RU2406034C2 - Газотурбинная горелка и способ эксплуатации газотурбинной горелки - Google Patents

Газотурбинная горелка и способ эксплуатации газотурбинной горелки Download PDF

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Publication number
RU2406034C2
RU2406034C2 RU2008138545/06A RU2008138545A RU2406034C2 RU 2406034 C2 RU2406034 C2 RU 2406034C2 RU 2008138545/06 A RU2008138545/06 A RU 2008138545/06A RU 2008138545 A RU2008138545 A RU 2008138545A RU 2406034 C2 RU2406034 C2 RU 2406034C2
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RU
Russia
Prior art keywords
fuel
gas
gaseous fuel
exhaust gas
turbine burner
Prior art date
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RU2008138545/06A
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English (en)
Russian (ru)
Other versions
RU2008138545A (ru
Inventor
Андреас ХЕЙЛОС (DE)
Андреас ХЕЙЛОС
Вернер КРЕБС (DE)
Вернер КРЕБС
КАМПЕН Яп ВАН (NL)
КАМПЕН Яп ВАН
Original Assignee
Сименс Акциенгезелльшафт
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.)
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Application filed by Сименс Акциенгезелльшафт filed Critical Сименс Акциенгезелльшафт
Publication of RU2008138545A publication Critical patent/RU2008138545A/ru
Application granted granted Critical
Publication of RU2406034C2 publication Critical patent/RU2406034C2/ru

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    • 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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • F23R3/24—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants of the fluid-screen type

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
RU2008138545/06A 2006-02-28 2007-02-20 Газотурбинная горелка и способ эксплуатации газотурбинной горелки RU2406034C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006009562.6 2006-02-28
DE102006009562 2006-02-28

Publications (2)

Publication Number Publication Date
RU2008138545A RU2008138545A (ru) 2010-04-10
RU2406034C2 true RU2406034C2 (ru) 2010-12-10

Family

ID=38009771

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2008138545/06A RU2406034C2 (ru) 2006-02-28 2007-02-20 Газотурбинная горелка и способ эксплуатации газотурбинной горелки

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

Citations (7)

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US4896501A (en) * 1987-10-22 1990-01-30 Faulkner Robie L Turbojet engine with sonic injection afterburner
US5341640A (en) * 1993-03-30 1994-08-30 Faulkner Robie L Turbojet engine with afterburner and thrust augmentation ejectors
RU2035008C1 (ru) * 1992-05-28 1995-05-10 Михаил Яковлевич Бобрик Способ сжигания углеводородного топлива
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
RU2003136814A (ru) * 2002-12-20 2005-05-20 Дженерал Электрик Компани (US) Импульсная детонационная система для газотурбинного двигателя и гахотурбинный двигатель с такой системой
RU2004123918A (ru) * 2003-08-05 2006-01-27 Снекма Мотер (Fr) Форсажное кольцо для двухконтурного турбореактивного двигателя, форсажное устройство и турбореактивный двигатель

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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
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
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
GB2390150A (en) * 2002-06-26 2003-12-31 Alstom Reheat combustion system for a gas turbine including an accoustic screen

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4896501A (en) * 1987-10-22 1990-01-30 Faulkner Robie L Turbojet engine with sonic injection afterburner
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
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
RU2003136814A (ru) * 2002-12-20 2005-05-20 Дженерал Электрик Компани (US) Импульсная детонационная система для газотурбинного двигателя и гахотурбинный двигатель с такой системой
RU2004123918A (ru) * 2003-08-05 2006-01-27 Снекма Мотер (Fr) Форсажное кольцо для двухконтурного турбореактивного двигателя, форсажное устройство и турбореактивный двигатель

Also Published As

Publication number Publication date
RU2008138545A (ru) 2010-04-10
EP1989486A1 (de) 2008-11-12
CN101395428A (zh) 2009-03-25
US20100043440A1 (en) 2010-02-25
JP2009528503A (ja) 2009-08-06
CN101395428B (zh) 2010-12-08
WO2007099046A1 (de) 2007-09-07
JP4776697B2 (ja) 2011-09-21

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20200221