ES2160804T3 - Procedimiento para quemar un combustible en una turbina de gas, asi como la correspondiente turbina de gas. - Google Patents

Procedimiento para quemar un combustible en una turbina de gas, asi como la correspondiente turbina de gas.

Info

Publication number
ES2160804T3
ES2160804T3 ES96905682T ES96905682T ES2160804T3 ES 2160804 T3 ES2160804 T3 ES 2160804T3 ES 96905682 T ES96905682 T ES 96905682T ES 96905682 T ES96905682 T ES 96905682T ES 2160804 T3 ES2160804 T3 ES 2160804T3
Authority
ES
Spain
Prior art keywords
gas turbine
fuel
compression section
torsion
burn
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.)
Expired - Lifetime
Application number
ES96905682T
Other languages
English (en)
Inventor
Manfred Ziegner
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.)
Siemens AG
Siemens Corp
Original Assignee
Siemens AG
Siemens Corp
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 Siemens AG, Siemens Corp filed Critical Siemens AG
Application granted granted Critical
Publication of ES2160804T3 publication Critical patent/ES2160804T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/425—Combustion chambers comprising a tangential or helicoidal arrangement of the flame tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

LA INVENCION CONCIERNE A UN METODO PARA QUEMAR UN MATERIAL COMBUSTIBLE (5) EN UNA CORRIENTE (4) DE AIRE COMPRIMIDO QUE FLUYE A TRAVES DE UNA TURBINA DE GAS (1) DESDE UNA SECCION DE COMPRESION (2) A UNA SECCION DE TURBINA (3), ENTRE LAS CUALES SE PRODUCE LA COMBUSTION DEL MATERIAL, Y TAMBIEN CONCIERNE A UNA TURBINA DE GAS ADECUADA. EN LA SECCION DE COMPRESION (2) SE INYECTA EL COMBUSTIBLE EN EL FLUJO DE CORRIENTE (4). PARA EL GUIADO DE LA CORRIENTE (4) SE UTILIZA UN CANAL ANULAR (16), MIENTRAS QUE PARA INYECTAR EL COMBUSTIBLE (5) EN LA SECCION DE COMPRESION (2) SE EMPLEAN TOBERAS (6). CUANDO EL FLUJO DE CORRIENTE SALE DE LA SECCION DE COMPRESION (2), SE LE APLICA UNA PRIMERA TORSION (7) Y AL PRODUCIRSE LA COMBUSTION (4) SE TRANSFORMA EN UNA SEGUNDA TORSION (8). ESTA ULTIMA RESULTA SER LA TORSION NOMINAL QUE SE PRECISA PARA LLEVAR EL FLUJO DE CORRIENTE (4) A LA SECCION DE TURBINA (3).
ES96905682T 1995-03-06 1996-03-05 Procedimiento para quemar un combustible en una turbina de gas, asi como la correspondiente turbina de gas. Expired - Lifetime ES2160804T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19507763A DE19507763A1 (de) 1995-03-06 1995-03-06 Verfahren und Vorrichtung zur Verbrennung eines Brennstoffs in einer Gasturbine

Publications (1)

Publication Number Publication Date
ES2160804T3 true ES2160804T3 (es) 2001-11-16

Family

ID=7755753

Family Applications (1)

Application Number Title Priority Date Filing Date
ES96905682T Expired - Lifetime ES2160804T3 (es) 1995-03-06 1996-03-05 Procedimiento para quemar un combustible en una turbina de gas, asi como la correspondiente turbina de gas.

Country Status (7)

Country Link
US (1) US6003297A (es)
EP (1) EP0813668B1 (es)
JP (1) JP3939753B2 (es)
DE (2) DE19507763A1 (es)
ES (1) ES2160804T3 (es)
IN (1) IN187803B (es)
WO (1) WO1996027764A1 (es)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19641725A1 (de) * 1996-10-10 1998-04-16 Asea Brown Boveri Gasturbine mit einer sequentiellen Verbrennung
US20020166324A1 (en) 1998-04-02 2002-11-14 Capstone Turbine Corporation Integrated turbine power generation system having low pressure supplemental catalytic reactor
US6192668B1 (en) * 1999-10-19 2001-02-27 Capstone Turbine Corporation Method and apparatus for compressing gaseous fuel in a turbine engine
DE10035676A1 (de) * 2000-07-21 2002-02-07 Siemens Ag Gasturbine und Verfahren zum Betrieb einer Gasturbine
AU2002235119A1 (en) * 2000-09-05 2002-05-06 Sudarshan Paul Dev Nested core gas turbine engine
US7784261B2 (en) * 2006-05-25 2010-08-31 Siemens Energy, Inc. Combined cycle power plant
GB0617925D0 (en) * 2006-09-12 2006-10-18 Rolls Royce Plc Components for a gas turbine engine
WO2009082275A1 (en) * 2007-12-20 2009-07-02 Volvo Aero Corporation A gas turbine engine
US8006500B1 (en) * 2008-01-29 2011-08-30 Florida Turbine Technologies, Inc. Swirl combustor with counter swirl fuel slinger
US20150000298A1 (en) * 2013-03-15 2015-01-01 Advanced Green Technologies, Llc Fuel conditioner, combustor and gas turbine improvements
US9599019B2 (en) * 2014-02-05 2017-03-21 United Technologies Corporation Dual oil supply tube
US11499485B2 (en) * 2020-02-10 2022-11-15 Raytheon Technologies Corporation Engine control device and methods thereof

