GB922069A - Combustion chamber for a gas turbine engine - Google Patents

Combustion chamber for a gas turbine engine

Info

Publication number
GB922069A
GB922069A GB31570/60A GB3157060A GB922069A GB 922069 A GB922069 A GB 922069A GB 31570/60 A GB31570/60 A GB 31570/60A GB 3157060 A GB3157060 A GB 3157060A GB 922069 A GB922069 A GB 922069A
Authority
GB
United Kingdom
Prior art keywords
intake
air
combustion chamber
gas turbine
turbine engine
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
GB31570/60A
Inventor
Frederick Reginald Murray
Ralph Janes
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
Priority to NL268838D priority Critical patent/NL268838A/xx
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB31570/60A priority patent/GB922069A/en
Priority to US134452A priority patent/US3119234A/en
Priority to FR872525A priority patent/FR1299453A/en
Priority to BE607939A priority patent/BE607939A/en
Priority to DER31090A priority patent/DE1217139B/en
Priority to CH1058261A priority patent/CH392153A/en
Publication of GB922069A publication Critical patent/GB922069A/en
Expired 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • F23R3/04—Air inlet arrangements
    • 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

Abstract

922,069. Generating combustion products under pressure. ROLLS-ROYCE Ltd. Sept. 7, 1961 [Sept. 13, 1960], No. 31570/60. Class 51 (1). The air intake 24 for one of a series of flame tubes 13 arranged in an annular chamber formed by walls 11, 12 has upstream an elongated crosssection, Fig. 2, which progressively changes to a circular section at its downstream end, Fig. 7. A duct 26, increasing in size from the upstream to the downstream end of the intake, diverts air to the spaces between the flame tubes 13 and the walls 11, 12 so as to ensure an even distribution of air through the apertures 21, 22, 23. Baffle members 25, located in the intake, form a throat 27 in the plane of the burners so as to guide the air towards the centre of the intake and into the ducts 26.
GB31570/60A 1960-09-13 1960-09-13 Combustion chamber for a gas turbine engine Expired GB922069A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
NL268838D NL268838A (en) 1960-09-13
GB31570/60A GB922069A (en) 1960-09-13 1960-09-13 Combustion chamber for a gas turbine engine
US134452A US3119234A (en) 1960-09-13 1961-08-28 Combustion chamber for a gas turbine engine
FR872525A FR1299453A (en) 1960-09-13 1961-09-06 Combustion chamber for gas turbo-engine
BE607939A BE607939A (en) 1960-09-13 1961-09-07 Combustion chamber for gas turbo-engine
DER31090A DE1217139B (en) 1960-09-13 1961-09-12 Combustion chamber for a gas turbine plant
CH1058261A CH392153A (en) 1960-09-13 1961-09-12 Combustion chamber for gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB31570/60A GB922069A (en) 1960-09-13 1960-09-13 Combustion chamber for a gas turbine engine

Publications (1)

Publication Number Publication Date
GB922069A true GB922069A (en) 1963-03-27

Family

ID=10325096

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31570/60A Expired GB922069A (en) 1960-09-13 1960-09-13 Combustion chamber for a gas turbine engine

Country Status (6)

Country Link
US (1) US3119234A (en)
BE (1) BE607939A (en)
CH (1) CH392153A (en)
DE (1) DE1217139B (en)
GB (1) GB922069A (en)
NL (1) NL268838A (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3232054A (en) * 1964-02-20 1966-02-01 Lucas Industries Ltd Liquid fuel combustion apparatus, for jet-propulsion engines, gas turbines, or other prime movers
US3320743A (en) * 1965-09-01 1967-05-23 Comb Efficiency Corp Gasifier and burner
GB1135670A (en) * 1966-04-20 1968-12-04 Rolls Royce Combustion chamber for a gas turbine engine
US3391535A (en) * 1966-08-31 1968-07-09 United Aircraft Corp Burner assemblies
US3500639A (en) * 1968-09-10 1970-03-17 Gen Electric Combustion chamber mounting means
US3930369A (en) * 1974-02-04 1976-01-06 General Motors Corporation Lean prechamber outflow combustor with two sets of primary air entrances
US4597258A (en) * 1984-11-26 1986-07-01 United Technologies Corporation Combustor mount
US9546601B2 (en) * 2012-11-20 2017-01-17 General Electric Company Clocked combustor can array
JP6586389B2 (en) 2016-04-25 2019-10-02 三菱重工業株式会社 Compressor diffuser and gas turbine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2560223A (en) * 1948-02-04 1951-07-10 Wright Aeronautical Corp Double air-swirl baffle construction for fuel burners
GB694484A (en) * 1949-06-30 1953-07-22 Rolls Royce Improvements relating to combustion equipment for gas turbine engines
US2676460A (en) * 1950-03-23 1954-04-27 United Aircraft Corp Burner construction of the can-an-nular type having means for distributing airflow to each can
GB741488A (en) * 1953-02-24 1955-12-07 Lucas Industries Ltd Combustion chambers for jet-propulsion engines, gas turbines and other prime movers
US2930193A (en) * 1955-08-29 1960-03-29 Gen Electric Cowled dome liner for combustors
DE1071419B (en) * 1955-10-14 1959-12-17 Joseph Lucas (Industries) Limited, Birmingham (Großbritannien) Riag combustion chamber for jet engines and the like
US2999359A (en) * 1956-04-25 1961-09-12 Rolls Royce Combustion equipment of gas-turbine engines
DE1066385B (en) * 1956-11-21 1959-10-01 Rolls-Royce Limited, Derby (Großbritannien) Burning plant of gas tank aggregates
GB842677A (en) * 1957-05-28 1960-07-27 Gen Motors Corp Improvements relating to gas turbine engines

Also Published As

Publication number Publication date
BE607939A (en) 1962-01-02
CH392153A (en) 1965-05-15
US3119234A (en) 1964-01-28
DE1217139B (en) 1966-05-18
NL268838A (en)

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