IN2014DE02753A - - Google Patents

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Publication number
IN2014DE02753A
IN2014DE02753A IN2753DE2014A IN2014DE02753A IN 2014DE02753 A IN2014DE02753 A IN 2014DE02753A IN 2753DE2014 A IN2753DE2014 A IN 2753DE2014A IN 2014DE02753 A IN2014DE02753 A IN 2014DE02753A
Authority
IN
India
Prior art keywords
combustor
flow
fuel
sequential
gas turbine
Prior art date
Application number
Other languages
English (en)
Inventor
Adnan Eroglu
Juergen Hoffmann
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 IN2014DE02753A publication Critical patent/IN2014DE02753A/en

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • 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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/263—Control of fuel supply by means of fuel metering valves
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
    • F23C6/047—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure with fuel supply in stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N1/00—Regulating fuel supply
    • F23N1/002—Regulating fuel supply using electronic means
    • 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
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2227/00—Ignition or checking
    • F23N2227/10—Sequential burner running
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2237/00—Controlling
    • F23N2237/02—Controlling two or more burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2241/00—Applications
    • F23N2241/20—Gas turbines
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
IN2753DE2014 2013-10-01 2014-09-25 IN2014DE02753A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP13186852.3A EP2857658A1 (de) 2013-10-01 2013-10-01 Gasturbine mit einer sequentiellen Brennanordnung

Publications (1)

Publication Number Publication Date
IN2014DE02753A true IN2014DE02753A (de) 2015-06-26

Family

ID=49303782

Family Applications (1)

Application Number Title Priority Date Filing Date
IN2753DE2014 IN2014DE02753A (de) 2013-10-01 2014-09-25

Country Status (8)

Country Link
US (2) US9708983B2 (de)
EP (1) EP2857658A1 (de)
JP (1) JP2015072114A (de)
KR (1) KR20150039107A (de)
CN (1) CN104633711A (de)
CA (1) CA2865729A1 (de)
IN (1) IN2014DE02753A (de)
RU (1) RU2014138247A (de)

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EP3101342B1 (de) * 2015-06-02 2020-04-29 Ansaldo Energia IP UK Limited Verfahren und system zum betrieb einer verbrennungsvorrichtung
FR3037384B1 (fr) * 2015-06-11 2017-06-23 Turbomeca Module de chambre de combustion cvc de turbomachine comportant une prechambre de combustion
EP3135880B1 (de) * 2015-08-25 2020-07-08 Ansaldo Energia IP UK Limited Gasturbine mit sequentieller verbrennungsanordnung und brennstoffzusammensetzungssteuerung
EP3228939B1 (de) * 2016-04-08 2020-08-05 Ansaldo Energia Switzerland AG Verfahren zur verbrennung eines brennstoffs und verbrennungsvorrichtung
EP3421761B1 (de) * 2017-06-30 2020-11-25 Ansaldo Energia IP UK Limited Sekundäre brennkammer für eine sequentielle gasturbinenbrennkammer
RU2747655C2 (ru) * 2017-11-17 2021-05-11 Ансальдо Энергия Свитзерленд Аг Горелка промежуточного подогрева для газовой турбины и газовая турбина, содержащая такую горелку промежуточного подогрева
FR3076320B1 (fr) * 2017-12-28 2020-02-07 Safran Aircraft Engines Procede de commande de l'alimentation en carburant d'une chambre de combustion d'une turbomachine, systeme d'alimentation en carburant et turbomachine
US11085321B2 (en) * 2018-01-30 2021-08-10 Honeywell International Inc. Bleed air compensated continuous power assurance analysis system and method
EP3524799A1 (de) * 2018-02-13 2019-08-14 Siemens Aktiengesellschaft Verfahren zum betreiben einer brenneranordnung einer gasturbine
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
JP7231493B2 (ja) * 2019-06-12 2023-03-01 三菱重工業株式会社 制御装置、ガスタービン、制御方法及びプログラム
EP3822469B1 (de) * 2019-11-18 2023-01-04 Ansaldo Energia Switzerland AG Gasturbinentriebwerk mit wechselnden mustern von aktiven brennern und verfahren zur steuerung eines gasturbinentriebwerks
EP4019844B1 (de) * 2020-12-24 2024-04-03 Ansaldo Energia Switzerland AG Gasturbinenmotor mit erster und zweiter kraftstoffstufensteuerung und verfahren zur steuerung eines gasturbinenmotors
EP4343131A1 (de) * 2022-09-23 2024-03-27 General Electric Technology GmbH Verfahren zum betrieb eines verbrennungssystems, verbrennungssystem und gasturbine mit diesem verbrennungssystem

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Also Published As

Publication number Publication date
US20170298837A1 (en) 2017-10-19
RU2014138247A (ru) 2016-04-10
JP2015072114A (ja) 2015-04-16
US9708983B2 (en) 2017-07-18
CN104633711A (zh) 2015-05-20
CA2865729A1 (en) 2015-04-01
US20150107259A1 (en) 2015-04-23
EP2857658A1 (de) 2015-04-08
KR20150039107A (ko) 2015-04-09

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