GB1114728A - Burner e.g. for a gas turbine engine combustion chamber - Google Patents

Burner e.g. for a gas turbine engine combustion chamber

Info

Publication number
GB1114728A
GB1114728A GB13054/67A GB1305467A GB1114728A GB 1114728 A GB1114728 A GB 1114728A GB 13054/67 A GB13054/67 A GB 13054/67A GB 1305467 A GB1305467 A GB 1305467A GB 1114728 A GB1114728 A GB 1114728A
Authority
GB
United Kingdom
Prior art keywords
burner
gas turbine
combustion chamber
turbine engine
engine combustion
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
GB13054/67A
Inventor
Keith Gradon
Richard Alfred Harvey
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB13054/67A priority Critical patent/GB1114728A/en
Publication of GB1114728A publication Critical patent/GB1114728A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/38Nozzles; Cleaning devices therefor
    • F23D11/383Nozzles; Cleaning devices therefor with swirl means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/24Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space

Abstract

1,114,728. Spray burners. ROLLS-ROYCE Ltd. 20 March, 1967, No. 13054/67. Heading F4T. A burner for a gas turbine has a centrally disposed pilot conduit 20 and a fuel chamber 22 communicating via passages 24, an annulus 25 and swirl slots 26 with an annular duct 27 and pilot jet orifice 31 and fuel can also pass through a bore 34 and hole 36 to fill at least part of the annular vortex flow and prevent or reduce the passage of combustion gases upstream through jet orifice 31.
GB13054/67A 1967-03-20 1967-03-20 Burner e.g. for a gas turbine engine combustion chamber Expired GB1114728A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB13054/67A GB1114728A (en) 1967-03-20 1967-03-20 Burner e.g. for a gas turbine engine combustion chamber

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB13054/67A GB1114728A (en) 1967-03-20 1967-03-20 Burner e.g. for a gas turbine engine combustion chamber
US704803A US3498059A (en) 1967-03-20 1968-02-12 Burner,e.g.,for a gas turbine engine combustion chamber
FR1556547D FR1556547A (en) 1967-03-20 1968-02-20
DE19681626044 DE1626044A1 (en) 1967-03-20 1968-03-06 Burners, especially for the combustion chamber of a gas turbine engine

Publications (1)

Publication Number Publication Date
GB1114728A true GB1114728A (en) 1968-05-22

Family

ID=10015957

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13054/67A Expired GB1114728A (en) 1967-03-20 1967-03-20 Burner e.g. for a gas turbine engine combustion chamber

Country Status (4)

Country Link
US (1) US3498059A (en)
DE (1) DE1626044A1 (en)
FR (1) FR1556547A (en)
GB (1) GB1114728A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2308790A1 (en) * 1975-04-25 1976-11-19 Rolls Royce FUEL INJECTOR FOR GAS TURBINE ENGINE
US5365738A (en) * 1991-12-26 1994-11-22 Solar Turbines Incorporated Low emission combustion nozzle for use with a gas turbine engine
RU2560099C2 (en) * 2011-01-31 2015-08-20 Дженерал Электрик Компани Fuel nozzle (versions)
RU2578785C1 (en) * 2014-07-14 2016-03-27 Публичное акционерное общество "МОТОР СИЧ" Double fuel atomiser "gas plus fuel oil"

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3684186A (en) * 1970-06-26 1972-08-15 Ex Cell O Corp Aerating fuel nozzle
US3958416A (en) * 1974-12-12 1976-05-25 General Motors Corporation Combustion apparatus
US4221558A (en) * 1978-02-21 1980-09-09 Selas Corporation Of America Burner for use with oil or gas
DE3147564C2 (en) * 1980-12-02 1991-07-11 United Technologies Corp., Hartford, Conn., Us
US4798330A (en) * 1986-02-14 1989-01-17 Fuel Systems Textron Inc. Reduced coking of fuel nozzles
DE10353423B3 (en) * 2003-11-15 2005-04-14 Eads Space Transportation Gmbh Rocket motor casing has cooling passages for fuel or liquid oxygen within concentric structure
US7082765B2 (en) * 2004-09-01 2006-08-01 General Electric Company Methods and apparatus for reducing gas turbine engine emissions
FR2896030B1 (en) * 2006-01-09 2008-04-18 Snecma Sa COOLING A MULTIMODE INJECTION DEVICE FOR A COMBUSTION CHAMBER, IN PARTICULAR A TURBOREACTOR
US8096130B2 (en) * 2006-07-20 2012-01-17 Pratt & Whitney Canada Corp. Fuel conveying member for a gas turbine engine
US8161751B2 (en) * 2009-04-30 2012-04-24 General Electric Company High volume fuel nozzles for a turbine engine
CN103471098B (en) * 2012-06-05 2018-02-23 雷乐士公司 Combustion chamber cylinder cover for low NOx liquid-fuel burners
FR3003632B1 (en) * 2013-03-19 2016-10-14 Snecma INJECTION SYSTEM FOR TURBOMACHINE COMBUSTION CHAMBER HAVING AN ANNULAR WALL WITH CONVERGENT INTERNAL PROFILE

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1381095A (en) * 1920-03-27 1921-06-07 Fletcher C Starr Fuel-oil burner
US2595759A (en) * 1948-11-30 1952-05-06 Gen Electric Atomizing nozzle for spraying viscous liquids
US2561939A (en) * 1948-12-30 1951-07-24 A V Roe Canada Ltd Dual spray nozzle for fuel burners
US2771744A (en) * 1952-05-07 1956-11-27 Rolls Royee Ltd Fuel injection means of combustion equipment for gas turbine engines
US2907527A (en) * 1956-04-10 1959-10-06 Thompson Ramo Wooldridge Inc Nozzle
US3091926A (en) * 1959-12-16 1963-06-04 Lucas Industries Ltd Oil burners
US3078046A (en) * 1960-01-01 1963-02-19 Dowty Fuel Syst Ltd Liquid supply systems

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2308790A1 (en) * 1975-04-25 1976-11-19 Rolls Royce FUEL INJECTOR FOR GAS TURBINE ENGINE
US5365738A (en) * 1991-12-26 1994-11-22 Solar Turbines Incorporated Low emission combustion nozzle for use with a gas turbine engine
RU2560099C2 (en) * 2011-01-31 2015-08-20 Дженерал Электрик Компани Fuel nozzle (versions)
RU2578785C1 (en) * 2014-07-14 2016-03-27 Публичное акционерное общество "МОТОР СИЧ" Double fuel atomiser "gas plus fuel oil"

Also Published As

Publication number Publication date
DE1626044A1 (en) 1970-08-20
US3498059A (en) 1970-03-03
FR1556547A (en) 1969-02-07

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