WO2014071120A3 - System and method for a turbine combustor - Google Patents

System and method for a turbine combustor Download PDF

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Publication number
WO2014071120A3
WO2014071120A3 PCT/US2013/067948 US2013067948W WO2014071120A3 WO 2014071120 A3 WO2014071120 A3 WO 2014071120A3 US 2013067948 W US2013067948 W US 2013067948W WO 2014071120 A3 WO2014071120 A3 WO 2014071120A3
Authority
WO
WIPO (PCT)
Prior art keywords
head end
chamber
turbine combustor
end chamber
flow
Prior art date
Application number
PCT/US2013/067948
Other languages
French (fr)
Other versions
WO2014071120A2 (en
Inventor
Carolyn Ashley Antoniono
William Lawrence Byrne
Elizabeth Angelyn Fadde
Original Assignee
General Electric Company
Exxonmobil Upstream Research Company
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
Priority claimed from US14/067,714 external-priority patent/US9631815B2/en
Application filed by General Electric Company, Exxonmobil Upstream Research Company filed Critical General Electric Company
Publication of WO2014071120A2 publication Critical patent/WO2014071120A2/en
Publication of WO2014071120A3 publication Critical patent/WO2014071120A3/en

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
    • F23R3/04—Air inlet arrangements
    • 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 
    • F23C9/00—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
    • 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
    • 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
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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 
    • F23C2202/00—Fluegas recirculation
    • F23C2202/30—Premixing fluegas with combustion air
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Abstract

A system including a turbine combustor (160) with a head end portion (166) having a head end chamber, a combustion portion (168) having a combustion chamber disposed downstream from the head end chamber, a cap (331) disposed between the head end chamber and the combustion chamber, and a flow distributor (332) configured to distribure at least one of an exhaust flow, an oxidant flow, an oxidant-exhaust mixture, or any combination thereof circumferentially around the head end chamber.
PCT/US2013/067948 2012-11-02 2013-11-01 System and method for a turbine combustor WO2014071120A2 (en)

Applications Claiming Priority (12)

Application Number Priority Date Filing Date Title
US201261722114P 2012-11-02 2012-11-02
US201261722118P 2012-11-02 2012-11-02
US201261722111P 2012-11-02 2012-11-02
US201261722115P 2012-11-02 2012-11-02
US61/722,114 2012-11-02
US61/722,111 2012-11-02
US61/722,115 2012-11-02
US61/722,118 2012-11-02
US201261747201P 2012-12-28 2012-12-28
US61/747,201 2012-12-28
US14/067,714 2013-10-30
US14/067,714 US9631815B2 (en) 2012-12-28 2013-10-30 System and method for a turbine combustor

Publications (2)

Publication Number Publication Date
WO2014071120A2 WO2014071120A2 (en) 2014-05-08
WO2014071120A3 true WO2014071120A3 (en) 2014-11-27

Family

ID=50628252

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2013/067948 WO2014071120A2 (en) 2012-11-02 2013-11-01 System and method for a turbine combustor

Country Status (1)

Country Link
WO (1) WO2014071120A2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10378773B2 (en) 2014-09-19 2019-08-13 United Technologies Corporation Turbine engine diffuser assembly with airflow mixer

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6430933B1 (en) * 1998-09-10 2002-08-13 Alstom Oscillation attenuation in combustors
US20060101801A1 (en) * 2004-11-18 2006-05-18 Siemens Westinghouse Power Corporation Combustor flow sleeve with optimized cooling and airflow distribution
US20100275601A1 (en) * 2009-05-01 2010-11-04 General Electric Company Turbine air flow conditioner
WO2010141777A1 (en) * 2009-06-05 2010-12-09 Exxonmobil Upstream Research Company Combustor systems and methods for using same
US20120167586A1 (en) * 2011-01-05 2012-07-05 Donald Mark Bailey Fuel Nozzle Passive Purge Cap Flow
US8281596B1 (en) * 2011-05-16 2012-10-09 General Electric Company Combustor assembly for a turbomachine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6430933B1 (en) * 1998-09-10 2002-08-13 Alstom Oscillation attenuation in combustors
US20060101801A1 (en) * 2004-11-18 2006-05-18 Siemens Westinghouse Power Corporation Combustor flow sleeve with optimized cooling and airflow distribution
US20100275601A1 (en) * 2009-05-01 2010-11-04 General Electric Company Turbine air flow conditioner
WO2010141777A1 (en) * 2009-06-05 2010-12-09 Exxonmobil Upstream Research Company Combustor systems and methods for using same
US20120167586A1 (en) * 2011-01-05 2012-07-05 Donald Mark Bailey Fuel Nozzle Passive Purge Cap Flow
US8281596B1 (en) * 2011-05-16 2012-10-09 General Electric Company Combustor assembly for a turbomachine

Also Published As

Publication number Publication date
WO2014071120A2 (en) 2014-05-08

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