SG130102A1 - Gas turbine system and method of operation - Google Patents

Gas turbine system and method of operation

Info

Publication number
SG130102A1
SG130102A1 SG200604972-0A SG2006049720A SG130102A1 SG 130102 A1 SG130102 A1 SG 130102A1 SG 2006049720 A SG2006049720 A SG 2006049720A SG 130102 A1 SG130102 A1 SG 130102A1
Authority
SG
Singapore
Prior art keywords
combustor
turbine system
turbine
gas turbine
gas stream
Prior art date
Application number
SG200604972-0A
Other languages
English (en)
Inventor
Jeffrey Scott Goldmeer
Joel Meier Haynes
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of SG130102A1 publication Critical patent/SG130102A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous 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
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003Gas-turbine plants with heaters between turbine stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03341Sequential combustion chambers or burners
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/14Combined heat and power generation [CHP]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/16Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
SG200604972-0A 2005-08-10 2006-07-24 Gas turbine system and method of operation SG130102A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/201,497 US20070033945A1 (en) 2005-08-10 2005-08-10 Gas turbine system and method of operation

Publications (1)

Publication Number Publication Date
SG130102A1 true SG130102A1 (en) 2007-03-20

Family

ID=37387436

Family Applications (3)

Application Number Title Priority Date Filing Date
SG200604972-0A SG130102A1 (en) 2005-08-10 2006-07-24 Gas turbine system and method of operation
SG200901464-8A SG150564A1 (en) 2005-08-10 2006-07-24 Gas turbine system and method of operation
SG2012058897A SG183707A1 (en) 2005-08-10 2006-07-24 Gas turbine system and method of operation

Family Applications After (2)

Application Number Title Priority Date Filing Date
SG200901464-8A SG150564A1 (en) 2005-08-10 2006-07-24 Gas turbine system and method of operation
SG2012058897A SG183707A1 (en) 2005-08-10 2006-07-24 Gas turbine system and method of operation

Country Status (5)

