GB650462A - Improvements in or relating to combustion apparatus - Google Patents

Improvements in or relating to combustion apparatus

Info

Publication number
GB650462A
GB650462A GB29268/47A GB2926847A GB650462A GB 650462 A GB650462 A GB 650462A GB 29268/47 A GB29268/47 A GB 29268/47A GB 2926847 A GB2926847 A GB 2926847A GB 650462 A GB650462 A GB 650462A
Authority
GB
United Kingdom
Prior art keywords
whirl
flame tube
annular
fuel
primary air
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
GB29268/47A
Inventor
Hugh Stanley Ellis
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 NL72524D priority Critical patent/NL72524C/xx
Priority to BE485523D priority patent/BE485523A/xx
Application filed by Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB29268/47A priority patent/GB650462A/en
Priority to US53967A priority patent/US2687010A/en
Priority to FR973862D priority patent/FR973862A/en
Publication of GB650462A publication Critical patent/GB650462A/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00—Subject-matter not provided for in other groups of this subclass
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • 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
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2700/00—Special arrangements for combustion apparatus using fluent fuel
    • F23C2700/02—Combustion apparatus using liquid fuel
    • F23C2700/023—Combustion apparatus using liquid fuel without pre-vaporising means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Abstract

650,462. Burners. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. Nov. 3, 1947, No. 29268. [Class 75(i)] [Also in Group XII] In an annular combustion chamber enclosed in an air duct suitable for a gas turbine plant the primary air is introduced into the flame tube so as to cause it to form an annular whirl. The fuel is injected within the whirl in substantially the direction of the circular axis of the whirl. An annular flame tube has inner and outer cylindrical walls 1, 8 and an air inlet 2. Primary air enters the flame tube through holes 4, 5, 6 and moves in a whirl indicated by the arrows B. Fuel is injected along the whirl from pipes 7. Specification 650,528 is referred to.
GB29268/47A 1947-11-03 1947-11-03 Improvements in or relating to combustion apparatus Expired GB650462A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
NL72524D NL72524C (en) 1947-11-03
BE485523D BE485523A (en) 1947-11-03
GB29268/47A GB650462A (en) 1947-11-03 1947-11-03 Improvements in or relating to combustion apparatus
US53967A US2687010A (en) 1947-11-03 1948-10-11 Combustion apparatus
FR973862D FR973862A (en) 1947-11-03 1948-10-20 Improvements to combustion devices

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB29268/47A GB650462A (en) 1947-11-03 1947-11-03 Improvements in or relating to combustion apparatus

Publications (1)

Publication Number Publication Date
GB650462A true GB650462A (en) 1951-02-28

Family

ID=10288831

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29268/47A Expired GB650462A (en) 1947-11-03 1947-11-03 Improvements in or relating to combustion apparatus

Country Status (5)

Country Link
US (1) US2687010A (en)
BE (1) BE485523A (en)
FR (1) FR973862A (en)
GB (1) GB650462A (en)
NL (1) NL72524C (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2742762A (en) * 1951-05-31 1956-04-24 Ca Nat Research Council Combustion chamber for axial flow gas turbines
EP0350503A1 (en) * 1987-12-14 1990-01-17 Sundstrand Corp Fuel injectors for turbine engines.
EP0528297A1 (en) * 1991-08-09 1993-02-24 United Technologies Corporation Single vortex combustor arrangement

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2913874A (en) * 1955-03-30 1959-11-24 Gen Electric Tailpipe thrust augmentor
US2952126A (en) * 1955-05-10 1960-09-13 Midland Ross Corp Combustion unit for supplying hot gas for jet aircraft
BE551418A (en) * 1955-10-28
US3088281A (en) * 1956-04-03 1963-05-07 Bristol Siddeley Engines Ltd Combustion chambers for use with swirling combustion supporting medium
US3000183A (en) * 1957-01-30 1961-09-19 Gen Motors Corp Spiral annular combustion chamber
US3075352A (en) * 1958-11-28 1963-01-29 Gen Motors Corp Combustion chamber fluid inlet construction
NL251000A (en) * 1959-04-28
GB903834A (en) * 1960-05-18 1962-08-22 Rolls Royce Combustion chamber
US3355891A (en) * 1966-05-02 1967-12-05 Barry V Rhodes Ram jet engine and fuel injection system therefor
US3645095A (en) * 1970-11-25 1972-02-29 Avco Corp Annualr combustor
US4891936A (en) * 1987-12-28 1990-01-09 Sundstrand Corporation Turbine combustor with tangential fuel injection and bender jets
US5109671A (en) * 1989-12-05 1992-05-05 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
US5195315A (en) * 1991-01-14 1993-03-23 United Technologies Corporation Double dome combustor with counter rotating toroidal vortices and dual radial fuel injection
US5636510A (en) * 1994-05-25 1997-06-10 Westinghouse Electric Corporation Gas turbine topping combustor
GB2454247A (en) * 2007-11-02 2009-05-06 Siemens Ag A Combustor for a Gas-Turbine Engine Has a Burner Head with Fuel Delivered at a Compound Angle

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1533533A (en) * 1922-06-06 1925-04-14 Int Motor Co Combustion chamber for oil-burning furnaces
CH206286A (en) * 1937-11-18 1939-07-31 Messerschmitt Boelkow Blohm Combustion chamber for gas flow machines, such as. B. gas turbines, especially for use in aircraft.
US2398654A (en) * 1940-01-24 1946-04-16 Anglo Saxon Petroleum Co Combustion burner
BE461591A (en) * 1944-03-16
US2517015A (en) * 1945-05-16 1950-08-01 Bendix Aviat Corp Combustion chamber with shielded fuel nozzle
US2510571A (en) * 1946-05-11 1950-06-06 Esther C Goddard Combustion chamber with annular target area
US2488911A (en) * 1946-11-09 1949-11-22 Surface Combustion Corp Combustion apparatus for use with turbines
BE482256A (en) * 1947-05-23

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2742762A (en) * 1951-05-31 1956-04-24 Ca Nat Research Council Combustion chamber for axial flow gas turbines
EP0350503A1 (en) * 1987-12-14 1990-01-17 Sundstrand Corp Fuel injectors for turbine engines.
EP0350503A4 (en) * 1987-12-14 1990-05-14 Sundstrand Corp Fuel injectors for turbine engines.
EP0528297A1 (en) * 1991-08-09 1993-02-24 United Technologies Corporation Single vortex combustor arrangement

Also Published As

Publication number Publication date
BE485523A (en)
NL72524C (en)
US2687010A (en) 1954-08-24
FR973862A (en) 1951-02-15

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