DE2020416A1 - Brennkammer fuer Gasturbinentriebwerke - Google Patents

Brennkammer fuer Gasturbinentriebwerke

Info

Publication number
DE2020416A1
DE2020416A1 DE19702020416 DE2020416A DE2020416A1 DE 2020416 A1 DE2020416 A1 DE 2020416A1 DE 19702020416 DE19702020416 DE 19702020416 DE 2020416 A DE2020416 A DE 2020416A DE 2020416 A1 DE2020416 A1 DE 2020416A1
Authority
DE
Germany
Prior art keywords
combustion chamber
secondary air
sections
air
cross
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.)
Pending
Application number
DE19702020416
Other languages
German (de)
English (en)
Inventor
Hagen Hermann Dr Techn
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 AG
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
Priority to DE19702020416 priority Critical patent/DE2020416A1/de
Priority to GB43662/70A priority patent/GB1277980A/en
Priority to FR707045028A priority patent/FR2092926B2/fr
Priority to US00123164A priority patent/US3765171A/en
Publication of DE2020416A1 publication Critical patent/DE2020416A1/de
Pending legal-status Critical Current

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
    • F23R3/26Controlling the air flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00Geometry
    • F05B2250/40Movement of component
    • F05B2250/41Movement 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)
DE19702020416 1969-09-11 1970-04-27 Brennkammer fuer Gasturbinentriebwerke Pending DE2020416A1 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE19702020416 DE2020416A1 (de) 1970-04-27 1970-04-27 Brennkammer fuer Gasturbinentriebwerke
GB43662/70A GB1277980A (en) 1969-09-11 1970-09-11 Gas turbine engines
FR707045028A FR2092926B2 (enExample) 1970-04-27 1970-12-14
US00123164A US3765171A (en) 1970-04-27 1971-03-11 Combustion chamber for gas turbine engines

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
DE2020416A1 true DE2020416A1 (de) 1971-11-11

Family

ID=5769451

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19702020416 Pending DE2020416A1 (de) 1969-09-11 1970-04-27 Brennkammer fuer Gasturbinentriebwerke

Country Status (3)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19829398A1 (de) * 1998-07-01 2000-01-05 Asea Brown Boveri Gasturbine

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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 (en) * 1978-05-15 1979-12-13 Purification Sciences Inc Engine
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
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 (en) * 2013-03-01 2014-09-04 Rolls-Royce Corporation Bi-metal strip-seal
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
US12085283B2 (en) * 2021-06-07 2024-09-10 General Electric Company Combustor for a gas turbine engine
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
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
FR3145795A1 (fr) * 2023-02-13 2024-08-16 Safran Aircraft Engines Ensemble pour turbomachine et turbomachine associee
US20240318821A1 (en) * 2023-03-20 2024-09-26 General Electric Company Combustor with a dilution passage

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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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19829398A1 (de) * 1998-07-01 2000-01-05 Asea Brown Boveri Gasturbine

Also Published As

Publication number Publication date
FR2092926B2 (enExample) 1973-02-02
US3765171A (en) 1973-10-16
FR2092926A2 (enExample) 1972-01-28

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