FR2092926B2 - - Google Patents

Info

Publication number
FR2092926B2
FR2092926B2 FR707045028A FR7045028A FR2092926B2 FR 2092926 B2 FR2092926 B2 FR 2092926B2 FR 707045028 A FR707045028 A FR 707045028A FR 7045028 A FR7045028 A FR 7045028A FR 2092926 B2 FR2092926 B2 FR 2092926B2
Authority
FR
France
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.)
Expired
Application number
FR707045028A
Other versions
FR2092926A2 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MTU Aero Engines GmbH
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2092926A2 publication Critical patent/FR2092926A2/fr
Application granted granted Critical
Publication of FR2092926B2 publication Critical patent/FR2092926B2/fr
Expired legal-status Critical Current

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/40—Movement of component
    • F05B2250/41—Movement of component with one degree of freedom

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Combustion (AREA)
FR707045028A 1970-04-27 1970-12-14 Expired FR2092926B2 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19702020416 DE2020416A1 (de) 1970-04-27 1970-04-27 Brennkammer fuer Gasturbinentriebwerke

Publications (2)

Publication Number Publication Date
FR2092926A2 FR2092926A2 (fr) 1972-01-28
FR2092926B2 true FR2092926B2 (fr) 1973-02-02

Family

ID=5769451

Family Applications (1)

Application Number Title Priority Date Filing Date
FR707045028A Expired FR2092926B2 (fr) 1970-04-27 1970-12-14

Country Status (3)

