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MX2013010930A - Montaje de turbina de gas y el metodo de operacion correspondiente. - Google Patents

Montaje de turbina de gas y el metodo de operacion correspondiente.

Info

Publication number
MX2013010930A
MX2013010930A MX2013010930A MX2013010930A MX2013010930A MX 2013010930 A MX2013010930 A MX 2013010930A MX 2013010930 A MX2013010930 A MX 2013010930A MX 2013010930 A MX2013010930 A MX 2013010930A MX 2013010930 A MX2013010930 A MX 2013010930A
Authority
MX
Mexico
Prior art keywords
burner
gas turbine
turbine assembly
operating method
corresponding operating
Prior art date
Application number
MX2013010930A
Other languages
English (en)
Inventor
Adnan Eroglu
Ewald Freitag
Robert Marmilic
Jaan Hellat
Original Assignee
Alstom Technology Ltd
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 Alstom Technology Ltd filed Critical Alstom Technology Ltd
Publication of MX2013010930A publication Critical patent/MX2013010930A/es

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/72—Application in combination with a steam turbine
    • F05D2220/722—Application in combination with a steam turbine as part of an integrated gasification combined cycle
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03341—Sequential combustion chambers or burners
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
    • Y02E20/18—Integrated gasification combined cycle [IGCC], e.g. combined with carbon capture and storage [CCS]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Combustion Of Fluid Fuel (AREA)

Abstract

La invención se refiere a un montaje de turbina de gas que consiste substancialmente de por lo menos un compresor, por lo menos un primer quemador (8, 201), por lo menos un segundo quemador (9, 202) que está conectado corriente abajo del primer quemador, y por lo menos una turbina (5) que está conectada corriente abajo del segundo quemador. Al menos el primer y segundo quemadores (8, 9) forman un componente de elemento de cámara de combustión tubular o cuasi10 tubular (100, 200, 300) en la dirección de flujo de la ruta de combustión de los quemadores, el elemento de cámara de combustión está cerrado o casi cerrado y se extiende entre el compresor (2) y la turbina (5). Los elementos de cámara de combustión están dispuestos alrededor del rotor del montaje de turbina de gas en la forma de un anillo.
MX2013010930A 2011-04-08 2012-04-05 Montaje de turbina de gas y el metodo de operacion correspondiente. MX2013010930A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH00636/11A CH704829A2 (de) 2011-04-08 2011-04-08 Gasturbogruppe und zugehöriges Betriebsverfahren.
PCT/EP2012/056323 WO2012136787A1 (de) 2011-04-08 2012-04-05 Gasturbogruppe und zugehöriges betriebsverfahren

Publications (1)

Publication Number Publication Date
MX2013010930A true MX2013010930A (es) 2014-06-05

Family

ID=46001168

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2013010930A MX2013010930A (es) 2011-04-08 2012-04-05 Montaje de turbina de gas y el metodo de operacion correspondiente.

Country Status (11)

Country Link
US (1) US10774740B2 (es)
EP (1) EP2694878B1 (es)
JP (1) JP5946519B2 (es)
KR (1) KR101638333B1 (es)
CN (1) CN103443542B (es)
BR (1) BR112013025839A2 (es)
CA (1) CA2832493C (es)
CH (1) CH704829A2 (es)
MX (1) MX2013010930A (es)
RU (1) RU2563446C2 (es)
WO (1) WO2012136787A1 (es)

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Also Published As

Publication number Publication date
WO2012136787A1 (de) 2012-10-11
EP2694878A1 (de) 2014-02-12
CA2832493A1 (en) 2012-10-11
EP2694878B1 (de) 2018-12-12
CN103443542B (zh) 2016-10-26
CA2832493C (en) 2017-05-30
CN103443542A (zh) 2013-12-11
JP5946519B2 (ja) 2016-07-06
KR20140027237A (ko) 2014-03-06
BR112013025839A2 (pt) 2016-12-20
KR101638333B1 (ko) 2016-07-12
US10774740B2 (en) 2020-09-15
US20140033728A1 (en) 2014-02-06
JP2014510256A (ja) 2014-04-24
RU2013149862A (ru) 2015-05-20
RU2563446C2 (ru) 2015-09-20
CH704829A2 (de) 2012-11-15

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