CA1179156A - Gas turbine combustor - Google Patents

Gas turbine combustor

Info

Publication number
CA1179156A
CA1179156A CA000396692A CA396692A CA1179156A CA 1179156 A CA1179156 A CA 1179156A CA 000396692 A CA000396692 A CA 000396692A CA 396692 A CA396692 A CA 396692A CA 1179156 A CA1179156 A CA 1179156A
Authority
CA
Canada
Prior art keywords
fuel
cavity
divergent
nozzles
cavities
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
CA000396692A
Other languages
English (en)
French (fr)
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
Application granted granted Critical
Publication of CA1179156A publication Critical patent/CA1179156A/en
Expired 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
CA000396692A 1981-02-27 1982-02-22 Gas turbine combustor Expired CA1179156A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US23866881A 1981-02-27 1981-02-27
US238,668 1981-02-27

Publications (1)

Publication Number Publication Date
CA1179156A true CA1179156A (en) 1984-12-11

Family

ID=22898839

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000396692A Expired CA1179156A (en) 1981-02-27 1982-02-22 Gas turbine combustor

Country Status (13)

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

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 (de) * 1996-07-10 2001-05-03 Mtu Aero Engines Gmbh Brenner mit Zerstäuberdüse
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 (de) * 2001-08-17 2002-11-28 Eisenmann Kg Maschbau Thermische Nachverbrennungsvorrichtung
CN103334833B (zh) 2007-11-12 2019-04-05 格塔斯热力学驱动系统有限责任公司 轴向活塞发动机以及用于操作轴向活塞发动机的方法
US8783585B2 (en) * 2009-05-20 2014-07-22 General Electric Company Methods and systems for mixing reactor feed
JP6910036B2 (ja) * 2017-10-31 2021-07-28 国立研究開発法人産業技術総合研究所 燃焼器および燃焼方法

Also Published As

Publication number Publication date
JPS57157935A (en) 1982-09-29
IT8219859A0 (it) 1982-02-25
JPS6126774Y2 (de) 1986-08-11
IT1149777B (it) 1986-12-10
MX155871A (es) 1988-05-16
GB2094464B (en) 1984-08-30
NL8200333A (nl) 1982-09-16
IN155686B (de) 1985-02-23
BR8201026A (pt) 1983-01-04
JPS6016866U (ja) 1985-02-05
CH661974A5 (de) 1987-08-31
GB2094464A (en) 1982-09-15
ZA82831B (en) 1983-03-30
AU7998082A (en) 1982-09-02
AU546612B2 (en) 1985-09-12
BE892290A (fr) 1982-08-25
AR227092A1 (es) 1982-09-15

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Legal Events

Date Code Title Description
MKEC Expiry (correction)
MKEX Expiry