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US32896A (en) * 1861-07-23 Grain threshing aetd separating machine
CH214256A (de) * 1939-06-28 1941-04-15 Bbc Brown Boveri & Cie Verbrennungsturbinenanlage.
DE889242C (de) * 1944-01-18 1953-09-10 Ernst Heinkel Ag Strahltriebwerk
DE847091C (de) * 1944-05-13 1952-08-21 Daimler Benz Ag Heissluftstrahltriebwerk
DE826805C (de) * 1944-11-11 1952-01-07 Maschf Augsburg Nuernberg Ag Gasturbinenanlage
US2630678A (en) * 1947-08-18 1953-03-10 United Aircraft Corp Gas turbine power plant with fuel injection between compressor stages
FR1006128A (fr) * 1947-11-19 1952-04-21 Dispositif d'alimentation et de combustion pour turbines à gaz et turbo-réacteurs
US2671314A (en) * 1950-01-26 1954-03-09 Socony Vacuum Oil Co Inc Gas turbine and method of operation therefor
US2755623A (en) * 1953-02-19 1956-07-24 Ferri Antonio Rotating flow combustor
US3019606A (en) * 1959-09-04 1962-02-06 Avco Corp Combustion section for a gas turbine engine
GB1039677A (en) * 1963-07-10 1966-08-17 Rolls Royce Combustion chamber for a gas turbine engine
GB1048968A (en) * 1964-05-08 1966-11-23 Rolls Royce Combustion chamber for a gas turbine engine
CH419425A (de) * 1964-08-07 1966-08-31 Bbc Brown Boveri & Cie Einrichtung zur Regelung eines Turboverdichters
US3701255A (en) * 1970-10-26 1972-10-31 United Aircraft Corp Shortened afterburner construction for turbine engine
DE2925091A1 (de) * 1979-06-21 1981-01-08 Vinko Dipl Ing Mucic Verbrennungskraftmaschine
JPS5857658B2 (ja) * 1980-04-02 1983-12-21 工業技術院長 セラミツクスによる高熱曝露壁面の熱遮断構造
USRE32896E (en) 1984-06-06 1989-03-28 Ethyl Corporation Gem cyclodialkylation of amines and amides
DE3663189D1 (en) * 1985-03-04 1989-06-08 Siemens Ag Burner disposition for combustion installations, especially for combustion chambers of gas turbine installations, and method for its operation
DE3860569D1 (de) * 1987-01-26 1990-10-18 Siemens Ag Hybridbrenner fuer vormischbetrieb mit gas und/oder oel, insbesondere fuer gasturbinenanlagen.
DE3819898A1 (de) * 1988-06-11 1989-12-14 Daimler Benz Ag Brennkammer fuer eine thermische stroemungsmaschine
US5207064A (en) * 1990-11-21 1993-05-04 General Electric Company Staged, mixed combustor assembly having low emissions
EP0489193B1 (de) * 1990-12-05 1997-07-23 Asea Brown Boveri Ag Gasturbinen-Brennkammer
DE4232383A1 (de) * 1992-09-26 1994-03-31 Asea Brown Boveri Gasturbogruppe
EP0592717B1 (de) * 1992-10-16 1998-02-25 Asea Brown Boveri Ag Gasbetriebener Vormischbrenner

Also Published As

Publication number Publication date
JPH11501380A (ja) 1999-02-02
EP0813668B1 (de) 2001-07-25
DE19507763A1 (de) 1996-09-12
EP0813668A1 (de) 1997-12-29
IN187803B (es) 2002-06-29
DE59607363D1 (de) 2001-08-30
JP3939753B2 (ja) 2007-07-04
WO1996027764A1 (de) 1996-09-12
US6003297A (en) 1999-12-21

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