JP2009528503A5 - - Google Patents

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Publication number
JP2009528503A5
JP2009528503A5 JP2008556749A JP2008556749A JP2009528503A5 JP 2009528503 A5 JP2009528503 A5 JP 2009528503A5 JP 2008556749 A JP2008556749 A JP 2008556749A JP 2008556749 A JP2008556749 A JP 2008556749A JP 2009528503 A5 JP2009528503 A5 JP 2009528503A5
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JP
Japan
Prior art keywords
gas
combustor
fuel
gas turbine
gaseous fuel
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
JP2008556749A
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English (en)
Japanese (ja)
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JP2009528503A (ja
JP4776697B2 (ja
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Publication date
Application filed filed Critical
Priority claimed from PCT/EP2007/051597 external-priority patent/WO2007099046A1/de
Publication of JP2009528503A publication Critical patent/JP2009528503A/ja
Publication of JP2009528503A5 publication Critical patent/JP2009528503A5/ja
Application granted granted Critical
Publication of JP4776697B2 publication Critical patent/JP4776697B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2008556749A 2006-02-28 2007-02-20 ガスタービン用燃焼器およびガスタービン用燃焼器の運転方法 Expired - Fee Related JP4776697B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102006009562.6 2006-02-28
DE102006009562 2006-02-28
PCT/EP2007/051597 WO2007099046A1 (de) 2006-02-28 2007-02-20 Gasturbinenbrenner und verfahren zum betreiben eines gasturbinenbrenners

Publications (3)

Publication Number Publication Date
JP2009528503A JP2009528503A (ja) 2009-08-06
JP2009528503A5 true JP2009528503A5 (enExample) 2010-04-02
JP4776697B2 JP4776697B2 (ja) 2011-09-21

Family

ID=38009771

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008556749A Expired - Fee Related JP4776697B2 (ja) 2006-02-28 2007-02-20 ガスタービン用燃焼器およびガスタービン用燃焼器の運転方法

Country Status (6)

Country Link
US (1) US20100043440A1 (enExample)
EP (1) EP1989486A1 (enExample)
JP (1) JP4776697B2 (enExample)
CN (1) CN101395428B (enExample)
RU (1) RU2406034C2 (enExample)
WO (1) WO2007099046A1 (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9528439B2 (en) * 2013-03-15 2016-12-27 General Electric Company Systems and apparatus relating to downstream fuel and air injection in gas turbines
US10222066B2 (en) * 2016-05-26 2019-03-05 Siemens Energy, Inc. Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engine
US11156156B2 (en) 2018-10-04 2021-10-26 Raytheon Technologies Corporation Gas turbine engine with a unitary structure and method for manufacturing the same
DE102019204746A1 (de) 2019-04-03 2020-10-08 Siemens Aktiengesellschaft Hitzeschildkachel mit Dämpfungsfunktion
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
US12454912B2 (en) 2020-12-03 2025-10-28 Rtx Corporation Supplemental thrust system for a gas turbine engine

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1217843A (fr) * 1958-12-10 1960-05-05 Snecma Brûleur de combustion ou de post-combustion pour combustible chaud
DE1235670B (de) * 1962-11-06 1967-03-02 Deutsche Forsch Luft Raumfahrt Vorrichtung zur Flammenstabilisierung in Gleichdruck-Brennkammern
DE1800611A1 (de) * 1968-10-02 1970-05-27 Hertel Dr Ing Heinrich Anordnung zum Einspritzen von Kraftstoff in einen an einer Einspritzduese mit UEberschallgeschwindigkeit vorbeistroemenden Luftstrom
DE1926728B1 (de) * 1969-05-24 1971-03-25 Messerschmitt Boelkow Blohm Brennkammer fuer Strahltriebwerke,insbesondere fuer Raketen-Staustrahltriebwerke
GB1283827A (en) * 1970-09-26 1972-08-02 Rolls Royce Improvements in or relating to combustion apparatus
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
US4255777A (en) * 1977-11-21 1981-03-10 Exxon Research & Engineering Co. Electrostatic atomizing device
US4581675A (en) * 1980-09-02 1986-04-08 Exxon Research And Engineering Co. Electrostatic atomizing device
US4683541A (en) * 1985-03-13 1987-07-28 David Constant V Rotary fluidized bed combustion system
US4821512A (en) * 1987-05-05 1989-04-18 United Technologies Corporation Piloting igniter for supersonic combustor
US4793305A (en) * 1987-07-16 1988-12-27 Dresser Industries, Inc. High turbulence combustion chamber for turbocharged lean burn gaseous fueled engine
US4896501A (en) * 1987-10-22 1990-01-30 Faulkner Robie L Turbojet engine with sonic injection afterburner
US5070690A (en) * 1989-04-26 1991-12-10 General Electric Company Means and method for reducing differential pressure loading in an augmented gas turbine engine
US4991774A (en) * 1989-08-24 1991-02-12 Charged Injection Corporation Electrostatic injector using vapor and mist insulation
US5093602A (en) * 1989-11-17 1992-03-03 Charged Injection Corporation Methods and apparatus for dispersing a fluent material utilizing an electron beam
RU2035008C1 (ru) * 1992-05-28 1995-05-10 Михаил Яковлевич Бобрик Способ сжигания углеводородного топлива
US5341640A (en) * 1993-03-30 1994-08-30 Faulkner Robie L Turbojet engine with afterburner and thrust augmentation ejectors
US5515681A (en) * 1993-05-26 1996-05-14 Simmonds Precision Engine Systems Commonly housed electrostatic fuel atomizer and igniter apparatus for combustors
CH688899A5 (de) * 1994-05-26 1998-05-15 Asea Brown Boveri Verfahren zur Regelung einer Gasturbogruppe.
JPH08193716A (ja) * 1995-01-17 1996-07-30 Hitachi Ltd ガスタービン燃焼器
RU2116567C1 (ru) * 1996-03-11 1998-07-27 Акционерное общество открытого типа "Северсталь" Многоствольное эжекторное горелочное устройство
US6112512A (en) * 1997-08-05 2000-09-05 Lockheed Martin Corporation Method and apparatus of pulsed injection for improved nozzle flow control
GB2390150A (en) * 2002-06-26 2003-12-31 Alstom Reheat combustion system for a gas turbine including an accoustic screen
US6883302B2 (en) * 2002-12-20 2005-04-26 General Electric Company Methods and apparatus for generating gas turbine engine thrust with a pulse detonation thrust augmenter
FR2858661B1 (fr) * 2003-08-05 2005-10-07 Snecma Moteurs Dispositif de post-combustion

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