SG130102A1 - Gas turbine system and method of operation - Google Patents
Gas turbine system and method of operationInfo
- 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
Links
- 239000000446 fuel Substances 0.000 abstract 3
- 238000003303 reheating Methods 0.000 abstract 3
- 239000003570 air Substances 0.000 abstract 1
- 239000012080 ambient air Substances 0.000 abstract 1
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
- F23R3/02—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
- F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-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
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03341—Sequential combustion chambers or burners
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/14—Combined heat and power generation [CHP]
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined 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)
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)
| 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)
| 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 |
-
2005
- 2005-08-10 US US11/201,497 patent/US20070033945A1/en not_active Abandoned
-
2006
- 2006-07-24 SG SG200604972-0A patent/SG130102A1/en unknown
- 2006-07-24 SG SG200901464-8A patent/SG150564A1/en unknown
- 2006-07-24 SG SG2012058897A patent/SG183707A1/en unknown
- 2006-08-07 EP EP06254130.5A patent/EP1752709A3/fr not_active Withdrawn
- 2006-08-09 JP JP2006216559A patent/JP2007046611A/ja not_active Ceased
- 2006-08-10 CN CNA2006101148213A patent/CN1912367A/zh active Pending
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 |