PL2748443T3 - Sposób mieszania reagentów spalania do spalania w turbinie gazowej - Google Patents

Sposób mieszania reagentów spalania do spalania w turbinie gazowej

Info

Publication number
PL2748443T3
PL2748443T3 PL11871108T PL11871108T PL2748443T3 PL 2748443 T3 PL2748443 T3 PL 2748443T3 PL 11871108 T PL11871108 T PL 11871108T PL 11871108 T PL11871108 T PL 11871108T PL 2748443 T3 PL2748443 T3 PL 2748443T3
Authority
PL
Poland
Prior art keywords
combustion
gas turbine
turbine engine
reactants
mixing
Prior art date
Application number
PL11871108T
Other languages
English (en)
Polish (pl)
Inventor
Majed Toqan
Brent Allan Gregory
Jonathan David Regele
Ryan Sadao Yamane
Original Assignee
Majed Toqan
Brent Allan Gregory
Jonathan David Regele
Ryan Sadao Yamane
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 Majed Toqan, Brent Allan Gregory, Jonathan David Regele, Ryan Sadao Yamane filed Critical Majed Toqan
Publication of PL2748443T3 publication Critical patent/PL2748443T3/pl

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)
PL11871108T 2011-08-22 2011-08-22 Sposób mieszania reagentów spalania do spalania w turbinie gazowej PL2748443T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PCT/US2011/048622 WO2013028169A1 (fr) 2011-08-22 2011-08-22 Chambre de combustion tubo-annulaire dotée de buses d'air et de combustible tangentielles destinées à être utilisées sur des moteurs de turbine à gaz
EP11871108.4A EP2748443B1 (fr) 2011-08-22 2011-08-22 Méthode pour mélanger des réactifs de combustion pour la combustion dans un moteur de turbine à gaz

Publications (1)

Publication Number Publication Date
PL2748443T3 true PL2748443T3 (pl) 2019-09-30

Family

ID=47746712

Family Applications (1)

Application Number Title Priority Date Filing Date
PL11871108T PL2748443T3 (pl) 2011-08-22 2011-08-22 Sposób mieszania reagentów spalania do spalania w turbinie gazowej

Country Status (7)

Country Link
EP (1) EP2748443B1 (fr)
JP (1) JP6086371B2 (fr)
KR (1) KR101774094B1 (fr)
CN (1) CN104053883B (fr)
PL (1) PL2748443T3 (fr)
RU (1) RU2619673C2 (fr)
WO (1) WO2013028169A1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102010646B1 (ko) 2017-07-04 2019-08-13 두산중공업 주식회사 터닝 가이드, 연료 노즐, 연료 노즐 조립체 및 이를 포함하는 가스 터빈
CN107631323B (zh) * 2017-09-05 2019-12-06 中国联合重型燃气轮机技术有限公司 燃气轮机的喷嘴
CN108487988A (zh) * 2018-03-14 2018-09-04 罗显平 一种燃气螺管转子发动机全环形燃烧室
CN109404965A (zh) * 2018-12-04 2019-03-01 新奥能源动力科技（上海）有限公司 一种燃气轮机的燃烧室及燃气轮机
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
CN112923398B (zh) * 2021-03-04 2022-07-22 西北工业大学 一种加力燃烧室防振隔热屏
CN114646077B (zh) * 2022-03-23 2023-08-11 西北工业大学 一种环腔开孔的空气雾化喷嘴

Family Cites Families (28)

