FR2392232A1 - Chambre de combustion notamment chambre de combustion annulaire pour turboreacteur - Google Patents

Chambre de combustion notamment chambre de combustion annulaire pour turboreacteur

Info

Publication number
FR2392232A1
FR2392232A1 FR7815615A FR7815615A FR2392232A1 FR 2392232 A1 FR2392232 A1 FR 2392232A1 FR 7815615 A FR7815615 A FR 7815615A FR 7815615 A FR7815615 A FR 7815615A FR 2392232 A1 FR2392232 A1 FR 2392232A1
Authority
FR
France
Prior art keywords
combustion chamber
turboreactor
compressor
annular
especially 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.)
Granted
Application number
FR7815615A
Other languages
English (en)
Other versions
FR2392232B3 (fr
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.)
MTU Aero Engines GmbH
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2392232A1 publication Critical patent/FR2392232A1/fr
Application granted granted Critical
Publication of FR2392232B3 publication Critical patent/FR2392232B3/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • 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
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

a. Chambre de combustion notamment chambre de combustion annulaire pour turboréacteur. b. Chambre de combustion caractérisée en ce qu'au niveau de la zone primaire, elle est susceptible d'être refroidie par de l'air pris directement à la sortie du compresseur, et la tête du tube de flamme est essentiellement réalisée à deux parois et le volume annulaire entouré par les deux segments de parois est relié par des organes de guidage d'air traversant radialement le canal annulaire et qui sont reliés à la conduite d'extraction d'air à l'extrémité du compresseur.
FR7815615A 1977-05-25 1978-05-25 Chambre de combustion notamment chambre de combustion annulaire pour turboreacteur Granted FR2392232A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19772723546 DE2723546A1 (de) 1977-05-25 1977-05-25 Brennkammer, insbesondere ringumkehrbrennkammer fuer gasturbinentriebwerke

Publications (2)

Publication Number Publication Date
FR2392232A1 true FR2392232A1 (fr) 1978-12-22
FR2392232B3 FR2392232B3 (fr) 1981-01-23

Family

ID=6009800

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7815615A Granted FR2392232A1 (fr) 1977-05-25 1978-05-25 Chambre de combustion notamment chambre de combustion annulaire pour turboreacteur

Country Status (4)

Country Link
US (1) US4203283A (fr)
DE (1) DE2723546A1 (fr)
FR (1) FR2392232A1 (fr)
GB (1) GB1596912A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014053728A1 (fr) 2012-10-01 2014-04-10 Turbomeca Chambre de combustion comprenant un tube à flamme fixé au moyen de trois éléments de centrage

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1159293B (it) * 1982-04-23 1987-02-25 Giavelli Mec Spa Bruciatore con preriscaldamento dell'aria di combustione, particolarmente per forni ceramici di cottura
GB2124747A (en) * 1982-07-23 1984-02-22 Heung Duk Dan A gas turbine combustion system
GB2204672B (en) * 1987-05-06 1991-03-06 Rolls Royce Plc Combustor
GB2209592A (en) * 1987-08-17 1989-05-17 Admiral Design & Res Ltd Radiant heater
US5111655A (en) * 1989-12-22 1992-05-12 Sundstrand Corporation Single wall combustor assembly
FR2670869B1 (fr) * 1990-12-19 1994-10-21 Snecma Chambre de combustion comportant deux enceintes successives.
US5628193A (en) * 1994-09-16 1997-05-13 Alliedsignal Inc. Combustor-to-turbine transition assembly
US6405703B1 (en) 2001-06-29 2002-06-18 Brian Sowards Internal combustion engine
US7200987B2 (en) * 2004-06-18 2007-04-10 General Electric Company Off-axis pulse detonation configuration for gas turbine engine
US7350358B2 (en) * 2004-11-16 2008-04-01 Pratt & Whitney Canada Corp. Exit duct of annular reverse flow combustor and method of making the same
US20070245710A1 (en) * 2006-04-21 2007-10-25 Honeywell International, Inc. Optimized configuration of a reverse flow combustion system for a gas turbine engine
US9631815B2 (en) * 2012-12-28 2017-04-25 General Electric Company System and method for a turbine combustor
FR3001497B1 (fr) * 2013-01-29 2016-05-13 Turbomeca Ensemble de combustion de turbomachine comprenant un circuit d alimentation de carburant ameliore
US11112119B2 (en) * 2018-10-25 2021-09-07 General Electric Company Combustor assembly for a turbo machine
CN113137639B (zh) * 2021-04-25 2022-07-15 中国航发湖南动力机械研究所 涡桨发动机回流燃烧室及涡桨发动机

