AU546612B2 - Multi-annular gas turbine combustor - Google Patents

Multi-annular gas turbine combustor

Info

Publication number
AU546612B2
AU546612B2 AU79980/82A AU7998082A AU546612B2 AU 546612 B2 AU546612 B2 AU 546612B2 AU 79980/82 A AU79980/82 A AU 79980/82A AU 7998082 A AU7998082 A AU 7998082A AU 546612 B2 AU546612 B2 AU 546612B2
Authority
AU
Australia
Prior art keywords
gas turbine
turbine combustor
annular gas
annular
combustor
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.)
Ceased
Application number
AU79980/82A
Other versions
AU7998082A (en
Inventor
Janos M. Beer
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.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of AU7998082A publication Critical patent/AU7998082A/en
Application granted granted Critical
Publication of AU546612B2 publication Critical patent/AU546612B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • 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 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
    • 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
    • F23C9/006—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber the recirculation taking place in 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
    • 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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • 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
AU79980/82A 1981-02-27 1982-01-29 Multi-annular gas turbine combustor Ceased AU546612B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US23866881A 1981-02-27 1981-02-27
US238668 1988-08-31

Publications (2)

Publication Number Publication Date
AU7998082A AU7998082A (en) 1982-09-02
AU546612B2 true AU546612B2 (en) 1985-09-12

Family

ID=22898839

Family Applications (1)

Application Number Title Priority Date Filing Date
AU79980/82A Ceased AU546612B2 (en) 1981-02-27 1982-01-29 Multi-annular gas turbine combustor

Country Status (13)

Country Link
JP (2) JPS57157935A (en)
AR (1) AR227092A1 (en)
AU (1) AU546612B2 (en)
BE (1) BE892290A (en)
BR (1) BR8201026A (en)
CA (1) CA1179156A (en)
CH (1) CH661974A5 (en)
GB (1) GB2094464B (en)
IN (1) IN155686B (en)
IT (1) IT1149777B (en)
MX (1) MX155871A (en)
NL (1) NL8200333A (en)
ZA (1) ZA82831B (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4702073A (en) * 1986-03-10 1987-10-27 Melconian Jerry O Variable residence time vortex combustor
US5361586A (en) * 1993-04-15 1994-11-08 Westinghouse Electric Corporation Gas turbine ultra low NOx combustor
US5454712A (en) * 1993-09-15 1995-10-03 The Boc Group, Inc. Air-oxy-fuel burner method and apparatus
DE19627760C2 (en) * 1996-07-10 2001-05-03 Mtu Aero Engines Gmbh Burner with atomizer nozzle
US6240731B1 (en) * 1997-12-31 2001-06-05 United Technologies Corporation Low NOx combustor for gas turbine engine
US6354072B1 (en) * 1999-12-10 2002-03-12 General Electric Company Methods and apparatus for decreasing combustor emissions
US7175423B1 (en) * 2000-10-26 2007-02-13 Bloom Engineering Company, Inc. Air staged low-NOx burner
DE10140422C1 (en) * 2001-08-17 2002-11-28 Eisenmann Kg Maschbau Thermal post-combustion device for cleaning waste gases comprises a burner having a second flame tube surrounding the end of a first flame tube with a greater radius to form an annular gap
JP5598763B2 (en) * 2007-11-12 2014-10-01 ゲタス Axial piston engine and method for operating an axial piston engine
US8783585B2 (en) * 2009-05-20 2014-07-22 General Electric Company Methods and systems for mixing reactor feed
JP6910036B2 (en) * 2017-10-31 2021-07-28 国立研究開発法人産業技術総合研究所 Combustor and combustion method

Also Published As

Publication number Publication date
CA1179156A (en) 1984-12-11
IT8219859A0 (en) 1982-02-25
IN155686B (en) 1985-02-23
IT1149777B (en) 1986-12-10
MX155871A (en) 1988-05-16
AU7998082A (en) 1982-09-02
JPS6016866U (en) 1985-02-05
ZA82831B (en) 1983-03-30
BR8201026A (en) 1983-01-04
GB2094464A (en) 1982-09-15
CH661974A5 (en) 1987-08-31
GB2094464B (en) 1984-08-30
AR227092A1 (en) 1982-09-15
JPS6126774Y2 (en) 1986-08-11
NL8200333A (en) 1982-09-16
BE892290A (en) 1982-08-25
JPS57157935A (en) 1982-09-29

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