UA76298C2 - Afterburner ring for two-contour turbo-jet engine, afterburner unit and turbo-jet engine - Google Patents

Afterburner ring for two-contour turbo-jet engine, afterburner unit and turbo-jet engine Download PDF

Info

Publication number
UA76298C2
UA76298C2 UA20040806541A UA20040806541A UA76298C2 UA 76298 C2 UA76298 C2 UA 76298C2 UA 20040806541 A UA20040806541 A UA 20040806541A UA 20040806541 A UA20040806541 A UA 20040806541A UA 76298 C2 UA76298 C2 UA 76298C2
Authority
UA
Ukraine
Prior art keywords
ring
sector
casing
annular
afterburner
Prior art date
Application number
UA20040806541A
Other languages
English (en)
Ukrainian (uk)
Inventor
Jacques Marcel Arthur Bunel
Jacques Andre Michel Roche
Stephane Henri Guy Touchaud
Original Assignee
Snecma Moteurs
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 Snecma Moteurs filed Critical Snecma Moteurs
Publication of UA76298C2 publication Critical patent/UA76298C2/uk

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Processes For Solid Components From Exhaust (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Supercharger (AREA)
  • Incineration Of Waste (AREA)
  • Combustion Of Fluid Fuel (AREA)
UA20040806541A 2003-08-05 2004-08-04 Afterburner ring for two-contour turbo-jet engine, afterburner unit and turbo-jet engine UA76298C2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0309657A FR2858661B1 (fr) 2003-08-05 2003-08-05 Dispositif de post-combustion

Publications (1)

Publication Number Publication Date
UA76298C2 true UA76298C2 (en) 2006-07-17

Family

ID=33548306

Family Applications (1)

Application Number Title Priority Date Filing Date
UA20040806541A UA76298C2 (en) 2003-08-05 2004-08-04 Afterburner ring for two-contour turbo-jet engine, afterburner unit and turbo-jet engine

Country Status (11)

Country Link
US (1) US7287383B2 (de)
EP (1) EP1505347B1 (de)
JP (1) JP4056996B2 (de)
KR (1) KR20050016140A (de)
CN (1) CN100368731C (de)
CA (1) CA2475430A1 (de)
DE (1) DE602004000485T2 (de)
ES (1) ES2256829T3 (de)
FR (1) FR2858661B1 (de)
RU (1) RU2291315C2 (de)
UA (1) UA76298C2 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1989486A1 (de) * 2006-02-28 2008-11-12 Siemens Aktiengesellschaft Gasturbinenbrenner und verfahren zum betreiben eines gasturbinenbrenners
FR2900460B1 (fr) * 2006-04-28 2012-10-05 Snecma Systeme annulaire de post-combustion d'une turbomachine
EP2153051A4 (de) * 2007-05-22 2013-06-19 Volvo Aero Corp Abdeckanordnung für einen turbomotor
FR2921042B1 (fr) * 2007-09-14 2010-05-14 Airbus Dispositif de generation de fumee pour aeronef et aeronef equipe d'un tel dispositif
FR2935464B1 (fr) * 2008-09-01 2018-10-26 Safran Aircraft Engines Dispositif de fixation d'un bras accroche flammes sur un carter de post-combustion.
CN101776283B (zh) * 2009-01-13 2012-06-20 北京航空航天大学 带射流注入的火焰稳定装置
US10267406B2 (en) * 2013-07-07 2019-04-23 United Technologies Corporation Inseparable machined lubricant manifold
FR3082284B1 (fr) * 2018-06-07 2020-12-11 Safran Aircraft Engines Chambre de combustion pour une turbomachine
GB201819748D0 (en) 2018-10-12 2019-01-16 Rolls Royce Plc Afterburner system
CN109611887B (zh) * 2018-11-01 2020-10-09 中国航发沈阳发动机研究所 一种燃烧装置
GB202006964D0 (en) * 2020-05-12 2020-06-24 Rolls Royce Plc Afterburner strut with integrated fueld feed lines
FR3121973A1 (fr) * 2021-04-19 2022-10-21 Safran Aircraft Engines Cône de diffusion pour partie arrière de turboréacteur intégrant un anneau accroche-flamme en bord de fuite
FR3121974B1 (fr) * 2021-04-19 2024-01-19 Safran Aircraft Engines Dispositif accroche-flammes pour postcombustion de turboréacteur comprenant des bras à trois branches
GB2615335B (en) * 2022-02-04 2024-05-08 Rolls Royce Plc A reheat assembly

