EP0335978A4 - Gas turbine combustor. - Google Patents

Gas turbine combustor.

Info

Publication number
EP0335978A4
EP0335978A4 EP19880907798 EP88907798A EP0335978A4 EP 0335978 A4 EP0335978 A4 EP 0335978A4 EP 19880907798 EP19880907798 EP 19880907798 EP 88907798 A EP88907798 A EP 88907798A EP 0335978 A4 EP0335978 A4 EP 0335978A4
Authority
EP
European Patent Office
Prior art keywords
premixed gas
main
gas turbine
nozzle
auxiliary
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.)
Granted
Application number
EP19880907798
Other languages
German (de)
French (fr)
Other versions
EP0335978A1 (en
EP0335978B1 (en
Inventor
Yasuo Iwai
Shigeru Azuhata
Kenichi Sohma
Kiyoshi Narato
Hironobu Kobayashi
Tooru Inada
Tadayoshi Murakami
Norio Arashi
Yoji Ishibashi
Michio Kuroda
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Publication of EP0335978A1 publication Critical patent/EP0335978A1/en
Publication of EP0335978A4 publication Critical patent/EP0335978A4/en
Application granted granted Critical
Publication of EP0335978B1 publication Critical patent/EP0335978B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D23/00Assemblies of two or more burners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/26Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid with provision for a retention flame
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

This invention relates to a gas turbine combustor of a premixing combustion system in which a fuel and the air are mixed and burnt, consisting of a cylindrical main nozzle provided on an upstream end wall of a cylindrical combustion chamber, an auxiliary nozzle formed around the main nozzle, a main premixed gas supply means for supplying a premixed gas to the main nozzle, and an auxiliary premixed gas supply means for supplying a premixed gas, the excess air ratio of which is smaller than that of the main premixed gas, to the auxiliary nozzle. Owing to this arrangement, a lean premixed gas having an excess air ratio larger than 1 can be burnt stably under low to high loads of a gas turbine.
EP88907798A 1987-09-04 1988-08-31 Gas turbine combustor Expired - Lifetime EP0335978B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP62220206A JP2528894B2 (en) 1987-09-04 1987-09-04 Gas turbine combustor
JP220206/87 1987-09-04
PCT/JP1988/000870 WO1989002052A1 (en) 1987-09-04 1988-08-31 Gas turbine combustor

Publications (3)

Publication Number Publication Date
EP0335978A1 EP0335978A1 (en) 1989-10-11
EP0335978A4 true EP0335978A4 (en) 1989-12-13
EP0335978B1 EP0335978B1 (en) 1995-11-08

Family

ID=16747549

Family Applications (1)

Application Number Title Priority Date Filing Date
EP88907798A Expired - Lifetime EP0335978B1 (en) 1987-09-04 1988-08-31 Gas turbine combustor

Country Status (5)

