CH313855A - Dispositif de combustion - Google Patents

Dispositif de combustion


Publication number
CH313855A CH313855DA CH313855A CH 313855 A CH313855 A CH 313855A CH 313855D A CH313855D A CH 313855DA CH 313855 A CH313855 A CH 313855A
Prior art keywords
Prior art date
Application number
Other languages
English (en)
Allen Sidney
Original Assignee
Armstrong Siddeley Motors Ltd
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 GB313855X priority Critical
Application filed by Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Publication of CH313855A publication Critical patent/CH313855A/fr



    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous 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
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
CH313855D 1950-07-17 1951-06-18 Dispositif de combustion CH313855A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB313855X 1950-07-17

Publications (1)

Publication Number Publication Date
CH313855A true CH313855A (fr) 1956-05-15



Family Applications (1)

Application Number Title Priority Date Filing Date
CH313855D CH313855A (fr) 1950-07-17 1951-06-18 Dispositif de combustion

Country Status (6)

Country Link
US (1) US2704435A (fr)
BE (1) BE503026A (fr)
CH (1) CH313855A (fr)
DE (1) DE887286C (fr)
FR (1) FR1036194A (fr)
GB (1) GB691068A (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2806516A (en) * 1952-03-28 1957-09-17 Thermo Mecanique Soc Combustion apparatus for use with boilers
US2913874A (en) * 1955-03-30 1959-11-24 Gen Electric Tailpipe thrust augmentor
DE1074920B (fr) * 1955-07-07
US3067582A (en) * 1955-08-11 1962-12-11 Phillips Petroleum Co Method and apparatus for burning fuel at shear interface between coaxial streams of fuel and air
US2999359A (en) * 1956-04-25 1961-09-12 Rolls Royce Combustion equipment of gas-turbine engines
US2974488A (en) * 1956-11-27 1961-03-14 Snecma Combustion devices for continuous-flow internal combustion machines
DE1102491B (de) * 1957-10-19 1961-03-16 Bristol Siddeley Engines Ltd Verbrennungseinrichtung fuer ein Gasturbinentriebwerk
US2988878A (en) * 1958-07-14 1961-06-20 United Aircraft Corp Fuel nozzle for bypass engine
US3078666A (en) * 1958-08-29 1963-02-26 Tuval Miron Method and apparatus for the combustion of fuel
US3085401A (en) * 1959-01-22 1963-04-16 Rolls Royce Reheat combustion equipment of gas-turbine engines
US3066926A (en) * 1959-04-23 1962-12-04 Air Prod & Chem Air heating method
US3166904A (en) * 1960-05-18 1965-01-26 Melenric John Alden Combustion chamber for gas turbine engines
US3087301A (en) * 1960-07-13 1963-04-30 United Aircraft Corp Leading edge fuel manifold
DE1193734B (de) * 1960-07-13 1965-05-26 United Aircraft Corp Brennstoffeinspritzvorrichtung fuer Gasturbinen-Strahltriebwerke
US3210928A (en) * 1960-08-19 1965-10-12 Joseph J Zelinski Fuel cooled combustor assembly
US3338051A (en) * 1965-05-28 1967-08-29 United Aircraft Corp High velocity ram induction burner
IT1111808B (it) * 1978-03-28 1986-01-13 Rolls Royce Perfezionamenti apportati ai dispositivi di combustione di motori a turbina a gas
JPH0370128B2 (fr) * 1981-05-12 1991-11-06 Hitachi Ltd
GB2284884B (en) * 1993-12-16 1997-12-10 Rolls Royce Plc A gas turbine engine combustion chamber
JP2007113888A (ja) * 2005-10-24 2007-05-10 Kawasaki Heavy Ind Ltd ガスタービンエンジンの燃焼器構造

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2517015A (en) * 1945-05-16 1950-08-01 Bendix Aviat Corp Combustion chamber with shielded fuel nozzle
US2417445A (en) * 1945-09-20 1947-03-18 Pinkel Benjamin Combustion chamber
US2518000A (en) * 1946-03-01 1950-08-08 Daniel And Florence Guggenheim Auxiliary combustion chambers for reaction jet propulsion apparatus
US2520388A (en) * 1946-11-21 1950-08-29 Power Jets Res & Dev Ltd Apparatus for supporting combustion in fast-moving air streams
US2545495A (en) * 1947-08-06 1951-03-20 Westinghouse Electric Corp Annular combustion chamber air flow arrangement about the fuel nozzle end
US2560207A (en) * 1948-02-04 1951-07-10 Wright Aeronautical Corp Annular combustion chamber with circumferentially spaced double air-swirl burners
US2592110A (en) * 1949-05-21 1952-04-08 Curtiss Wright Corp Orifice type flame holder construction
US2548087A (en) * 1950-01-21 1951-04-10 A V Roe Canada Ltd Vaporizer system for combustion chambers

Also Published As

Publication number Publication date
FR1036194A (fr) 1953-09-04
US2704435A (en) 1955-03-22
DE887286C (de) 1953-08-20
BE503026A (fr)
GB691068A (en) 1953-05-06

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