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2862359A (en) * 1952-10-28 1958-12-02 Gen Motors Corp Fuel manifold and flameholder in combustion apparatus for jet engines
FR1321385A (fr) * 1962-05-09 1963-03-15 Rolls Royce Réchauffeur à combustion pour turbine à gaz ou analogue
US3269116A (en) * 1965-04-29 1966-08-30 United Aircraft Corp Centrally supported flameholder
US3747345A (en) * 1972-07-24 1973-07-24 United Aircraft Corp Shortened afterburner construction for turbine engine
FR2696502B1 (fr) * 1992-10-07 1994-11-04 Snecma Dispositif de post-combustion pour turbo réacteur double flux.
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
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
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
US5127224A (en) * 1991-03-25 1992-07-07 United Technologies Corporation Spray-ring mounting assembly
US5179832A (en) * 1991-07-26 1993-01-19 United Technologies Corporation Augmenter flame holder construction
FR2709342B1 (fr) * 1993-08-25 1995-09-22 Snecma Dispositif de post combustion d'un turboréacteur.
RU2117806C1 (ru) * 1995-02-15 1998-08-20 Открытое акционерное общество "А.Люлька-Сатурн" Форсажная камера газотурбинного двигателя
FR2770284B1 (fr) * 1997-10-23 1999-11-19 Snecma Accroche-flamme carbure et a refroidissement optimise

Also Published As

Publication number Publication date
US7287383B2 (en) 2007-10-30
JP4056996B2 (ja) 2008-03-05
CN1580641A (zh) 2005-02-16
ES2256829T3 (es) 2006-07-16
DE602004000485T2 (de) 2007-01-04
JP2005054792A (ja) 2005-03-03
EP1505347B1 (de) 2006-03-15
EP1505347A1 (de) 2005-02-09
CA2475430A1 (fr) 2005-02-05
FR2858661A1 (fr) 2005-02-11
CN100368731C (zh) 2008-02-13
RU2004123918A (ru) 2006-01-27
KR20050016140A (ko) 2005-02-21
US20050086941A1 (en) 2005-04-28
DE602004000485D1 (de) 2006-05-11
RU2291315C2 (ru) 2007-01-10
FR2858661B1 (fr) 2005-10-07

Similar Documents

Publication Publication Date Title
JP4731039B2 (ja) ドーム・ライナ継手を具えるガスタービン燃焼器
CN102678335B (zh) 紊流化后端衬套组件
US9322556B2 (en) Flow sleeve assembly for a combustion module of a gas turbine combustor
US8082739B2 (en) Combustor exit temperature profile control via fuel staging and related method
CN102954493B (zh) 燃料喷嘴以及燃烧器
CN107191970B (zh) 燃气涡轮流套管安装
RU2373416C2 (ru) Турбореактивный двигатель со средствами защиты устройства инжекции топлива и устройство инжекции топлива для турбореактивного двигателя
UA76298C2 (en) Afterburner ring for two-contour turbo-jet engine, afterburner unit and turbo-jet engine
EP2690364A2 (de) Verbrennerhaube und Wärmeabschirmanordnung
CN108006696B (zh) 燃烧器组件和燃烧器
US20140174090A1 (en) System for supplying fuel to a combustor
CN107975820A (zh) 燃烧器空气罩组件及燃烧器组件
US20170268783A1 (en) Axially staged fuel injector assembly mounting
RU2358139C2 (ru) Устройство для подачи воздуха и топлива к кольцу форсунок в форсажной камере
HUP0401114A2 (en) Low nox combustion liner with cooling air plenum recesses
RU2382895C2 (ru) Турбореактивный двигатель с защитным экраном топливного коллектора кольца форсунок, кольцо форсунок и защитный экран
US7617689B2 (en) Combustor dome assembly including retaining ring
US10669860B2 (en) Gas turbine blade
RU2755240C2 (ru) Горелка для камеры сгорания газотурбинной энергосиловой установки, камера сгорания газотурбинной энергосиловой установки, содержащая такую горелку, и газотурбинная энергосиловая установка, содержащая такую камеру сгорания
JP7139162B2 (ja) 気体燃料および液体燃料の機能を有する二重燃料燃料ノズル
JP7051298B2 (ja) 燃焼ライナ冷却
US20250060104A1 (en) Combustor panel and gas turbine combustor including same