DE3165211D1 - Fuel injection device for a gas turbine - Google Patents

Fuel injection device for a gas turbine

Info

Publication number
DE3165211D1
DE3165211D1 DE8181400797T DE3165211T DE3165211D1 DE 3165211 D1 DE3165211 D1 DE 3165211D1 DE 8181400797 T DE8181400797 T DE 8181400797T DE 3165211 T DE3165211 T DE 3165211T DE 3165211 D1 DE3165211 D1 DE 3165211D1
Authority
DE
Germany
Prior art keywords
fuel injection
gas turbine
injection device
turbine
fuel
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
DE8181400797T
Other languages
German (de)
Inventor
Bruno Deroide
Philippe Marc Denis Gastebois
Alain Jacques Gerard Jacquet
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE3165211D1 publication Critical patent/DE3165211D1/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36—Details, e.g. burner cooling means, noise reduction means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/12—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour characterised by the shape or arrangement of the outlets from the nozzle
DE8181400797T 1980-06-06 1981-05-21 Fuel injection device for a gas turbine Expired DE3165211D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8012558A FR2484020A1 (en) 1980-06-06 1980-06-06 FUEL INJECTION ASSEMBLY FOR TURBOREACTOR CHAMBER

Publications (1)

Publication Number Publication Date
DE3165211D1 true DE3165211D1 (en) 1984-09-06

Family

ID=9242761

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8181400797T Expired DE3165211D1 (en) 1980-06-06 1981-05-21 Fuel injection device for a gas turbine

Country Status (3)

Country Link
EP (1) EP0041878B1 (en)
DE (1) DE3165211D1 (en)
FR (1) FR2484020A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2839777B2 (en) * 1991-12-24 1998-12-16 株式会社東芝 Fuel injection nozzle for gas turbine combustor
US8973368B2 (en) * 2011-01-26 2015-03-10 United Technologies Corporation Mixer assembly for a gas turbine engine
US9920932B2 (en) 2011-01-26 2018-03-20 United Technologies Corporation Mixer assembly for a gas turbine engine
CN104776430B (en) * 2015-04-15 2017-05-03 陈民 High-energy-saving environment-friendly liquid combustor

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1698258A (en) * 1926-07-16 1929-01-08 Adolf F Haffenreffer Method of combustion
FR1094871A (en) * 1959-01-22 1955-05-25 Thomson Houston Comp Francaise Improvements to injected fuel combustion devices
US3339613A (en) * 1965-01-04 1967-09-05 Carrier Corp Flame stabilization
US3667221A (en) * 1969-04-17 1972-06-06 Gen Electric Fuel delivery apparatus
US3648457A (en) * 1970-04-30 1972-03-14 Gen Electric Combustion apparatus
FR2330871A2 (en) * 1972-11-13 1977-06-03 Snecma Fuel injector for aircraft gas turbine - has swirl vanes to increase fuel flow at low engine speed and to reduce pollution
DE2605134C2 (en) * 1975-02-12 1984-10-04 Fascione, Pietro, Busto Arsizio, Varese Device for feeding a mixture of air and recirculated flue gas to a burner

Also Published As

Publication number Publication date
FR2484020A1 (en) 1981-12-11
EP0041878B1 (en) 1984-08-01
FR2484020B1 (en) 1985-05-17
EP0041878A3 (en) 1982-09-22
EP0041878A2 (en) 1981-12-16

Similar Documents

Publication Publication Date Title
GB2073401B (en) Fuel nozzle guide heatshield for a gas turbine engine
GB2073398B (en) Fuel nozzle guide and seal for a gas turbine engine
JPS57186026A (en) Gas turbine fuel device
GB2078859B (en) Control means for a gas turbine engine
JPS5575535A (en) Fuel injection apparatus for gas turbine engine
DE3265642D1 (en) Fuel nozzle assembly for a gas turbine engine
DE3264214D1 (en) Apparatus for converting a fuel into combustible gas
IL63170A0 (en) Dual fuel stem for a gas turbine engine
JPS5625607A (en) Duplex fufl injection device for gas turbine engine
JPS57122130A (en) Fuel feeder for gas turbine engine
JPS5374614A (en) Fuel nozzle for gas turbine
GB2088961B (en) Fuel control system for a gas turbine engine
GB2114661B (en) Casing structure for a gas turbine engine
GB2102936B (en) Fuel injector for gas turbine engines
GB2161914B (en) Combustion equipment for a gas turbine engine
GB2004050B (en) Fuel nozzle assembly for a gas turbine engine
GB2120325B (en) Prediffuser for a gas turbine engine
DE3372519D1 (en) Fuel control system for a gas turbine engine
GB2105027B (en) Starting means for a gas turbine engine
GB2089433B (en) Fuel driven hydraulic alternator for a gas turbine
DE3264407D1 (en) Fuel control apparatus for a gas turbine engine
IL63171A0 (en) Fuel nozzle for a gas turbine engine
DE3263471D1 (en) Ignition device for fuel injected into a rapidly flowing gas stream
JPS5751916A (en) 2-speed governor for fuel injector
JPS56168037A (en) Fuel injector for gas turbine engine

Legal Events

Date Code Title Description
8339 Ceased/non-payment of the annual fee