GB691068A - Fuel burning means for a gaseous-fluid propulsion jet - Google Patents

Fuel burning means for a gaseous-fluid propulsion jet

Info

Publication number
GB691068A
GB691068A GB17794/50A GB1779450A GB691068A GB 691068 A GB691068 A GB 691068A GB 17794/50 A GB17794/50 A GB 17794/50A GB 1779450 A GB1779450 A GB 1779450A GB 691068 A GB691068 A GB 691068A
Authority
GB
United Kingdom
Prior art keywords
casing
jet
fuel
supplied
stabilizing device
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
GB17794/50A
Inventor
Sidney Allen
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.)
Armstrong Siddeley Motors Ltd
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
Application filed by Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Publication of GB691068A publication Critical patent/GB691068A/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
    • F23R3/02—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
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

691,068. Generating combustion products under pressure. ARMSTRONG SIDDELEY MOTORS, Ltd. April 18, 1951 [July 17, 1950], No. 17794/50. Class 51(i) [Also in Group XI] Fuel burning means for a gaseous fluid propulsion jet comprises a flame stabilizing device 11 and a tubular casing 14 of small length compared with the length of the jet pipe 18, disposed within the jet pipe, the stabilizing device 11 being of smaller diameter than the casing. Fuel is supplied to an appropriate part of the casing 14 through the manifold 15 so as to ensure proper combustion. Some of the gaseous fluid passes between the casing 14 and the jet pipe 18. Pilot fuel is supplied to the stabilizing device through a pipe 12 and nozzles 27 and the upstream end of the device has swirl vanes 26. Further casings 14a, 14b of increasing diameters are disposed downstream of the casing 14, fuel being supplied to each through manifolds 15a, 15b. As shown, the device 11 is wholly within the casing 14 but it may be arranged entirely upstream or downstream of the casing. The invention is applicable in the case of reheating exhaust gases in a gas turbine jet propulsion plant or in the case of a ram jet. Specification 674.641 is referred to.
GB17794/50A 1950-07-17 1950-07-17 Fuel burning means for a gaseous-fluid propulsion jet Expired GB691068A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
GB691068A true GB691068A (en) 1953-05-06

Family

ID=10322289

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17794/50A Expired GB691068A (en) 1950-07-17 1950-07-17 Fuel burning means for a gaseous-fluid propulsion jet

Country Status (6)

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

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 (en) * 1955-07-07 1960-02-04 Ing habil Fritz A F Schmidt Murnau Dr (Obb) Method and device for regulating gas turbine combustion chambers with subdivided combustion and several pressure levels
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 (en) * 1957-10-19 1961-03-16 Bristol Siddeley Engines Ltd Combustion device for a gas turbine engine
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 (en) * 1960-07-13 1965-05-26 United Aircraft Corp Fuel injector for gas turbine jet engines
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 (en) * 1978-03-28 1986-01-13 Rolls Royce REFINEMENTS MADE TO COMBUSTION DEVICES FOR GAS TURBINE ENGINES
JPS57187531A (en) * 1981-05-12 1982-11-18 Hitachi Ltd Low nox gas turbine burner
GB2284884B (en) * 1993-12-16 1997-12-10 Rolls Royce Plc A gas turbine engine combustion chamber
JP2007113888A (en) * 2005-10-24 2007-05-10 Kawasaki Heavy Ind Ltd Gas turbine engine combustor structure

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
CH313855A (en) 1956-05-15
US2704435A (en) 1955-03-22
DE887286C (en) 1953-08-20
BE503026A (en)
FR1036194A (en) 1953-09-04

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