Country Link
US (1) US20070033945A1 (fr)
EP (1) EP1752709A3 (fr)
JP (1) JP2007046611A (fr)
CN (1) CN1912367A (fr)
SG (3) SG130102A1 (fr)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8387390B2 (en) 2006-01-03 2013-03-05 General Electric Company Gas turbine combustor having counterflow injection mechanism
EP1995433A1 (fr) * 2007-05-24 2008-11-26 Siemens Aktiengesellschaft Ensemble turbine à gaz tout comme procédé de commande d'un ensemble turbine à gaz
US9062563B2 (en) * 2008-04-09 2015-06-23 General Electric Company Surface treatments for preventing hydrocarbon thermal degradation deposits on articles
US8511059B2 (en) * 2008-09-30 2013-08-20 Alstom Technology Ltd. Methods of reducing emissions for a sequential combustion gas turbine and combustor for a gas turbine
US20100175379A1 (en) * 2009-01-09 2010-07-15 General Electric Company Pre-mix catalytic partial oxidation fuel reformer for staged and reheat gas turbine systems
US20100175386A1 (en) * 2009-01-09 2010-07-15 General Electric Company Premixed partial oxidation syngas generation and gas turbine system
EP2211110B1 (fr) 2009-01-23 2019-05-01 Ansaldo Energia Switzerland AG Brûleur pour turbine à gaz
US8763400B2 (en) * 2009-08-04 2014-07-01 General Electric Company Aerodynamic pylon fuel injector system for combustors
ES2399309T3 (es) * 2009-09-07 2013-03-27 Alstom Technology Ltd Método para cambiar una planta de turbina de gas combustible gaseoso a combustible líquido y viceversa
WO2011054739A2 (fr) 2009-11-07 2011-05-12 Alstom Technology Ltd Système d'injection pour brûleur de réchauffage
WO2011054760A1 (fr) * 2009-11-07 2011-05-12 Alstom Technology Ltd Système de refroidissement permettant d'accroître le rendement d'une turbine à gaz
WO2011054771A2 (fr) 2009-11-07 2011-05-12 Alstom Technology Ltd Brûleur à prémélange pour chambre de combustion de turbine à gaz
WO2011054757A2 (fr) 2009-11-07 2011-05-12 Alstom Technology Ltd Système d'injection pour brûleur de réchauffage avec lances à combustible
WO2011054766A2 (fr) 2009-11-07 2011-05-12 Alstom Technology Ltd Système d'injection de brûleur de postcombustion
CH703105A1 (de) * 2010-05-05 2011-11-15 Alstom Technology Ltd Gasturbine mit einer sekundärbrennkammer.
RU2531110C2 (ru) * 2010-06-29 2014-10-20 Дженерал Электрик Компани Газотурбинная установка и установка, содержащая лопатки-форсунки (варианты)
EA029301B1 (ru) * 2010-07-02 2018-03-30 Эксонмобил Апстрим Рисерч Компани Интегрированные системы для получения со(варианты) и способ производства электроэнергии
US8745987B2 (en) 2010-10-28 2014-06-10 General Electric Company Late lean injection manifold
US20120159922A1 (en) * 2010-12-23 2012-06-28 Michael Gurin Top cycle power generation with high radiant and emissivity exhaust
US8984859B2 (en) * 2010-12-28 2015-03-24 Rolls-Royce North American Technologies, Inc. Gas turbine engine and reheat system
US8863525B2 (en) 2011-01-03 2014-10-21 General Electric Company Combustor with fuel staggering for flame holding mitigation
CH704829A2 (de) * 2011-04-08 2012-11-15 Alstom Technology Ltd Gasturbogruppe und zugehöriges Betriebsverfahren.
EP2581561B8 (fr) * 2011-10-12 2017-07-12 Ansaldo Energia IP UK Limited Procédé d'exploitation de mélanges d'hydrogène/gaz naturel dans une turbine à gaz de réchauffage et turbine à gaz
ITFI20110257A1 (it) * 2011-12-02 2013-06-03 Nuovo Pignone Spa "cooling system for gas turbine load coupling"
US9121608B2 (en) * 2011-12-29 2015-09-01 General Electric Company Gas turbine engine including secondary combustion chamber integrated with the stator vanes in the turbine/expansion section of the engine and a method of operating the same
RU2561956C2 (ru) 2012-07-09 2015-09-10 Альстом Текнолоджи Лтд Газотурбинная система сгорания
EP2600063A3 (fr) * 2013-02-19 2014-05-07 Alstom Technology Ltd Procédé de fonctionnement d'une turbine à gaz avec combustion étagée et/ou séquentielle
US9624829B2 (en) 2013-03-05 2017-04-18 Industrial Turbine Company (Uk) Limited Cogen heat load matching through reheat and capacity match
US10036317B2 (en) 2013-03-05 2018-07-31 Industrial Turbine Company (Uk) Limited Capacity control of turbine by the use of a reheat combustor in multi shaft engine
US9458767B2 (en) 2013-03-18 2016-10-04 General Electric Company Fuel injection insert for a turbine nozzle segment
US9328663B2 (en) * 2013-05-30 2016-05-03 General Electric Company Gas turbine engine and method of operating thereof
CN103321748B (zh) * 2013-06-19 2016-03-16 北京理工大学 立式燃气轮机
US9534541B2 (en) 2013-10-11 2017-01-03 General Electric Company System and method for improving efficiency of a gas turbine engine
CN104763474A (zh) * 2015-03-28 2015-07-08 中国船舶重工集团公司第七�三研究所 新型三转子对转涡轮
US11859539B2 (en) 2021-02-01 2024-01-02 General Electric Company Aircraft propulsion system with inter-turbine burner
CN114876645B (zh) * 2022-06-10 2023-11-03 贾煊 一种双燃料节能环保航空发动机
US11958575B2 (en) * 2022-06-15 2024-04-16 Stena Power & Lng Solutions As System for offshore production of fuel