* 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
SU1176678A1 (ru) * 1984-03-01 1995-08-27 О.Г. Жирицкий Жаровая труба камеры сгорания газотурбинного двигателя
SU1471748A1 (ru) * 1986-10-27 1995-08-09 О.Г. Жирицкий Жаровая труба камеры сгорания газотурбинного двигателя
US4938020A (en) * 1987-06-22 1990-07-03 Sundstrand Corporation Low cost annular combustor
US4891936A (en) * 1987-12-28 1990-01-09 Sundstrand Corporation Turbine combustor with tangential fuel injection and bender jets
JPH0375414A (ja) * 1989-08-15 1991-03-29 Nissan Motor Co Ltd ガスタービン燃焼器
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
US6427446B1 (en) * 2000-09-19 2002-08-06 Power Systems Mfg., Llc Low NOx emission combustion liner with circumferentially angled film cooling holes
JP4608154B2 (ja) * 2001-09-27 2011-01-05 大阪瓦斯株式会社 ガスタービン用燃焼装置及びそれを備えたガスタービン
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 (ja) * 2002-09-04 2007-08-15 石川島播磨重工業株式会社 拡散燃焼方式低ＮＯｘ燃焼器
JP3901629B2 (ja) * 2002-11-11 2007-04-04 石川島播磨重工業株式会社 アニュラ型渦巻き拡散火炎燃焼器
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
US20070107437A1 (en) 2005-11-15 2007-05-17 Evulet Andrei T Low emission combustion and method of operation
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
US8863528B2 (en) * 2006-07-27 2014-10-21 United Technologies Corporation Ceramic combustor can for a gas turbine engine
WO2008047825A1 (fr) * 2006-10-20 2008-04-24 Ihi Corporation Chambre de combustion de turbine à gaz
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 (ja) * 2009-04-02 2010-10-28 Ihi Corp ガスタービンの燃焼器
US8904799B2 (en) * 2009-05-25 2014-12-09 Majed Toqan Tangential combustor with vaneless turbine for use on gas turbine engines

Also Published As

Publication number Publication date
KR101774094B1 (ko) 2017-09-04
WO2013028169A1 (fr) 2013-02-28
KR20140082659A (ko) 2014-07-02
EP2748443A1 (fr) 2014-07-02
CN104053883A (zh) 2014-09-17
CN104053883B (zh) 2017-02-15
RU2014110631A (ru) 2015-09-27
EP2748443A4 (fr) 2015-05-27
EP2748443B1 (fr) 2019-04-24
JP2014526030A (ja) 2014-10-02
RU2619673C2 (ru) 2017-05-17
WO2013028169A8 (fr) 2014-04-17
JP6086371B2 (ja) 2017-03-01

Similar Documents

Publication Publication Date Title
GB201121887D0 (en) Intake liner for a gas turbine engine
EP2693122A4 (fr) Chambre de combustion pour un moteur de turbine à gaz et turbine à gaz
PL2748443T3 (pl) Sposób mieszania reagentów spalania do spalania w turbinie gazowej
GB201007063D0 (en) A gas turbine engine
EP2794182A4 (fr) Structure de support pour un moteur à turbine à gaz
ZA201403473B (en) Improvement of a combustion engine
GB2497809B (en) Method of servicing a gas turbine engine
ZA201404392B (en) Engine utilizing a plurality of fuels, and a related method thereof
BR112013011673A2 (pt) injetor de combustível para um motor de turbina a gás e método de operação de um motor de turbina a gás
GB201111002D0 (en) A method for operating an internal combustion engine
GB201420514D0 (en) Gas fuel turbine engine for reduced oscillations
GB201420524D0 (en) Method of reducing combustion induced oscillations in a turbine engine
EP2713013A4 (fr) Moteur de turbine à gaz
GB201104043D0 (en) A gas turbine engine
EP2844855A4 (fr) Collecteur pour turbine à gaz
GB201220378D0 (en) A gas turbine engine exhaust nozzle
EP2900975A4 (fr) Section de chambre de combustion de moteur à turbine à gaz
EP2554823A4 (fr) Dispositif d'alimentation en carburant d'un moteur à turbine à gaz
EP2730395B8 (fr) Procédé de fabrication d'un arbre de turbine à gaz
GB201112045D0 (en) A gas turbine engine exhaust nozzle
GB201106050D0 (en) A retention device for a composite blade of a gas turbine engine
GB2489673B (en) A containment casing for a gas turbine engine
EP2795067A4 (fr) Procédé de fabrication d'un composant d'une turbine à gaz
EP2703612A4 (fr) Épurateur de gaz d'échappement destiné à un moteur à combustion interne
EP2562394A4 (fr) Dispositif d'apport de carburant pour turbine à gaz