CA1209813A - Turbine combustor having more uniform mixing of fuel and air for improved downstream combustion - Google Patents

Turbine combustor having more uniform mixing of fuel and air for improved downstream combustion

Info

Publication number
CA1209813A
CA1209813A CA000434626A CA434626A CA1209813A CA 1209813 A CA1209813 A CA 1209813A CA 000434626 A CA000434626 A CA 000434626A CA 434626 A CA434626 A CA 434626A CA 1209813 A CA1209813 A CA 1209813A
Authority
CA
Canada
Prior art keywords
fuel
air
combustor
sidewall
mixing
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
CA000434626A
Other languages
English (en)
French (fr)
Inventor
Joel L. Toof
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 CA1209813A publication Critical patent/CA1209813A/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
    • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
CA000434626A 1982-08-19 1983-08-15 Turbine combustor having more uniform mixing of fuel and air for improved downstream combustion Expired CA1209813A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US40968282A 1982-08-19 1982-08-19
US409,682 1982-08-19

Publications (1)

Publication Number Publication Date
CA1209813A true CA1209813A (en) 1986-08-19

Family

ID=23621546

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000434626A Expired CA1209813A (en) 1982-08-19 1983-08-15 Turbine combustor having more uniform mixing of fuel and air for improved downstream combustion

Country Status (7)

Country Link
EP (1) EP0103159B1 (ja)
JP (1) JPS5944524A (ja)
AR (1) AR229741A1 (ja)
CA (1) CA1209813A (ja)
DE (1) DE3368974D1 (ja)
IE (1) IE54394B1 (ja)
MX (1) MX156751A (ja)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6223537B1 (en) * 1997-11-24 2001-05-01 Alliedsignal Power Systems Catalytic combustor for gas turbines
US6908232B2 (en) 2003-03-21 2005-06-21 Agilent Technologies, Inc. Fiber optic connectors and methods of making the same
CN105121962B (zh) * 2013-04-25 2018-06-22 安萨尔多能源瑞士股份公司 具有稀释气体的连续燃烧
CN115445130A (zh) * 2022-08-23 2022-12-09 国网安徽省电力有限公司电力科学研究院 一种消防炮用的管流机构

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2579614A (en) * 1944-06-23 1951-12-25 Allis Chalmers Mfg Co Combustion chamber with rotating fuel and air stream surrounding a flame core
FR2221621B1 (ja) * 1973-03-13 1976-09-10 Snecma
US3937008A (en) * 1974-12-18 1976-02-10 United Technologies Corporation Low emission combustion chamber
US4118171A (en) * 1976-12-22 1978-10-03 Engelhard Minerals & Chemicals Corporation Method for effecting sustained combustion of carbonaceous fuel

Also Published As

Publication number Publication date
JPS622216B2 (ja) 1987-01-19
IE54394B1 (en) 1989-09-13
IE831719L (en) 1984-02-19
MX156751A (es) 1988-09-29
AR229741A1 (es) 1983-10-31
EP0103159A1 (en) 1984-03-21
EP0103159B1 (en) 1987-01-07
JPS5944524A (ja) 1984-03-13
DE3368974D1 (en) 1987-02-12

Similar Documents

Publication Publication Date Title
US5622054A (en) Low NOx lobed mixer fuel injector
US8726668B2 (en) Fuel atomization dual orifice fuel nozzle
US8387391B2 (en) Aerodynamically enhanced fuel nozzle
US6834505B2 (en) Hybrid swirler
US4653278A (en) Gas turbine engine carburetor
US5930999A (en) Fuel injector and multi-swirler carburetor assembly
US6675587B2 (en) Counter swirl annular combustor
EP3137814B1 (en) Combustor burner arrangement
US20120151928A1 (en) Cooling flowpath dirt deflector in fuel nozzle
JPH07217451A (ja) 燃料噴射装置
US6571559B1 (en) Anti-carboning fuel-air mixer for a gas turbine engine combustor
US20040079086A1 (en) Piloted airblast lean direct fuel injector with modified air splitter
US10731862B2 (en) Systems and methods for a multi-fuel premixing nozzle with integral liquid injectors/evaporators
US3722216A (en) Annular slot combustor
US4237694A (en) Combustion equipment for gas turbine engines
US3834159A (en) Combustion apparatus
US10914237B2 (en) Airblast injector for a gas turbine engine
CN109539314A (zh) 一种具有波浪式叶片的新型径向旋流器
US9677766B2 (en) Fuel nozzle for use in a turbine engine and method of assembly
CA1209813A (en) Turbine combustor having more uniform mixing of fuel and air for improved downstream combustion
CA1209810A (en) Turbine combustor having improved secondary nozzle structure for more uniform mixing of fuel and air and improved downstream combustion
US9581334B2 (en) Annular combustion chamber in a turbine engine
EP4008959B1 (en) Apparatus for a turbine engine including a fuel splash plate

Legal Events

Date Code Title Description
MKEX Expiry