2000-02-24 | 2004-07-29 | Willis Jeffrey W. | Multi-stage multi-plane combustion method for a gas turbine engine |
US20070107437A1 (en) * | 2005-11-15 | 2007-05-17 | Evulet Andrei T | Low emission combustion and method of operation |
EP1882885A2 (en) * | 2006-07-27 | 2008-01-30 | United Technologies Corporation | Ceramic combuster can for a gas turbine engine |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU1176678A1 (en) * | 1984-03-01 | 1995-08-27 | О.Г. Жирицкий | Fire tube of internal combustion gas-turbine engine |
SU1471748A1 (en) * | 1986-10-27 | 1995-08-09 | О.Г. Жирицкий | Flame tube of gas-turbine engine combustion chamber |
US4891936A (en) * | 1987-12-28 | 1990-01-09 | Sundstrand Corporation | Turbine combustor with tangential fuel injection and bender jets |
JPH0375414A (en) * | 1989-08-15 | 1991-03-29 | Nissan Motor Co Ltd | Gas turbine combustor |
US5113647A (en) * | 1989-12-22 | 1992-05-19 | Sundstrand Corporation | Gas turbine annular combustor |
GB2295887A (en) * | 1994-12-08 | 1996-06-12 | Rolls Royce Plc | Combustor assembly |
US6427446B1 (en) * | 2000-09-19 | 2002-08-06 | Power Systems Mfg., Llc | Low NOx emission combustion liner with circumferentially angled film cooling holes |
JP4608154B2 (en) * | 2001-09-27 | 2011-01-05 | 大阪瓦斯株式会社 | Gas turbine combustion apparatus and gas turbine provided with the same |
US6751961B2 (en) * | 2002-05-14 | 2004-06-22 | United Technologies Corporation | Bulkhead panel for use in a combustion chamber of a gas turbine engine |
JP3959632B2 (en) * | 2002-09-04 | 2007-08-15 | 石川島播磨重工業株式会社 | Diffusion combustion type low NOx combustor |
JP3901629B2 (en) * | 2002-11-11 | 2007-04-04 | 石川島播磨重工業株式会社 | Annular swirl diffusion flame combustor |
US7052231B2 (en) * | 2003-04-28 | 2006-05-30 | General Electric Company | Methods and apparatus for injecting fluids in gas turbine engines |
US6923001B2 (en) * | 2003-07-14 | 2005-08-02 | Siemens Westinghouse Power Corporation | Pilotless catalytic combustor |
US20070119183A1 (en) * | 2005-11-28 | 2007-05-31 | General Electric Company | Gas turbine engine combustor |
GB0610578D0 (en) * | 2006-05-27 | 2006-07-05 | Rolls Royce Plc | Method of removing deposits |
WO2008047825A1 (en) * | 2006-10-20 | 2008-04-24 | Ihi Corporation | Gas turbine combustor |
US8015814B2 (en) * | 2006-10-24 | 2011-09-13 | Caterpillar Inc. | Turbine engine having folded annular jet combustor |
US20080163627A1 (en) * | 2007-01-10 | 2008-07-10 | Ahmed Mostafa Elkady | Fuel-flexible triple-counter-rotating swirler and method of use |
US8176739B2 (en) * | 2008-07-17 | 2012-05-15 | General Electric Company | Coanda injection system for axially staged low emission combustors |
US8079804B2 (en) * | 2008-09-18 | 2011-12-20 | Siemens Energy, Inc. | Cooling structure for outer surface of a gas turbine case |
US8661779B2 (en) * | 2008-09-26 | 2014-03-04 | Siemens Energy, Inc. | Flex-fuel injector for gas turbines |
JP2010243009A (en) * | 2009-04-02 | 2010-10-28 | Ihi Corp | Burner for gas turbine |
US8904799B2 (en) * | 2009-05-25 | 2014-12-09 | Majed Toqan | Tangential combustor with vaneless turbine for use on gas turbine engines |
-
2011
- 2011-08-22 CN CN201180073014.0A patent/CN104053883B/en active Active
- 2011-08-22 PL PL11871108T patent/PL2748443T3/en unknown
- 2011-08-22 JP JP2014527127A patent/JP6086371B2/en active Active
- 2011-08-22 WO PCT/US2011/048622 patent/WO2013028169A1/en unknown
- 2011-08-22 KR KR1020147007519A patent/KR101774094B1/en active IP Right Grant
- 2011-08-22 RU RU2014110631A patent/RU2619673C2/en active
- 2011-08-22 EP EP11871108.4A patent/EP2748443B1/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4098075A (en) * | 1976-06-01 | 1978-07-04 | United Technologies Corporation | Radial inflow combustor |
US4938020A (en) * | 1987-06-22 | 1990-07-03 | Sundstrand Corporation | Low cost annular combustor |
US20040144098A1 (en) * | 2000-02-24 | 2004-07-29 | Willis Jeffrey W. | Multi-stage multi-plane combustion method for a gas turbine engine |
US20070107437A1 (en) * | 2005-11-15 | 2007-05-17 | Evulet Andrei T | Low emission combustion and method of operation |
EP1882885A2 (en) * | 2006-07-27 | 2008-01-30 | United Technologies Corporation | Ceramic combuster can for a gas turbine engine |
Non-Patent Citations (1)
Title |
---|
See also references of WO2013028169A1 * |
Also Published As
Publication number | Publication date |
---|---|
RU2014110631A (en) | 2015-09-27 |
JP6086371B2 (en) | 2017-03-01 |
EP2748443B1 (en) | 2019-04-24 |
EP2748443A1 (en) | 2014-07-02 |
WO2013028169A1 (en) | 2013-02-28 |
JP2014526030A (en) | 2014-10-02 |
CN104053883B (en) | 2017-02-15 |
WO2013028169A8 (en) | 2014-04-17 |
PL2748443T3 (en) | 2019-09-30 |
CN104053883A (en) | 2014-09-17 |
KR101774094B1 (en) | 2017-09-04 |
KR20140082659A (en) | 2014-07-02 |
RU2619673C2 (en) | 2017-05-17 |
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