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2392231A1 (fr) * 1977-05-23 1978-12-22 Inst Francais Du Petrole Turbine a gaz comportant une chambre de combustion entre les etages de la turbine
US4896499A (en) * 1978-10-26 1990-01-30 Rice Ivan G Compression intercooled gas turbine combined cycle
US4813227A (en) * 1978-10-26 1989-03-21 Rice Ivan G Preheat gas turbine combined with steam turbine
FR2721694B1 (fr) * 1994-06-22 1996-07-19 Snecma Refroidissement de l'injecteur de décollage d'une chambre de combustion à deux têtes.
DE59409252D1 (de) * 1994-09-21 2000-05-04 Abb Alstom Power Ch Ag Brennkammer einer Gasturbogruppe
JP3585960B2 (ja) * 1994-09-21 2004-11-10 株式会社東芝 低カロリーガス用ガスタービン燃焼器
US5685140A (en) * 1995-06-21 1997-11-11 United Technologies Corporation Method for distributing fuel within an augmentor
US20020157378A1 (en) * 1997-06-26 2002-10-31 Konrad Vogeler Jet engine
DE19726975A1 (de) * 1997-06-26 1999-01-07 Asea Brown Boveri Strahltriebwerk
US6418724B1 (en) * 2000-06-12 2002-07-16 Cheng Power Systems, Inc. Method and apparatus to homogenize fuel and diluent for reducing emissions in combustion systems
US6619026B2 (en) * 2001-08-27 2003-09-16 Siemens Westinghouse Power Corporation Reheat combustor for gas combustion turbine
JP3951652B2 (ja) * 2001-09-13 2007-08-01 株式会社日立製作所 ガスタービン発電設備
AU2003258212B2 (en) * 2003-06-05 2009-03-19 Fluor Technologies Corporation Liquefied natural gas regasification configuration and method
US20070062216A1 (en) * 2003-08-13 2007-03-22 John Mak Liquefied natural gas regasification configuration and method

Also Published As

Publication number Publication date
EP1752709A3 (fr) 2013-11-27
SG183707A1 (en) 2012-09-27
CN1912367A (zh) 2007-02-14
EP1752709A2 (fr) 2007-02-14
SG150564A1 (en) 2009-03-30
US20070033945A1 (en) 2007-02-15
JP2007046611A (ja) 2007-02-22

Similar Documents

Publication Publication Date Title
SG130102A1 (en) Gas turbine system and method of operation
EP4001618A3 (fr) Craquage et séparation de combustible d'ammoniac
EP1939438A3 (fr) Réacteur à flux mixtes avec chauffage du flux dérivé
EP2562383A3 (fr) Procédé de fonctionnement d'une centrale électrique
EP1186761A3 (fr) Récupération d'énergie de l'air de soutirage du compresseur chez des turbines à gaz
ATE540213T1 (de) Verfahren zum betrieb einer gasturbinenanlage
EP1921256A3 (fr) Moteur refroidi interétage double
EP1942269A3 (fr) Moteur à turbine à gaz convertible
EP2660518A3 (fr) Résonateur acoustique situé au niveau du manchon d'écoulement d'une chambre de combustion de turbine à gaz
WO2010036432A3 (fr) Système et procédé de fonctionnement d’une turbine à gaz dotée d’un fluide de travail différent
EP2384400A4 (fr) Compresseur à taux de compression variable
MX2007013349A (es) Montaje de motor de turboventilador y metodo para ensamblar el mismo.
EP1688603A3 (fr) Ensemble moteur à turbine à gaz
MY149412A (en) Venturi cooling system
WO2010075393A3 (fr) Turbine à gaz et système d'entretien d'une turbine à gaz
EP1731734A3 (fr) Turboréacteur comportant des rotors contra-rotatifs
EP2562384A3 (fr) Procédé de fonctionnement d'une centrale électrique
WO2001018371A8 (fr) Systeme de turbine a gaz fonctionnant sous pression ambiante
EP1728990A3 (fr) Unité de puissance auxiliaire alimentée avec air d'une turbine à gaz
WO2002027167A3 (fr) Generateur de vapeur a air comprime destine a etre utilise dans le refroidissement d'une partie de transition d'une turbine de combustion
WO2008091502A3 (fr) Augmentation de puissance de turbines à combustion par injection d'air froid en amont du compresseur
EP2017826A3 (fr) Panneau acoustique
CA2576683C (fr) Turbine a gaz auxiliaire d'aeronef et methode d'exploitation
MY167118A (en) Low emission triple-cycle power generation systems and methods
EP1039115A3 (fr) Système de turbine à gaz