EP2748444A4 - Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines - Google Patents

Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines

Info

Publication number
EP2748444A4
EP2748444A4 EP11871243.9A EP11871243A EP2748444A4 EP 2748444 A4 EP2748444 A4 EP 2748444A4 EP 11871243 A EP11871243 A EP 11871243A EP 2748444 A4 EP2748444 A4 EP 2748444A4
Authority
EP
European Patent Office
Prior art keywords
staged
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
Application number
EP11871243.9A
Other languages
German (de)
French (fr)
Other versions
EP2748444B1 (en
EP2748444A2 (en
Inventor
Majed Toqan
Brent Allan Gregory
Jonathan David Regele
Ryan Sadao Yamane
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to PL11871243T priority Critical patent/PL2748444T3/en
Publication of EP2748444A2 publication Critical patent/EP2748444A2/en
Publication of EP2748444A4 publication Critical patent/EP2748444A4/en
Application granted granted Critical
Publication of EP2748444B1 publication Critical patent/EP2748444B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F23R3/44—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
    • F23R3/42—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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
EP11871243.9A 2011-08-22 2011-08-22 Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines Active EP2748444B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL11871243T PL2748444T3 (en) 2011-08-22 2011-08-22 Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2011/048612 WO2013028167A2 (en) 2011-08-22 2011-08-22 Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines

Publications (3)

Publication Number Publication Date
EP2748444A2 EP2748444A2 (en) 2014-07-02
EP2748444A4 true EP2748444A4 (en) 2015-05-27
EP2748444B1 EP2748444B1 (en) 2019-02-13

Family

ID=47747020

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11871243.9A Active EP2748444B1 (en) 2011-08-22 2011-08-22 Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines

Country Status (7)

Country Link
EP (1) EP2748444B1 (en)
JP (1) JP6086391B2 (en)
KR (1) KR101774093B1 (en)
CN (1) CN103998745B (en)
PL (1) PL2748444T3 (en)
RU (1) RU2611217C2 (en)
WO (1) WO2013028167A2 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10139111B2 (en) 2014-03-28 2018-11-27 Siemens Energy, Inc. Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engine
FR3032781B1 (en) * 2015-02-17 2018-07-06 Safran Helicopter Engines CONSTANT VOLUME COMBUSTION SYSTEM FOR AIRCRAFT ENGINE TURBOMACHINE
WO2018090383A1 (en) * 2016-11-21 2018-05-24 深圳智慧能源技术有限公司 Combustion chamber of gas turbine engine, and nozzle thereof
CN106439914A (en) * 2016-11-21 2017-02-22 深圳智慧能源技术有限公司 Combustion chamber of combustion gas turbine
WO2018090384A1 (en) * 2016-11-21 2018-05-24 深圳智慧能源技术有限公司 Combustion chamber of gas turbine engine
US11174792B2 (en) 2019-05-21 2021-11-16 General Electric Company System and method for high frequency acoustic dampers with baffles
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
KR102265626B1 (en) * 2020-09-25 2021-06-16 박재현 Sand spray test apparatus
CN114135901A (en) * 2021-11-08 2022-03-04 中国航发四川燃气涡轮研究院 Ablation-proof flame tube large-hole jet sleeve
CN114857617B (en) * 2022-05-20 2023-07-14 南昌航空大学 Support plate flame stabilizer of band saw tooth type groove vortex generator

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4098075A (en) * 1976-06-01 1978-07-04 United Technologies Corporation Radial inflow combustor
GB2044433A (en) * 1978-12-12 1980-10-15 Council Scient Ind Res Improved gas turbine engines operating on gaseous fuels
US4938020A (en) * 1987-06-22 1990-07-03 Sundstrand Corporation Low cost annular combustor
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 (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US6453658B1 (en) * 2000-02-24 2002-09-24 Capstone Turbine Corporation Multi-stage multi-plane combustion system for a gas turbine engine
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
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
CA2667047C (en) * 2006-10-20 2012-07-24 Ihi Corporation Gas turbine combustor
US8015814B2 (en) * 2006-10-24 2011-09-13 Caterpillar Inc. Turbine engine having folded annular jet combustor
US8176739B2 (en) * 2008-07-17 2012-05-15 General Electric Company Coanda injection system for axially staged low emission combustors
US20100242484A1 (en) * 2009-03-31 2010-09-30 Baha Mahmoud Suleiman Apparatus and method for cooling gas turbine engine combustors
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
US8388307B2 (en) * 2009-07-21 2013-03-05 Honeywell International Inc. Turbine nozzle assembly including radially-compliant spring member for gas turbine engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4098075A (en) * 1976-06-01 1978-07-04 United Technologies Corporation Radial inflow combustor
GB2044433A (en) * 1978-12-12 1980-10-15 Council Scient Ind Res Improved gas turbine engines operating on gaseous fuels
US4938020A (en) * 1987-06-22 1990-07-03 Sundstrand Corporation Low cost annular combustor
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)

* Cited by examiner, † Cited by third party
Title
See also references of WO2013028167A2 *

Also Published As

Publication number Publication date
WO2013028167A3 (en) 2014-03-20
EP2748444B1 (en) 2019-02-13
EP2748444A2 (en) 2014-07-02
RU2014110628A (en) 2015-09-27
CN103998745A (en) 2014-08-20
PL2748444T3 (en) 2019-11-29
RU2611217C2 (en) 2017-02-21
CN103998745B (en) 2017-02-15
KR20140082658A (en) 2014-07-02
KR101774093B1 (en) 2017-09-12
JP6086391B2 (en) 2017-03-01
JP2014526029A (en) 2014-10-02
WO2013028167A2 (en) 2013-02-28

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