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2638745A (en) * 1943-04-01 1953-05-19 Power Jets Res & Dev Ltd Gas turbine combustor having tangential air inlets for primary and secondary air
US2852914A (en) * 1955-12-30 1958-09-23 United Aircraft Corp Combustion chamber support means
DE1426325B2 (de) * 1964-12-12 1970-09-17 Daimler-Benz AG, 7OOO Stuttgart Gasturbinentriebwerk
US3705492A (en) * 1971-01-11 1972-12-12 Gen Motors Corp Regenerative gas turbine system
GB1424197A (en) * 1972-06-09 1976-02-11 Lucas Industries Ltd Combustion chambers for gas turbine engines
US3844116A (en) * 1972-09-06 1974-10-29 Avco Corp Duct wall and reverse flow combustor incorporating same
DE2416909A1 (de) * 1974-04-06 1975-10-16 Daimler Benz Ag Betriebsverfahren fuer eine gasturbinenanlage zur abgasverbesserung und entsprechende gasturbinenanlage
GB1490145A (en) * 1974-09-11 1977-10-26 Mtu Muenchen Gmbh Gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014053728A1 (fr) 2012-10-01 2014-04-10 Turbomeca Chambre de combustion comprenant un tube à flamme fixé au moyen de trois éléments de centrage

Also Published As

Publication number Publication date
FR2392232B3 (fr) 1981-01-23
DE2723546A1 (de) 1978-11-30
US4203283A (en) 1980-05-20
GB1596912A (en) 1981-09-03

Similar Documents

Publication Publication Date Title
FR2392232A1 (fr) Chambre de combustion notamment chambre de combustion annulaire pour turboreacteur
FR2383319A1 (fr) Injecteur pour turbine a gaz
FR2393940A1 (fr) Bruleur de chambre de combustion pour moteur a turbine a gaz
RU2003101666A (ru) Диффузор наземного или авиационного газотурбинного двигателя
FR2376994A1 (fr) Perfectionnements aux dispositifs a cavites resonnantes pour la reduction du bruit dans un conduit en presence d'un flux gazeux
KR940002550A (ko) 이차 버너
GB683555A (en) Improvements in or relating to combustion chamber
FR2398966A1 (fr) Bruleur a gaz
FR2400617A1 (fr) Moteur a combustion interne avec coffrage insonorisant
SE7713044L (sv) Oljebrennare
FR2368620A1 (fr) Dispositif pour le remplissage d'un systeme creux avec une seule ouverture de remplissage, notamment une enceinte de refroidissement de moteur
FR2363006A1 (fr) Thermocompresseur a piston libre
FR2358825A1 (fr) Dispositif de formation de gouttes pour installation d'arrosage par egouttement
GB1060095A (en) Improvements relating to the flow of a cooling fluid
FR2232966A5 (en) Combustion air cooled gas burner - coaxial casing, inner wall and partition ensure smooth flow
SU890030A1 (ru) Камера пульсирующего горени с резонансной трубой
FR2370246A1 (fr) Machine frigorifique sous carter
FR1071851A (fr) Perfectionnements apportés aux dispositifs pour le réglage de la section de sortie d'un conduit traversé par un fluide, notamment d'une tuyère de moteur à réaction
SU1661537A1 (ru) Устройство стабилизированной подачи
SU883601A2 (ru) Горелка
SU1426504A1 (ru) Оросительный трубопровод
GB1210113A (en) Gas turbine engine
SU71371A1 (ru) Газова горелка дл плит, таганов и тому подобного
SU77887A1 (ru) Вихревой эжекционный вакуум-насос
FR2381917A1 (fr) Piston en metal leger pour moteurs diesel a chambre de turbulence

Legal Events

Date Code Title Description
ST Notification of lapse