GB2040031B - Dual stage-dual mode low emission gas turbine combustion system - Google Patents

Dual stage-dual mode low emission gas turbine combustion system

Info

Publication number
GB2040031B
GB2040031B GB7904381A GB7943381A GB2040031B GB 2040031 B GB2040031 B GB 2040031B GB 7904381 A GB7904381 A GB 7904381A GB 7943381 A GB7943381 A GB 7943381A GB 2040031 B GB2040031 B GB 2040031B
Authority
GB
United Kingdom
Prior art keywords
dual
gas turbine
combustion system
low emission
turbine combustion
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
Application number
GB7904381A
Other versions
GB2040031A (en
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB2040031A publication Critical patent/GB2040031A/en
Application granted granted Critical
Publication of GB2040031B publication Critical patent/GB2040031B/en
Expired 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • 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
    • F02C9/32—Control of fuel supply characterised by throttling of fuel
    • F02C9/34—Joint control of separate flows to main and auxiliary burners
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/31—Fuel schedule for stage combustors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)
GB7904381A 1979-01-12 1979-12-17 Dual stage-dual mode low emission gas turbine combustion system Expired GB2040031B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US301679A 1979-01-12 1979-01-12

Publications (2)

Publication Number Publication Date
GB2040031A GB2040031A (en) 1980-08-20
GB2040031B true GB2040031B (en) 1983-02-09

Family

ID=21703684

Family Applications (2)

Application Number Title Priority Date Filing Date
GB7904381A Expired GB2040031B (en) 1979-01-12 1979-12-17 Dual stage-dual mode low emission gas turbine combustion system
GB8201277A Expired GB2098720B (en) 1979-01-12 1979-12-17 Stationary gas turbine combustor arrangements

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB8201277A Expired GB2098720B (en) 1979-01-12 1979-12-17 Stationary gas turbine combustor arrangements

Country Status (7)

Country Link
JP (1) JPS55112933A (en)
DE (1) DE3000672A1 (en)
FR (1) FR2446443A1 (en)
GB (2) GB2040031B (en)
IT (1) IT1130186B (en)
NL (1) NL187769C (en)
NO (1) NO150616C (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU559254B2 (en) * 1981-03-05 1987-03-05 Westinghouse Electric Corporation Catalytic gas turbine combustor fuel supply
US4545196A (en) * 1982-07-22 1985-10-08 The Garrett Corporation Variable geometry combustor apparatus
CA1209810A (en) * 1982-10-15 1986-08-19 Paul E. Scheihing Turbine combustor having improved secondary nozzle structure for more uniform mixing of fuel and air and improved downstream combustion
JPS6057131A (en) * 1983-09-08 1985-04-02 Hitachi Ltd Fuel feeding process for gas turbine combustor
JPS6429477U (en) * 1987-08-13 1989-02-22
US5237812A (en) * 1992-10-07 1993-08-24 Westinghouse Electric Corp. Auto-ignition system for premixed gas turbine combustors
US5487275A (en) * 1992-12-11 1996-01-30 General Electric Co. Tertiary fuel injection system for use in a dry low NOx combustion system
US5465570A (en) * 1993-12-22 1995-11-14 United Technologies Corporation Fuel control system for a staged combustor
DE4429757A1 (en) * 1994-08-22 1996-02-29 Abb Management Ag Two=stage combustion chamber
DE4441235A1 (en) * 1994-11-19 1996-05-23 Abb Management Ag Combustion chamber with multi-stage combustion
DE19649486A1 (en) * 1996-11-29 1998-06-04 Abb Research Ltd Combustion chamber
DE19728375A1 (en) * 1997-07-03 1999-01-07 Bmw Rolls Royce Gmbh Operating method for aircraft gas turbine engines
ITMI20032327A1 (en) * 2003-11-28 2005-05-29 Techint Spa GAS BURNER WITH LOW POLLUTING EMISSIONS.
DE102005060704A1 (en) 2005-12-19 2007-06-28 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustor
RU2534189C2 (en) * 2010-02-16 2014-11-27 Дженерал Электрик Компани Gas turbine combustion chamber (versions) and method of its operation
FR2969703B1 (en) * 2010-12-23 2014-11-28 Snecma FUEL SUPPLY METHOD OF A TURBOMACHINE
JP6906381B2 (en) * 2017-07-03 2021-07-21 株式会社東芝 Combustion equipment and gas turbine
CN114353121B (en) * 2022-01-18 2022-12-20 上海交通大学 Multi-nozzle fuel injection method for gas turbine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB726491A (en) * 1952-07-16 1955-03-16 Onera (Off Nat Aerospatiale) Improvements in internal combustion engines through which a continuous gaseous stream is flowing and in particular in turbo-jet and turbo-prop engines
US3728039A (en) * 1966-11-02 1973-04-17 Gen Electric Fluid cooled porous stator structure
AT279483B (en) * 1968-10-18 1970-03-10 Flensburger Maschinenbau Ansta LOADING TRUCK, IN PARTICULAR FOR TRANSPORTING HOT BLACK CEILING MIXED MATERIAL
US3777484A (en) * 1971-12-08 1973-12-11 Gen Electric Shrouded combustion liner
US3872664A (en) * 1973-10-15 1975-03-25 United Aircraft Corp Swirl combustor with vortex burning and mixing
GB1489339A (en) * 1973-11-30 1977-10-19 Rolls Royce Gas turbine engine combustion chambers
US3958413A (en) * 1974-09-03 1976-05-25 General Motors Corporation Combustion method and apparatus
US3958416A (en) * 1974-12-12 1976-05-25 General Motors Corporation Combustion apparatus
US3973390A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Combustor employing serially staged pilot combustion, fuel vaporization, and primary combustion zones
US3946553A (en) * 1975-03-10 1976-03-30 United Technologies Corporation Two-stage premixed combustor
JPS51123413A (en) * 1975-04-19 1976-10-28 Nissan Motor Co Ltd Combustion system of gas turbine
DE2629761A1 (en) * 1976-07-02 1978-01-05 Volkswagenwerk Ag COMBUSTION CHAMBER FOR GAS TURBINES
US4118171A (en) * 1976-12-22 1978-10-03 Engelhard Minerals & Chemicals Corporation Method for effecting sustained combustion of carbonaceous fuel
JPS5426481U (en) * 1977-07-26 1979-02-21
US4253301A (en) * 1978-10-13 1981-03-03 General Electric Company Fuel injection staged sectoral combustor for burning low-BTU fuel gas

Also Published As

Publication number Publication date
NL7909203A (en) 1980-07-15
GB2098720A (en) 1982-11-24
DE3000672A1 (en) 1980-07-24
NO150616B (en) 1984-08-06
IT8019051A0 (en) 1980-01-07
NL187769B (en) 1991-08-01
JPS638373B2 (en) 1988-02-22
GB2040031A (en) 1980-08-20
FR2446443B1 (en) 1983-10-28
DE3000672C2 (en) 1989-02-09
NO794284L (en) 1980-07-15
GB2098720B (en) 1983-04-27
FR2446443A1 (en) 1980-08-08
NL187769C (en) 1992-01-02
JPS55112933A (en) 1980-09-01
NO150616C (en) 1984-11-14
IT1130186B (en) 1986-06-11

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19961217