JPH0366570B2 - - Google Patents

Info

Publication number
JPH0366570B2
JPH0366570B2 JP59187223A JP18722384A JPH0366570B2 JP H0366570 B2 JPH0366570 B2 JP H0366570B2 JP 59187223 A JP59187223 A JP 59187223A JP 18722384 A JP18722384 A JP 18722384A JP H0366570 B2 JPH0366570 B2 JP H0366570B2
Authority
JP
Japan
Prior art keywords
ring
upstream
peripheral edge
yokes
annular
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
JP59187223A
Other languages
English (en)
Japanese (ja)
Other versions
JPS60155827A (ja
Inventor
Aran Bunowa Rune
Misheru Kuroozeru Robeeru
Arufuretsudo Juru Bandanburutsuku Roje
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.)
NASHIONARU DECHUUDO E DO KONSUTORYUKUSHION DE MOTOORU DABIASHION SOC
Original Assignee
NASHIONARU DECHUUDO E DO KONSUTORYUKUSHION DE MOTOORU DABIASHION SOC
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 NASHIONARU DECHUUDO E DO KONSUTORYUKUSHION DE MOTOORU DABIASHION SOC filed Critical NASHIONARU DECHUUDO E DO KONSUTORYUKUSHION DE MOTOORU DABIASHION SOC
Publication of JPS60155827A publication Critical patent/JPS60155827A/ja
Publication of JPH0366570B2 publication Critical patent/JPH0366570B2/ja
Granted 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)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Processes For Solid Components From Exhaust (AREA)
  • Combustion Of Fluid Fuel (AREA)
JP59187223A 1983-09-07 1984-09-06 ターボファンエンジンのアフターバーナ Granted JPS60155827A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8314249A FR2551500B1 (fr) 1983-09-07 1983-09-07 Anneau-bruleur pour postcombustion de moteur a reaction
FR8314249 1983-09-07

Publications (2)

Publication Number Publication Date
JPS60155827A JPS60155827A (ja) 1985-08-15
JPH0366570B2 true JPH0366570B2 (en]) 1991-10-17

Family

ID=9292032

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59187223A Granted JPS60155827A (ja) 1983-09-07 1984-09-06 ターボファンエンジンのアフターバーナ

Country Status (6)

Country Link
US (1) US4592200A (en])
EP (1) EP0142389B1 (en])
JP (1) JPS60155827A (en])
DE (1) DE3460874D1 (en])
FR (1) FR2551500B1 (en])
IL (1) IL72744A (en])

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4765136A (en) * 1985-11-25 1988-08-23 United Technologies Corporation Gas turbine engine augmentor
FR2626044A1 (fr) * 1988-01-14 1989-07-21 Snecma Melangeur de flux a section variable avec stabilisateur de rechauffe integre pour turboreacteur double flux
US4901527A (en) * 1988-02-18 1990-02-20 General Electric Company Low turbulence flame holder mount
US5103638A (en) * 1990-01-29 1992-04-14 Rolls-Royce Inc. Mounting arrangement
US5680754A (en) * 1990-02-12 1997-10-28 General Electric Company Compressor splitter for use with a forward variable area bypass injector
US5231825A (en) * 1990-04-09 1993-08-03 General Electric Company Method for compressor air extraction
US5155993A (en) * 1990-04-09 1992-10-20 General Electric Company Apparatus for compressor air extraction
US5127224A (en) * 1991-03-25 1992-07-07 United Technologies Corporation Spray-ring mounting assembly
FR2687734B1 (fr) * 1992-02-26 1994-08-26 Snecma Dispositif accroche-flammes a geometrie variable destine a etre utilise dans le dispositif post-combustion d'une turbomachine.
US5768886A (en) * 1995-09-29 1998-06-23 National Science Council Twin-plate flameholder construction
US6684641B2 (en) * 1999-12-15 2004-02-03 Osaka Gas Co., Ltd. Fluid distributor, burner device, gas turbine engine, and cogeneration system
FR2869953B1 (fr) * 2004-05-05 2008-07-04 Snecma Moteurs Sa Dispositif d'alimentation en air et en carburant d'un anneau-bruleur dans une chambre de postcombustion
JP5625585B2 (ja) * 2010-07-27 2014-11-19 株式会社Ihi アフタバーナ及び航空機エンジン
GB201013723D0 (en) 2010-08-17 2010-09-29 Rolls Royce Plc Manifold mounting arrangement
CN104439634B (zh) * 2014-11-07 2016-03-30 沈阳黎明航空发动机(集团)有限责任公司 一种防止环形v槽稳定器焊接变形的装置及其使用方法
FR3032519B1 (fr) * 2015-02-10 2017-02-24 Herakles Dispositif accroche-flamme
CN113883549B (zh) * 2021-12-08 2022-02-22 中国航发沈阳发动机研究所 一种兼顾雷达隐身的火焰稳定器
US11939922B2 (en) * 2022-08-19 2024-03-26 Pratt & Whitney Canada Corp. Fuel assembly for a gas turbine engine

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2799991A (en) * 1954-03-05 1957-07-23 Earl W Conrad Afterburner flame stabilization means
US2875580A (en) * 1957-04-16 1959-03-03 Westinghouse Electric Corp Flameholding apparatus
US3102392A (en) * 1959-04-21 1963-09-03 Snecma Combustion equipment for jet propulsion units
FR1245920A (fr) * 1960-01-19 1960-11-10 Le Ministre De La Defense Nati Collecteur de distribution de combustible isolé
GB938553A (en) * 1961-05-09 1963-10-02 Rolls Royce Reheat combustion apparatus for a gas turbine engine
FR1525092A (fr) * 1967-01-23 1968-05-17 Snecma Turbo-réacteur à flux de gaz chaud et à flux d'air froid
GB1211583A (en) * 1968-05-16 1970-11-11 Mini Of Technology Improvements in or relating to combustion devices
GB1255648A (en) * 1968-10-22 1971-12-01 Rolls Royce Duct burning system
US3646763A (en) * 1970-05-25 1972-03-07 Gen Electric Gas turbine engine with improved afterburner
US3698186A (en) * 1970-12-24 1972-10-17 United Aircraft Corp Afterburner combustion apparatus
FR2186608B1 (en]) * 1972-04-17 1975-08-29 Snecma
US3765178A (en) * 1972-09-08 1973-10-16 Gen Electric Afterburner flameholder
FR2227436B1 (en]) * 1973-04-27 1975-12-26 Snecma
US3931707A (en) * 1975-01-08 1976-01-13 General Electric Company Augmentor flameholding apparatus
FR2351258A1 (fr) * 1976-05-13 1977-12-09 Snecma Dispositif d'allumage de carburant injecte dans un milieu gazeux en ecoulement rapide
FR2404111A1 (fr) * 1977-09-27 1979-04-20 Snecma Dispositif de distribution de carburant

Also Published As

Publication number Publication date
FR2551500A1 (fr) 1985-03-08
US4592200A (en) 1986-06-03
IL72744A (en) 1992-03-29
EP0142389B1 (fr) 1986-10-01
DE3460874D1 (en) 1986-11-06
JPS60155827A (ja) 1985-08-15
IL72744A0 (en) 1984-11-30
EP0142389A1 (fr) 1985-05-22
FR2551500B1 (fr) 1985-11-08

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