CA927616A - Gas turbine engine with improved afterburner - Google Patents

Gas turbine engine with improved afterburner

Info

Publication number
CA927616A
CA927616A CA107807A CA107807A CA927616A CA 927616 A CA927616 A CA 927616A CA 107807 A CA107807 A CA 107807A CA 107807 A CA107807 A CA 107807A CA 927616 A CA927616 A CA 927616A
Authority
CA
Canada
Prior art keywords
gas turbine
turbine engine
afterburner
improved
improved afterburner
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
CA107807A
Other languages
English (en)
Other versions
CA107807S (en
Inventor
K. Arand John
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of CA927616A publication Critical patent/CA927616A/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
    • F23R3/02—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)
CA107807A 1970-05-25 1971-03-16 Gas turbine engine with improved afterburner Expired CA927616A (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
CA927616A true CA927616A (en) 1973-06-05

Family

ID=21910234

Family Applications (1)

Application Number Title Priority Date Filing Date
CA107807A Expired CA927616A (en) 1970-05-25 1971-03-16 Gas turbine engine with improved afterburner

Country Status (6)

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

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2122308B1 (enrdf_load_stackoverflow) * 1971-01-19 1976-03-05 Snecma Fr
FR2551500B1 (fr) * 1983-09-07 1985-11-08 Snecma Anneau-bruleur pour postcombustion de moteur a reaction
FR2586792B1 (fr) * 1985-09-03 1989-06-16 Snecma Dispositif de liaison entre un anneau bruleur ou accroche-flammes en materiau composite et un canal de chambre de post-combustion d'un turboreacteur
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 (fr) * 1960-01-19 1960-11-10 Le Ministre De La Defense Nati Collecteur de distribution de combustible isolé
FR1265727A (fr) * 1960-08-23 1961-06-30 Gen Electric Structure de tubes à flammes pour brûleurs de post-combustion de turbo-réacteurs
GB944202A (en) * 1961-07-11 1963-12-11 Rolls Royce Improvements in or relating to combustion equipment and ignition devices therefor
FR1406603A (fr) * 1964-06-09 1965-07-23 Snecma Dispositif de brûleur et son montage dans une chambre de combustion

Also Published As

Publication number Publication date
US3646763A (en) 1972-03-07
BE763178A (fr) 1971-07-16
FR2090250A1 (enrdf_load_stackoverflow) 1972-01-14
FR2090250B1 (enrdf_load_stackoverflow) 1975-01-17
DE2108690A1 (de) 1972-08-10
GB1335746A (en) 1973-10-31

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