BE763178A - GAS TURBINE ENGINE WITH ADVANCED AFTER-COMBUSTION DEVICE - Google Patents

GAS TURBINE ENGINE WITH ADVANCED AFTER-COMBUSTION DEVICE

Info

Publication number
BE763178A
BE763178A BE763178A BE763178A BE763178A BE 763178 A BE763178 A BE 763178A BE 763178 A BE763178 A BE 763178A BE 763178 A BE763178 A BE 763178A BE 763178 A BE763178 A BE 763178A
Authority
BE
Belgium
Prior art keywords
advanced
gas turbine
turbine engine
combustion device
combustion
Prior art date
Application number
BE763178A
Other languages
French (fr)
Inventor
J K Arand
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BE763178A publication Critical patent/BE763178A/en

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

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)
  • Control Of Turbines (AREA)
BE763178A 1970-05-25 1971-02-19 GAS TURBINE ENGINE WITH ADVANCED AFTER-COMBUSTION DEVICE BE763178A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US4029870A 1970-05-25 1970-05-25

Publications (1)

Publication Number Publication Date
BE763178A true BE763178A (en) 1971-07-16

Family

ID=21910234

Family Applications (1)

Application Number Title Priority Date Filing Date
BE763178A BE763178A (en) 1970-05-25 1971-02-19 GAS TURBINE ENGINE WITH ADVANCED AFTER-COMBUSTION DEVICE

Country Status (6)

Country Link
US (1) US3646763A (en)
BE (1) BE763178A (en)
CA (1) CA927616A (en)
DE (1) DE2108690A1 (en)
FR (1) FR2090250B1 (en)
GB (1) GB1335746A (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2122308B1 (en) * 1971-01-19 1976-03-05 Snecma Fr
FR2551500B1 (en) * 1983-09-07 1985-11-08 Snecma BURNER RING FOR POSTCOMBUSTION OF A REACTION ENGINE
FR2586792B1 (en) * 1985-09-03 1989-06-16 Snecma CONNECTION DEVICE BETWEEN A BURNER RING OR FLAME HANGER OF COMPOSITE MATERIAL AND A POST-COMBUSTION CHAMBER CHANNEL OF A TURBOREACTOR
US4815283A (en) * 1987-06-25 1989-03-28 The United States Of America As Represented By The Secretary Of The Air Force Afterburner flameholder construction
US5103638A (en) * 1990-01-29 1992-04-14 Rolls-Royce Inc. Mounting arrangement
EP0550126A1 (en) * 1992-01-02 1993-07-07 General Electric Company Thrust augmentor heat shield
US6351941B1 (en) * 2000-02-29 2002-03-05 General Electric Company Methods and apparatus for reducing thermal stresses in an augmentor
US7712315B2 (en) * 2006-04-20 2010-05-11 United Technologies Corporation Augmentor variable vane flame stabilization

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2714287A (en) * 1950-01-03 1955-08-02 Westinghouse Electric Corp Flameholder device for turbojet afterburner
GB821286A (en) * 1956-06-05 1959-10-07 Rolls Royce Improvements in or relating to reheat combustion equipment of jet-propulsion engines
US3102392A (en) * 1959-04-21 1963-09-03 Snecma Combustion equipment for jet propulsion units
US3056261A (en) * 1959-09-01 1962-10-02 Gen Electric Flameholder configuration
FR1245920A (en) * 1960-01-19 1960-11-10 Le Ministre De La Defense Nati Insulated fuel distribution manifold
FR1265727A (en) * 1960-08-23 1961-06-30 Gen Electric Structure of flame tubes for afterburner burners of turbo-reactors
GB944202A (en) * 1961-07-11 1963-12-11 Rolls Royce Improvements in or relating to combustion equipment and ignition devices therefor
FR1406603A (en) * 1964-06-09 1965-07-23 Snecma Burner device and its installation in a combustion chamber

Also Published As

Publication number Publication date
FR2090250A1 (en) 1972-01-14
GB1335746A (en) 1973-10-31
CA927616A (en) 1973-06-05
DE2108690A1 (en) 1972-08-10
US3646763A (en) 1972-03-07
FR2090250B1 (en) 1975-01-17

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