CH392153A - Combustion chamber for gas turbine - Google Patents

Combustion chamber for gas turbine

Info

Publication number
CH392153A
CH392153A CH1058261A CH1058261A CH392153A CH 392153 A CH392153 A CH 392153A CH 1058261 A CH1058261 A CH 1058261A CH 1058261 A CH1058261 A CH 1058261A CH 392153 A CH392153 A CH 392153A
Authority
CH
Switzerland
Prior art keywords
combustion chamber
gas turbine
turbine
gas
combustion
Prior art date
Application number
CH1058261A
Other languages
German (de)
Inventor
Reginald Murray Frederick
Janes Ralph
Original Assignee
Rolls Royce
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 filed Critical Rolls Royce
Publication of CH392153A publication Critical patent/CH392153A/en

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
CH1058261A 1960-09-13 1961-09-12 Combustion chamber for gas turbine CH392153A (en)

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
CH392153A true CH392153A (en) 1965-05-15

Family

ID=10325096

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1058261A CH392153A (en) 1960-09-13 1961-09-12 Combustion chamber for gas turbine

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
NL268838A (en)
US3119234A (en) 1964-01-28
DE1217139B (en) 1966-05-18
BE607939A (en) 1962-01-02
GB922069A (en) 1963-03-27

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