IT993117B - FLAME HOLDER FOR TURBOREACTOR AFTER BURNER - Google Patents

FLAME HOLDER FOR TURBOREACTOR AFTER BURNER

Info

Publication number
IT993117B
IT993117B IT28455/73A IT2845573A IT993117B IT 993117 B IT993117 B IT 993117B IT 28455/73 A IT28455/73 A IT 28455/73A IT 2845573 A IT2845573 A IT 2845573A IT 993117 B IT993117 B IT 993117B
Authority
IT
Italy
Prior art keywords
turboreactor
burner
flame holder
flame
holder
Prior art date
Application number
IT28455/73A
Other languages
Italian (it)
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
Application granted granted Critical
Publication of IT993117B publication Critical patent/IT993117B/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)
  • Exhaust Gas After Treatment (AREA)
IT28455/73A 1972-09-08 1973-08-31 FLAME HOLDER FOR TURBOREACTOR AFTER BURNER IT993117B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US28728172A 1972-09-08 1972-09-08

Publications (1)

Publication Number Publication Date
IT993117B true IT993117B (en) 1975-09-30

Family

ID=23102221

Family Applications (1)

Application Number Title Priority Date Filing Date
IT28455/73A IT993117B (en) 1972-09-08 1973-08-31 FLAME HOLDER FOR TURBOREACTOR AFTER BURNER

Country Status (8)

Country Link
US (1) US3765178A (en)
JP (1) JPS4992423A (en)
BE (1) BE804377A (en)
CA (1) CA958551A (en)
DE (1) DE2344630A1 (en)
FR (1) FR2199062A1 (en)
GB (1) GB1426784A (en)
IT (1) IT993117B (en)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3931707A (en) * 1975-01-08 1976-01-13 General Electric Company Augmentor flameholding apparatus
US4064691A (en) * 1975-11-04 1977-12-27 General Electric Company Cooling of fastener means for a removable flameholder
FR2351258A1 (en) * 1976-05-13 1977-12-09 Snecma FUEL IGNITION DEVICE INJECTED INTO A FAST FLOWING GASEOUS MEDIUM
US4203285A (en) * 1978-02-06 1980-05-20 The United States Of America As Represented By The Secretary Of The Air Force Partial swirl augmentor for a turbofan engine
US4490973A (en) * 1983-04-12 1985-01-01 The United States Of America As Represented By The Secretary Of The Air Force Flameholder with integrated air mixer
FR2551500B1 (en) * 1983-09-07 1985-11-08 Snecma BURNER RING FOR POSTCOMBUSTION OF A REACTION ENGINE
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
US5076062A (en) * 1987-11-05 1991-12-31 General Electric Company Gas-cooled flameholder assembly
US4893468A (en) * 1987-11-30 1990-01-16 General Electric Company Emissions control for gas turbine engine
FR2626044A1 (en) * 1988-01-14 1989-07-21 Snecma VARIABLE SECTION FLUX MIXER WITH INTEGRATED HEATING STABILIZER FOR DOUBLE FLOW TURBOJETACTOR
US4901527A (en) * 1988-02-18 1990-02-20 General Electric Company Low turbulence flame holder mount
US4887425A (en) * 1988-03-18 1989-12-19 General Electric Company Fuel spraybar
US5157917A (en) * 1991-05-20 1992-10-27 United Technologies Corporation Gas turbine engine cooling air flow
US5491974A (en) * 1993-04-15 1996-02-20 General Electric Company Removable afterburner flameholder
US5768886A (en) * 1995-09-29 1998-06-23 National Science Council Twin-plate flameholder construction
US6125813A (en) * 1997-06-09 2000-10-03 Patrick Power Products, Inc. Prechamber combustion for a rotary diesel engine
FR2873168B1 (en) * 2004-07-16 2008-10-31 Snecma Moteurs Sa TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER
US7565804B1 (en) * 2006-06-29 2009-07-28 General Electric Company Flameholder fuel shield
US7581398B2 (en) * 2006-06-29 2009-09-01 General Electric Company Purged flameholder fuel shield
US7568346B2 (en) * 2006-10-31 2009-08-04 General Electric Company Method and apparatus for assembling a flameholder for an augmenter
US9267687B2 (en) 2011-11-04 2016-02-23 General Electric Company Combustion system having a venturi for reducing wakes in an airflow
US9879862B2 (en) * 2013-03-08 2018-01-30 Rolls-Royce North American Technologies, Inc. Gas turbine engine afterburner
JP6229590B2 (en) * 2014-04-30 2017-11-15 株式会社Ihi Afterburner and aircraft engine
JP6245057B2 (en) * 2014-04-30 2017-12-13 株式会社Ihi Afterburner and aircraft engine
US10563868B2 (en) * 2017-05-08 2020-02-18 General Electric Company Coupling method and structure for a propulsion system hot section
CN115164234B (en) * 2022-05-12 2023-06-13 中国航发四川燃气涡轮研究院 Afterburner flame stabilizer
FR3136016B1 (en) * 2022-05-30 2024-05-03 Safran Aircraft Engines FLAME HOLDER RING FOR TURBORE ENGINE AFTERCOMBUSTION COMPRISING A DUCT FOR HEATING AN ANGULAR SEGMENT OF THE RING

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3054259A (en) * 1962-09-18 Combustion apparatus
US2296023A (en) * 1941-03-03 1942-09-15 Northrop Aircraft Inc Burner
GB684670A (en) * 1947-10-21 1952-12-24 Power Jets Res & Dev Ltd Improvements in or relating to combustion apparatus
US3156094A (en) * 1962-11-21 1964-11-10 Gen Electric Catalytic ignition means for a jet engine thrust augmentation system
GB1049977A (en) * 1964-11-19 1966-11-30 Rolls Royce Prime mover ignition device

Also Published As

Publication number Publication date
CA958551A (en) 1974-12-03
DE2344630A1 (en) 1974-03-14
US3765178A (en) 1973-10-16
GB1426784A (en) 1976-03-03
FR2199062A1 (en) 1974-04-05
BE804377A (en) 1974-01-02
JPS4992423A (en) 1974-09-03

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