Country Link
EP (1) EP0335978B1 (en)
JP (1) JP2528894B2 (en)
CN (1) CN1011064B (en)
DE (1) DE3854666T2 (en)
WO (1) WO1989002052A1 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2518986Y2 (en) * 1989-01-20 1996-12-04 川崎重工業株式会社 Gas turbine combustor
US5097666A (en) * 1989-12-11 1992-03-24 Sundstrand Corporation Combustor fuel injection system
JPH03260518A (en) * 1990-03-08 1991-11-20 Advance Koojienereeshiyon Syst Gijutsu Kenkyu Kumiai Gas turbine catalyst combustion system
JP2564022B2 (en) * 1990-06-07 1996-12-18 川崎重工業株式会社 Gas turbine combustor
JPH05196232A (en) * 1991-08-01 1993-08-06 General Electric Co <Ge> Back fire-resistant fuel staging type premixed combustion apparatus
US5318436A (en) * 1991-11-14 1994-06-07 United Technologies Corporation Low NOx combustion piloted by low NOx pilots
US5361586A (en) * 1993-04-15 1994-11-08 Westinghouse Electric Corporation Gas turbine ultra low NOx combustor
US5359847B1 (en) * 1993-06-01 1996-04-09 Westinghouse Electric Corp Dual fuel ultra-flow nox combustor
US5636510A (en) * 1994-05-25 1997-06-10 Westinghouse Electric Corporation Gas turbine topping combustor
US5491970A (en) * 1994-06-10 1996-02-20 General Electric Co. Method for staging fuel in a turbine between diffusion and premixed operations
US6298667B1 (en) * 2000-06-22 2001-10-09 General Electric Company Modular combustor dome
US6755024B1 (en) * 2001-08-23 2004-06-29 Delavan Inc. Multiplex injector
US6813889B2 (en) * 2001-08-29 2004-11-09 Hitachi, Ltd. Gas turbine combustor and operating method thereof
US6962055B2 (en) 2002-09-27 2005-11-08 United Technologies Corporation Multi-point staging strategy for low emission and stable combustion
EP1531305A1 (en) * 2003-11-12 2005-05-18 United Technologies Corporation Multi-point fuel injector
JP4015656B2 (en) * 2004-11-17 2007-11-28 三菱重工業株式会社 Gas turbine combustor
JP4418442B2 (en) * 2006-03-30 2010-02-17 三菱重工業株式会社 Gas turbine combustor and combustion control method
US7966820B2 (en) * 2007-08-15 2011-06-28 General Electric Company Method and apparatus for combusting fuel within a gas turbine engine
US20090223227A1 (en) * 2008-03-05 2009-09-10 General Electric Company Combustion cap with crown mixing holes
DE102008032265B4 (en) * 2008-07-09 2010-06-10 Deutsches Zentrum für Luft- und Raumfahrt e.V. incinerator
US8327642B2 (en) * 2008-10-21 2012-12-11 General Electric Company Multiple tube premixing device
US20110048022A1 (en) * 2009-08-29 2011-03-03 General Electric Company System and method for combustion dynamics control of gas turbine
US8613197B2 (en) * 2010-08-05 2013-12-24 General Electric Company Turbine combustor with fuel nozzles having inner and outer fuel circuits
US20120055163A1 (en) * 2010-09-08 2012-03-08 Jong Ho Uhm Fuel injection assembly for use in turbine engines and method of assembling same
US8707672B2 (en) * 2010-09-10 2014-04-29 General Electric Company Apparatus and method for cooling a combustor cap
US8991187B2 (en) * 2010-10-11 2015-03-31 General Electric Company Combustor with a lean pre-nozzle fuel injection system
US20130036743A1 (en) * 2011-08-08 2013-02-14 General Electric Company Turbomachine combustor assembly
US8966906B2 (en) * 2011-09-28 2015-03-03 General Electric Company System for supplying pressurized fluid to a cap assembly of a gas turbine combustor
US8966907B2 (en) * 2012-04-16 2015-03-03 General Electric Company Turbine combustor system having aerodynamic feed cap
US20130283802A1 (en) * 2012-04-27 2013-10-31 General Electric Company Combustor
DE102013204307A1 (en) 2013-03-13 2014-09-18 Siemens Aktiengesellschaft Jet burner with cooling channel in the base plate
US10101032B2 (en) * 2015-04-01 2018-10-16 General Electric Company Micromixer system for a turbine system and an associated method thereof
JP6423760B2 (en) * 2015-06-24 2018-11-14 三菱日立パワーシステムズ株式会社 Fuel nozzle structure of gas turbine combustor
JP6074090B1 (en) * 2016-02-02 2017-02-01 大口 元気 Liquid container with pump dispenser
CN106016362B (en) * 2016-05-16 2018-10-09 中国科学院工程热物理研究所 A kind of soft combustion chamber of gas turbine and its control method
CN109424976B (en) * 2017-09-05 2021-07-02 深圳意动航空科技有限公司 Flat aeroderivative gas nozzle
JP2019128125A (en) * 2018-01-26 2019-08-01 川崎重工業株式会社 Burner device
JP7489759B2 (en) * 2018-11-20 2024-05-24 三菱重工業株式会社 Combustor and gas turbine
JP2021055971A (en) * 2019-10-01 2021-04-08 三菱パワー株式会社 Gas turbine combustor
KR102433706B1 (en) * 2021-01-07 2022-08-19 두산에너빌리티 주식회사 Nozzle assembly, Combustor and Gas turbine comprising the same
KR102437976B1 (en) * 2021-01-14 2022-08-30 두산에너빌리티 주식회사 Nozzle assembly, Combustor and Gas turbine comprising the same
FR3135114A1 (en) * 2022-05-02 2023-11-03 Safran METHOD FOR INJECTING HYDROGEN-AIR MIXTURE FOR TURBOMACHINE BURNER

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3048014A (en) * 1955-07-07 1962-08-07 Fritz A F Schmidt Combustion chamber for jets and similar engines
CH407653A (en) * 1962-07-24 1966-02-15 Prvni Brnenska Strojirna Burners for gaseous and liquid fuel, in particular for gas turbines
US3919840A (en) * 1973-04-18 1975-11-18 United Technologies Corp Combustion chamber for dissimilar fluids in swirling flow relationship
US4100733A (en) * 1976-10-04 1978-07-18 United Technologies Corporation Premix combustor
EP0095788A1 (en) * 1982-05-28 1983-12-07 BBC Aktiengesellschaft Brown, Boveri & Cie. Gas turbine combustion chamber and method of operating it
GB2146425A (en) * 1983-09-08 1985-04-17 Hitachi Ltd Method of supplying fuel into gas turbine combustor
EP0169431A1 (en) * 1984-07-10 1986-01-29 Hitachi, Ltd. Gas turbine combustor

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5857656A (en) * 1981-09-30 1983-04-05 Toshiba Corp Switching device of control loop
JPH0630589Y2 (en) * 1989-04-19 1994-08-17 石川島播磨重工業株式会社 Supporting device for suspension frame in traveling carriage

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3048014A (en) * 1955-07-07 1962-08-07 Fritz A F Schmidt Combustion chamber for jets and similar engines
CH407653A (en) * 1962-07-24 1966-02-15 Prvni Brnenska Strojirna Burners for gaseous and liquid fuel, in particular for gas turbines
US3919840A (en) * 1973-04-18 1975-11-18 United Technologies Corp Combustion chamber for dissimilar fluids in swirling flow relationship
US4100733A (en) * 1976-10-04 1978-07-18 United Technologies Corporation Premix combustor
EP0095788A1 (en) * 1982-05-28 1983-12-07 BBC Aktiengesellschaft Brown, Boveri & Cie. Gas turbine combustion chamber and method of operating it
GB2146425A (en) * 1983-09-08 1985-04-17 Hitachi Ltd Method of supplying fuel into gas turbine combustor
EP0169431A1 (en) * 1984-07-10 1986-01-29 Hitachi, Ltd. Gas turbine combustor

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO8902052A1 *

Also Published As

Publication number Publication date
EP0335978A1 (en) 1989-10-11
DE3854666D1 (en) 1995-12-14
EP0335978B1 (en) 1995-11-08
CN1011064B (en) 1991-01-02
DE3854666T2 (en) 1996-04-25
JPS6463721A (en) 1989-03-09
JP2528894B2 (en) 1996-08-28
CN1032230A (en) 1989-04-05
WO1989002052A1 (en) 1989-03-09

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