Country Link
US (1) US3765171A (fr)
DE (1) DE2020416A1 (fr)
FR (1) FR2092926B2 (fr)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3952501A (en) * 1971-04-15 1976-04-27 United Aircraft Of Canada Limited Gas turbine control
US3975900A (en) * 1972-02-18 1976-08-24 Engelhard Minerals & Chemicals Corporation Method and apparatus for turbine system combustor temperature
US4179880A (en) * 1973-12-06 1979-12-25 Phillips Petroleum Company Combustion process and apparatus therefor
DE2416909A1 (de) * 1974-04-06 1975-10-16 Daimler Benz Ag Betriebsverfahren fuer eine gasturbinenanlage zur abgasverbesserung und entsprechende gasturbinenanlage
US3958413A (en) * 1974-09-03 1976-05-25 General Motors Corporation Combustion method and apparatus
FR2289738A2 (fr) * 1974-10-30 1976-05-28 Engelhard Min & Chem Procede et appareillage d'obtention d'une combustion entretenue dans une turbine a gaz
US3930368A (en) * 1974-12-12 1976-01-06 General Motors Corporation Combustion liner air valve
US4138842A (en) * 1975-11-05 1979-02-13 Zwick Eugene B Low emission combustion apparatus
US4050240A (en) * 1976-08-26 1977-09-27 General Motors Corporation Variable air admission device for a combustor assembly
WO1979001071A1 (fr) * 1978-05-15 1979-12-13 Purification Sciences Inc Moteur
US4296599A (en) * 1979-03-30 1981-10-27 General Electric Company Turbine cooling air modulation apparatus
JPS61195214A (ja) * 1985-02-22 1986-08-29 Hitachi Ltd ガスタ−ビン燃焼器の空気流量調整機構
US4944149A (en) * 1988-12-14 1990-07-31 General Electric Company Combustor liner with air staging for NOx control
FR2661714B1 (fr) * 1990-05-03 1994-06-17 Snecma Dispositif d'alimentation en comburant d'une turbine a gaz.
KR930013441A (ko) * 1991-12-18 1993-07-21 아더 엠.킹 다수의 연소기들을 포함한 가스터어빈 연소장치
US5685156A (en) * 1996-05-20 1997-11-11 Capstone Turbine Corporation Catalytic combustion system
FR2779807B1 (fr) * 1998-06-11 2000-07-13 Inst Francais Du Petrole Chambre de combustion de turbine a gaz a geometrie variable
DE19829398A1 (de) * 1998-07-01 2000-01-05 Asea Brown Boveri Gasturbine
US6453658B1 (en) 2000-02-24 2002-09-24 Capstone Turbine Corporation Multi-stage multi-plane combustion system for a gas turbine engine
NO318619B1 (no) * 2000-12-29 2005-04-18 Norsk Hydro As Anordning for forbrenning av et karbonholdig brensel, en fremgangsmate for a betjene nevnte anordning, samt anvendelse av anordningen.
US6609362B2 (en) * 2001-07-13 2003-08-26 Pratt & Whitney Canada Corp. Apparatus for adjusting combustor cycle
AUPR657901A0 (en) * 2001-07-25 2001-08-16 Micro Gas Turbine Pty Ltd A miniature multifuel gas turbine engine
SE523082C2 (sv) * 2001-11-20 2004-03-23 Volvo Aero Corp Anordning vid en brännkammare hos en gasturbin för reglering av inflöde av gas till brännkammarens förbränningszon
JP3978086B2 (ja) * 2002-05-31 2007-09-19 三菱重工業株式会社 航空機用ガスタービンシステム，及びガスタービンシステム並びにその動作方法
US20090260340A1 (en) * 2008-04-17 2009-10-22 General Electric Company Combustor of a Turbine, a Method of Retro-Fitting a Combustor of a Turbine and a Method of Building a Combustor of a Turbine
GB0815761D0 (en) * 2008-09-01 2008-10-08 Rolls Royce Plc Swirler for a fuel injector
US20110047961A1 (en) * 2009-08-28 2011-03-03 General Electric Company Pulse detonation inlet management system
RU2010101978A (ru) * 2010-01-15 2011-07-20 Дженерал Электрик Компани (US) Соединительный узел для газовой турбины
US9115669B2 (en) * 2011-10-28 2015-08-25 United Technologies Corporation Gas turbine engine exhaust nozzle cooling valve
US9010082B2 (en) * 2012-01-03 2015-04-21 General Electric Company Turbine engine and method for flowing air in a turbine engine
US9181813B2 (en) 2012-07-05 2015-11-10 Siemens Aktiengesellschaft Air regulation for film cooling and emission control of combustion gas structure
WO2014133615A1 (fr) * 2013-03-01 2014-09-04 Rolls-Royce Corporation Joint à bande bimétallique
US20150082794A1 (en) * 2013-09-26 2015-03-26 Reinhard Schilp Apparatus for acoustic damping and operational control of damping, cooling, and emissions in a gas turbine engine
FR3026469B1 (fr) * 2014-09-26 2019-04-19 Safran Aircraft Engines Paroi annulaire de chambre de combustion a alimentation d'air regule localement
FR3049044B1 (fr) * 2016-03-18 2019-12-20 IFP Energies Nouvelles Chambre de combustion d'une turbine, notamment d'une turbine a cycle thermodynamique avec recuperateur, pour la production d'energie, en particulier d'energie electrique.
FR3065059B1 (fr) * 2017-04-11 2020-11-06 Office National Detudes Rech Aerospatiales Foyer de turbine a gaz a geometrie variable auto-adaptative
US20220390114A1 (en) * 2021-06-07 2022-12-08 General Electric Company Combustor for a gas turbine engine
CN116592391A (zh) * 2022-02-07 2023-08-15 通用电气公司 具有可变初级区燃烧室的燃烧器
CN116592392A (zh) * 2022-02-07 2023-08-15 通用电气公司 操作具有可变燃烧室的燃烧器的方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2482394A (en) * 1945-02-12 1949-09-20 Edwin T Wyman Gas turbine
US2621477A (en) * 1948-06-03 1952-12-16 Power Jets Res & Dev Ltd Combustion apparatus having valve controlled passages for preheating the fuel-air mixture
US2655787A (en) * 1949-11-21 1953-10-20 United Aircraft Corp Gas turbine combustion chamber with variable area primary air inlet
US2770096A (en) * 1952-09-15 1956-11-13 Phillips Petroleum Co Continuous combustion chamber with air flow and turbulence controlled by flame frontposition
US2837893A (en) * 1952-12-12 1958-06-10 Phillips Petroleum Co Automatic primary and secondary air flow regulation for gas turbine combustion chamber
US3078672A (en) * 1959-03-28 1963-02-26 Maschf Augsburg Nuernberg Ag Process and apparatus for operating a continuous or intermittent combustion engine
US3577878A (en) * 1967-11-10 1971-05-11 Lucas Industries Ltd Flame tubes for gas turbine engines
US3584459A (en) * 1968-09-12 1971-06-15 Gen Motors Corp Gas turbine engine with combustion chamber bypass for fuel-air ratio control and turbine cooling

Also Published As

Publication number Publication date
FR2092926A2 (fr) 1972-01-28
US3765171A (en) 1973-10-16
DE2020416A1 (de) 1971-11-11

Similar Documents

Publication Publication Date Title
FR2092926B2 (fr)
AU1473870A (fr)
AU2044470A (fr)
AU2017870A (fr)
AU1833270A (fr)
AU1716970A (fr)
AU2085370A (fr)
AU2130570A (fr)
AU1517670A (fr)
AU1336970A (fr)
AU2112570A (fr)
AU1689770A (fr)
AU1343870A (fr)
AU1789870A (fr)
AU1581370A (fr)
AU1841070A (fr)
AU1872870A (fr)
AU1879170A (fr)
AU1881070A (fr)
AU1918570A (fr)
AU1943370A (fr)
AU1969370A (fr)
AU1974970A (fr)
AU1247570A (fr)
AU1832970A (fr)